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267 Commits

Author SHA1 Message Date
Ramon Roche c5f2a32c96 ci: build each platform on its own arch 2025-02-27 08:48:02 -08:00
Ramon Roche fd06661da9 ci: test container build push 2025-02-27 07:41:13 -08:00
Ramon Roche b786006443 ci: only build amd64 for tests
avoids docker engine error when trying to export manifest lists
2025-02-26 20:48:39 -08:00
Ramon Roche 379bb181f2 ci: multi platform container build
saves cache to s3 and defaults to gh public cache
2025-02-26 20:39:56 -08:00
Ramon Roche c942530825 ci: only push containers on tag events 2025-02-26 19:29:52 -08:00
Ramon Roche b5993c4ec0 setup: install all compilers for arch
plus better output formatting
2025-02-26 19:27:39 -08:00
Ramon Roche cdaaf81354 ci: build containers on releases only 2025-02-25 21:21:59 -08:00
Ramon Roche d60d760eb4 ci: build targets using px4-dev container 2025-02-25 21:21:59 -08:00
Eric Katzfey 0cb7b8b525 voxl2: Changed from old CONFIG_BOARD_ROOTFSDIR to new CONFIG_BOARD_ROOT_PATH in Posix builds (#24392) 2025-02-25 21:54:43 -05:00
Ramon Roche e6b80d8800 readme: minor cleanup 2025-02-25 21:16:54 -05:00
Pernilla 65a80dc8e6 VTOL: Don't overwrite attitude setpoint in Stabilized transition modes (#24406)
Co-authored-by: Silvan Fuhrer <silvan@auterion.com>
2025-02-25 20:06:16 +01:00
chfriedrich98 7c63468e8b mecanum: refactor code architecture 2025-02-25 17:06:17 +01:00
Jacob Dahl d602b569b1 msg: fix comments in SensorOpticalFlow and VehicleOpticalFlow (#24337) 2025-02-25 14:04:52 +01:00
bresch c09c63171c MC auto: fix land nudging
Revert removal of isTargetModified as this is required when the target
is changed by "RC help" (nudging) during landing.
2025-02-25 09:11:23 +01:00
Ramon Roche 393d4c13db ci: disable flash workflow comments (#24409)
Signed-off-by: Ramon Roche <mrpollo@gmail.com>
2025-02-24 12:02:28 -09:00
Marco Hauswirth 689db41c57 ci: flash test adjust permissions for downstream forks (#24404)
adds "contents: read" to permissions to enable clones on private forks of PX4 again. (#24404)
2025-02-24 07:33:54 -08:00
Alexander Lerach 2356cb973f Performance & testing targets
* Added minimal configs for performance testing

* Rename recovery to performance

* added mfg_cfg

* fix params & don't inherit from default

* rename performance -> performance-test

---------

Co-authored-by: Igor-Misic <igy1000mb@gmail.com>
2025-02-24 16:02:46 +01:00
Ted 35d96d57f9 control_allocator: Added linearization feature for 4 servo swash plates to prevent binding (#23961)
* control_allocator: Added linearization feature for heli swashplates to help prevent servo binding

* Apply suggestions from code review

Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>

* update description of CA_LIN_SERVO parameter

* update variable name

* add missing semi-colon

* fix variable referenced before assignment

* add missing indentation

Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>

* removed param unnecessary param

* removed whitespace

* remove CA_LIN_SERVO and enable feature if CA_MAX_SERVO_THROW > 0 plus Update param description.

* remove CA_MAX_SVO_THROW from actuators tab to avoid confusion during standard swashplate setup.

* added comment and fixed spelling mistake

* fix spelling mistake

* fix formatting

* reduce CA_MAX_SVO_THROW short description length to stop test failure

* ActuatorEffectivenessHelicopter: clarfification suggestions for servo linearization feature

* remove NAN check.

---------

Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2025-02-24 12:17:11 +00:00
Jacob Dahl 73b51242c8 nuttx: h7: eth: add checks for PHYID in stm32_phyinit
arch: stm32h7: Add support for dual bank flash memory
2025-02-22 08:46:12 -05:00
Jacob Dahl 11704985f3 ci: add write permissions for flash_analysis workflow (#24393) 2025-02-21 15:18:56 -08:00
Hamish Willee 4ea7de449a InternalCombustionEngineControl - doc corrections (#24359)
* InternalCombustionEngineControl - doc corrections

* Update InternalCombustionEngineControl.cpp
2025-02-21 08:34:08 +11:00
Silvan Fuhrer 24da87db12 FW Position Control: keep flaps in landing config during abort if below AIRSPD_MIN (#23877)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-02-20 09:28:27 +01:00
Silvan Fuhrer 29317d90c3 RPM capture: improve description of param RPM_CAP_ENABLE (#24368)
* RPM capture: improve description of param RPM_CAP_ENABLE
---------

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2025-02-20 09:19:43 +01:00
GuillaumeLaine 44d5bfc42c Tools: in px4_msgs copy versioned msgs to common root folder 2025-02-20 07:42:18 +01:00
GuillaumeLaine 86bfac7c8f fix Jenkins: add copy safeguard and copy to unified folder 2025-02-20 07:42:18 +01:00
Jacob Dahl 1db50cb331 mavlink: add missing fields for DISTANCE_SENSOR 2025-02-19 12:11:42 -05:00
Julian Oes 786c2a7f39 drivers/imu/invensense/mpu6000: include cstdlib for size_t 2025-02-19 12:09:54 -05:00
Jacob Dahl af311c8d45 gz: update submodule 2025-02-19 12:08:40 -05:00
Eric Katzfey 98ceb0ce79 voxl_esc: Added GPIO control feature
voxl_esc: Removed obsolete modal_io_data UORB topic
2025-02-19 11:00:15 -05:00
Eric Katzfey 73dbecadf1 Qurt: changed the mutex for I2C for the Qurt platform from a single mutex to one for each bus. (#23531) 2025-02-19 10:59:45 -05:00
chfriedrich98 04a3c4af20 Differential Rover: Refactor and clean up, align with Ackermann rover(#24318)
* differential: refactor code architecture

* Offboard fix

* fix accel/decel slew rate
2025-02-18 18:26:38 +01:00
Silvan Fuhrer 3c129aefa1 Add IC engine control module (#24055)
Internal combustion engine control module.
New actuator functions and RPM based start/restart logic.
Not enabled by default. 

---------

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Pernilla <pernilla@auterion.com>
2025-02-18 17:15:32 +01:00
Perre 412d4390a6 MC Slowmode: Yawstick for gimbal control, vehicle yaw follows gimbal (#24242)
* Yawsticks on gimbal, vehicle follows gimbal in slowmode, once vehicle has taken off

* Increase queue length to avoid automatically unadvertise queued publications with queue length 1

* Improve readability

---------

Co-authored-by: Pernilla <pernilla@auterion.com>
2025-02-18 14:38:11 +01:00
bresch 5e06ab1430 ekf-agp: do not reset to AGP if GNSS fusion is active 2025-02-18 14:35:10 +01:00
Silvan Fuhrer 3be8b680f6 msg_translation: Add vehicle_status_v1 translation
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Silvan Fuhrer 662c66e546 VehicleStatus: bump VERSION to 1 after removal of avoidance_system_required
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Silvan Fuhrer 3119510f25 Remove health_component::avoidance
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Matthias Grob ed9111ec49 Remove obstacle avoidance test with Gazebo classic and ROS 1 2025-02-18 14:33:16 +01:00
Matthias Grob 0b370ab5d3 Remove obstacle avoidance MAVLink Heartbeat check 2025-02-18 14:33:16 +01:00
Silvan 04cd247c90 FlightTaskAuto: remove isTargetModified()
As it is no longer needed w/o avoidance.

Signed-off-by: Silvan <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Silvan a1ff1d8372 tests: remove test_bezier
Signed-off-by: Silvan <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Silvan b916a96e00 Remove uorb topics exclusively used for avoidance
- TrajectoryBezier.msg
- TrajectoryWaypoint.msg
- VehicleTrajectoryBezier.msg
- VehicleTrajectoryWaypoint.msg

Additionally remove TRAJECTORY_REPRESENTATION_WAYPOINTS mavlink stream.

Signed-off-by: Silvan <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Silvan b7b6d45e18 lib: remove bezier
Signed-off-by: Silvan <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Silvan b34a5eb6f7 PositionControllerStatus: remove unused fields
Remove yaw_acceptance and altitude_acceptance_radius fields as they were only
filled by now removed avoidance controller.

Signed-off-by: Silvan <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Silvan 1f2dba68d2 remove avoidance library and logic
Signed-off-by: Silvan <silvan@auterion.com>
2025-02-18 14:33:16 +01:00
Marco Hauswirth d2cbe10243 Clean up temperature msg fields (#24272)
* remove temp field from airspeed.msg, adjust temp selection

* temp-sensor hirarchy: airspeed, ext. baro, default value

* directly use diff-press or baro temp in true-airspeed  calc

* improve clarity

* add enum for temperature source in VehicleAirData.msg
2025-02-18 13:23:10 +01:00
Daniel Agar 90b2290700 Tools: docker_run.sh fix entrypoint as user
- modern docker can specify the user at runtime (--user)
2025-02-18 00:26:06 -05:00
Daniel Agar 38de04a53a Tools/setup/ubuntu.sh: add curl for NXP mr-canhubk3 build (#24346) 2025-02-17 20:06:24 -08:00
Jacob Dahl 46609d5e6c voxl: document enable_debug command (#24353) 2025-02-17 19:55:24 -08:00
Daniel Agar e12c3c00a4 control_allocator: param update avoid temporary
- this is a harmless workaround for a GCC warning (-Wdangling-pointer) false positive
2025-02-17 14:35:15 -05:00
Ramon Roche 024dd701fb readme: update maintainers information (#24305)
* creates new maintainers file per oss best practices
* adds Pedro as Space maintainer
2025-02-17 11:11:37 -08:00
dirksavage88 01549a5832 fix to kconfig newline
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
2025-02-14 15:50:43 -05:00
dirksavage88 5ffa69ff54 fix newline in module.yaml
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
2025-02-14 15:50:43 -05:00
Eric Katzfey b0eb639587 voxl2_io: Updated to latest version from ModalAI fork
- Updated to the latest version of the voxl2_io driver from the ModalAI fork.
 - Moved to the platform independent Serial driver
 - Added voxl2_io driver to the SLPI DSP build
2025-02-14 14:33:38 -05:00
alexklimaj fd5bb9e69c uavcannode rangefinder: only publish reading too far or too close if less than or greater than. Not equal to. 2025-02-14 14:26:39 -05:00
Marco Hauswirth 61d595dc64 reset dist_to_ground_lock if dist_to_bottom is not valid. this avoids a reset to a previous dist_to_ground after a switch back to a valid measurement 2025-02-14 17:10:14 +01:00
bresch fe5c887895 mag check: do not require mag 0
sys_has_mag defines the required number of mags; if one mag is needed,
it can be any instance, not necessarily mag 0
2025-02-14 16:12:20 +01:00
bresch e3fd50667d Mag cal: automatically disable internal mags if external ones are available 2025-02-14 16:12:20 +01:00
Alexander Lerach 430be08131 Add payload tx/rx timeouts to DDS
* Add tx/rx timeouts

* Code style & tx default timeout

* Clarify TX/RX disable value
2025-02-14 14:54:42 +01:00
Alexander Lerach f2471861a3 Fix GPS RTCM instance selection 2025-02-14 09:39:59 +01:00
Eric Katzfey eb18edf5eb Don't allow spacecraft module parameters for VOXL 2 builds (#24336)
- VOXL 2 builds use DISABLE_PARAMS_MODULE_SCOPING for parameters. The new spacecraft module has duplicate symbols with the control_allocator module and so this kills the VOXL 2 build
2025-02-14 00:49:09 -05:00
Alex Klimaj a151d85a1c ARK Cannodes disable mag bias estimator by default (#24327) 2025-02-13 14:29:21 -09:00
Beat Küng 96461cdd7d ci: ignore changes to comments or constants in versioned message check
These can be changed without version increment
2025-02-13 13:02:39 +01:00
Jacob Dahl b77797b490 tools: px_uploader.py: change RuntimeErorr to printf warning for fw_maxsize greater than fw_maxsize (#24321) 2025-02-12 15:28:40 -09:00
Ramon Roche 195961ae83 ci: only push dev container on commit to main 2025-02-12 12:02:11 -05:00
Jacob Dahl 8acac41163 ark: pi6x: fix CDCACM_PRODUCTID (#24320) 2025-02-12 09:48:04 -07:00
Alex Klimaj 98cba19f50 esc_battery: report temperature
Co-authored-by: Jacob Dahl <37091262+dakejahl@users.noreply.github.com>
2025-02-11 21:17:53 -05:00
Beat Küng b96b4fb68d ci: run ROS humble + jazzy for translation node 2025-02-11 13:19:25 +01:00
Beat Küng 5a2fc5ef79 ci: check if a versioned .msg file is changed, a new version is added as well 2025-02-11 13:19:25 +01:00
Beat Küng 947cc7bcbe ci: run unit tests for ros translation node 2025-02-11 13:19:25 +01:00
Beat Küng f6bfa9812e msg: add message translation node for ROS 2025-02-11 13:19:25 +01:00
Beat Küng 975ec30c9c uxrce_dds_client: add DDS message versioning
This adds "_v" + string(T::MESSAGE_VERSION) to the ROS topic if the message
contains a MESSAGE_VERSION field (and the version is non-zero).
2025-02-11 13:19:25 +01:00
Silvan Fuhrer 136f9f48fc FW Position controller: transform RWTO_PSP to rad when used (#24312)
Signed-off-by: Silvan <silvan@auterion.com>
2025-02-11 12:12:11 +01:00
RomanBapst 2b75d2e738 run fog check independently from stuck check
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-02-11 09:08:25 +01:00
RomanBapst 8cedef2dc4 further cleanup
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-02-11 09:08:25 +01:00
RomanBapst 2c4d38e303 fixed mistake
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-02-11 09:08:25 +01:00
RomanBapst 806500fc4a further improve logic
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-02-11 09:08:25 +01:00
RomanBapst 73ade6d05c range finder: remove potential deadlock
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-02-11 09:08:25 +01:00
RomanBapst 35da86c85a improve unit tests for range fog detection
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-02-11 09:08:25 +01:00
alexklimaj 8576b49e49 make format: ignore libuavcan 2025-02-10 21:18:15 -05:00
Alexander Lerach 047578a844 Disarm PWM ESCs before reboot 2025-02-10 18:16:48 +01:00
chfriedrich98 55f51d7e7e ackermann: refactor code architecture 2025-02-10 15:54:24 +01:00
Bertug Dilman ce64263ce7 publish validated airspeed topic (#24302)
* publish validated airspeed topic

* fix typo
2025-02-07 14:44:48 +01:00
mahimayoga 69d95a6664 sf45: separate sensor yaw variable into FRD and sensor frames for clarity.
Obstacle map is created in sensor frame, but scaling for vehicle orientation is done in vehicle FRD frame.
2025-02-07 13:28:17 +01:00
mahimayoga 093b379b6b sf45/collision-prevention: replace repeated code with ObstacleMath library functions. 2025-02-07 13:28:17 +01:00
Pedro Roque e7e76e2e21 Spacecraft build and bare control allocator (#24221) 2025-02-06 23:54:24 -05:00
Marco Hauswirth de1ade8eb8 sensors/vehicle_air_data: only trigger the sensor fallback when the baro_fault flag switches from 0 -> 1 2025-02-06 23:47:32 -05:00
Alexander Lerach fd175d619c boards/modalai/voxl2/target: remove trailing spaces, consistent tabs/spaces in files 2025-02-06 23:43:34 -05:00
bresch 8d296a50f9 FlightTask: properly initialize EKF reset counters
This fixes a race condition when switching from a flight mode that is
not a flight task (e.g.: stabilized). In this case, the reset counters
were initialized to 0 and deltas were applied to the first setpoints if
the EKF had any of its reset counters different from 0.
2025-02-05 13:21:32 -05:00
Junwoo Hwang de650cab9e boards/matek/h743-slim: change parameter path to MicroSD 2025-02-05 13:09:02 -05:00
Daniel Agar bd2a009217 commander: remove MC nav test 2025-02-05 11:58:04 -05:00
alexklimaj 0faec9b3e7 boards: ARK Flow MR 2025-02-04 22:00:14 -05:00
Hamish Willee 9e5cfa330a Commander: Quick calibration supports mag too 2025-02-04 21:58:03 -05:00
Peter van der Perk 64d8f9a3c6 cmake: for vscode launch fallback to gdb-multiarch
Newer toolchains don't ship with arm-none-eabi-gdb hence we should use gdb-multiarch instead
2025-02-03 23:12:30 -05:00
Jacob Dahl 90a806f5f8 ark: v6x: update net config (#24281)
* ark: v6x: disable net binary config, update default net config

* added back CONFIG_IPCFG_BINARY=y

---------

Co-authored-by: Alex Klimaj <alex@arkelectron.com>
2025-02-03 10:10:02 -07:00
mahimayoga 48c0992a7d sf45: refactor how sensor orientation (yaw_cfg) correction is applied to incoming sensor data.
yaw_cfg is now read into the obstacle_distance message as the angle_offset. The offset is computed once at init and applied to each measurement.
2025-02-03 17:17:35 +01:00
mahimayoga 31bff3e5bb sf45: change handle_missed_bins() function logic.
To simplify logic for wrap-around cases and cases in which bins outside the FOV may be filled. Bin indices are offset such that the 0th bin is the first bin within the sensor FOV. This way we can always fill bins from smallest to largest index.
2025-02-03 17:17:35 +01:00
mahimayoga cb332e047d obstacle-math: add standard obstacle map functions.
These functions help simplify repeated calculations accross driver and collision prevention files that are computing bins, angles and sensor offsets in obstacle maps.
2025-02-03 17:17:35 +01:00
Perre f7dadd9b89 Remove inclusion of rotors in library to enable test (#24286) 2025-02-03 15:51:55 +01:00
Julian Oes a9214b3aa3 gimbal: don't spoof gimbal device (#24271)
The current approach was wrong because the gimbal protocol now
handles the case properly where the autopilot is in charge of a
non-MAVLink gimbal.

This means that we don't need to send message "as if we were a gimbal
device" and instead set thet gimbal_device_id to 1 (up to 6) to indicate
we are in charge or a non-MAVLink gimbal.
2025-01-31 12:59:41 +13:00
Matthias Grob 4c2e69b2e6 estimatorCheck: only warn about GPS in modes that require a position but fail all modes if GPS required by configuration 2025-01-30 18:45:10 +01:00
Matthias Grob f142363575 HealthAndArmingChecks: allow to warn in certain modes and fail arming checks in other modes
Previously it was only possible to warn in all modes and fail none or fail and warn in certain modes.
2025-01-30 18:45:10 +01:00
bresch 3b828e157a MC att: clarify prioritization algorithm
Especially rename "mix" which is just the delta yaw angle
2025-01-30 11:28:26 +01:00
Sam 3 Firestorm 1eb9d05f69 Gazebo classic: report correct limits for H480 gimbal yaw (#24269) 2025-01-29 18:37:00 +01:00
Balduin 96105cacc0 SIH airframes: clean up configs
- set SIH_L_ROLL that agrees with CA_* rotor geometry
 - remove unnecessary params & comments
 - clarify that ailerons are single channel
2025-01-29 16:22:43 +01:00
Silvan ddf591c4f5 Navigator: use FLT_EPSILON instead of 0.0001f for >0 float comparison
Signed-off-by: Silvan <silvan@auterion.com>
2025-01-29 15:42:51 +01:00
Silvan 2f2e56c097 Navigator: replace custom NAV_EPSILON_POSITION with FLT_EPSILON
Signed-off-by: Silvan <silvan@auterion.com>
2025-01-29 15:42:51 +01:00
Matthias Grob 7e47605871 batteryCheck: separate event messages for low, critical and emergency battery states 2025-01-29 15:32:47 +01:00
Balduin 41c4933e10 add standard vtol airframe 2025-01-29 11:15:00 +01:00
Bertug Dilman a0a2bdaea5 commander: COM_MODE_ARM_CHK parameter to allow mode registration while armed (#24249) 2025-01-28 14:33:15 +01:00
Silvan Fuhrer 58d3e1ea8e test: in VTOL integration test use VTOL_LAND (#24261)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-28 11:22:51 +01:00
Marco Hauswirth 4df65c133e add cs_baro_fault to switch to fallback baro if available (#24260) 2025-01-28 10:37:16 +01:00
Peter van der Perk 92b1f51623 tropic: Fix runtime error on new GCC 2025-01-27 14:20:16 -05:00
Peter van der Perk dc3f6a1608 fmu-v6xrt: Fix runtime error on new GCC
New GCC versions inline builtin function like memcpy. On the fmu-v6xrt we can't call the functions inside imxrt_ocram_initialize because the ram function still needs to be initialized.
This commit add a compile hint to not use builtins inside the imxrt_ocram_initialize function
2025-01-27 14:20:16 -05:00
Balduin 5bca71791a SIH: clean up control surface configuration (#24205)
* fix sign error in appropriate place

In PR https://github.com/PX4/PX4-Autopilot/pull/24175 I changed the
control surface deflection signs in generate_fw_aerodynamics to make the
1103 airframe work correctly. However, this breaks the 1101 airframe,
introducing sing errors there.

So, here the change in generate_fw_aerodynamics is reverted to the state
before PR #24175. Instead, the signs are set correctly by using
the HIL_ACT_REV bitfield in the respective airframe config files.

* match control surface parameters to SIH model
2025-01-27 16:52:29 +01:00
Matthias Grob 165f644580 control_allocator: fix typo and use [0,1] instead of [0%, 100%] in slew rate description
Co-authored-by: Hamish Willee <hamishwillee@gmail.com>
2025-01-27 08:43:11 +01:00
Matthias Grob c1cab2d4e0 control_allocator: add unit for slew rate and reword description 2025-01-27 08:43:11 +01:00
bresch c76e74338b ekf-replay: fix airspeed replay
If available, the EKF uses airspeed_validated, not airspeed
2025-01-26 23:05:39 -05:00
alexklimaj c3ba39f931 dshot: remove dshot 1200 2025-01-23 23:50:50 -05:00
cuav-liu1 1aab194f9e boards: fix 7-nano pwm voltage control pin not initialized 2025-01-23 15:58:49 -05:00
Silvan Fuhrer d0042aa275 FW defaults: remove EKF2_GPS_CHECK custom FW setting
We want to align the default over all vehicle types for
this param. There are still some thresholds that are
increased for FW.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-23 15:56:52 -05:00
Alex Klimaj 07e7c64e60 drivers/power_monitor/ina238: retry if read fails
* ina238: retry if read fails
* ina238: increase retries and only publish not connected if register check fails
* ina238: use I2C resets
2025-01-22 15:32:26 -05:00
Daniel Agar 6322ebc3db rcS: shift sensors + EKF startup earlier
- we want the drivers, sensors hub, and estimator running as soon as possible to initialize and avoid commander false positives complaining about missing data
2025-01-22 15:27:56 -05:00
PX4 BuildBot 752b25235c boards: update all NuttX defconfigs 2025-01-22 14:46:36 -05:00
PX4 BuildBot 1aa83d954b update all px4board kconfig 2025-01-22 14:46:24 -05:00
Julian Oes e3b98e6ed2 Tools: remove unused/wrong define and fix comment 2025-01-22 11:26:10 -05:00
Roman Bapst 045c8d9831 Mission feasibility checks: make adding new check less error prone (#24241)
* make adding new feasibility checks less prone to errors

Signed-off-by: RomanBapst <bapstroman@gmail.com>

* Update src/modules/navigator/MissionFeasibility/FeasibilityChecker.hpp

Co-authored-by: Silvan Fuhrer <silvan@auterion.com>

---------

Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-22 16:56:31 +01:00
RomanBapst 57fdda597b vtol_takeoff: store altitude on takeoff and don't use home position altitude
as vehicle does not need to be close to home position

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-01-22 14:03:18 +03:00
PavloZMN ee150a15b4 Optical Flow: add unit testes for only using downward distance sensor (#23266)
* Test for Optical Flow checks correct camera position

* Formatting fixed

* Update src/modules/sensors/vehicle_optical_flow/test/CMakeLists.txt

Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>

* Update src/modules/sensors/vehicle_optical_flow/test/VehicleOpticalFlowTest.cpp

Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>

* Update src/modules/sensors/vehicle_optical_flow/test/VehicleOpticalFlowTest.cpp

Co-authored-by: Silvan Fuhrer <silvan@auterion.com>

* For test GIVEN/WHEN/THEN added

---------

Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>
Co-authored-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-22 11:58:07 +01:00
bresch caaae6ed51 ekf2: allow sideslip fusion to always start with airspeed fusion
This allow sideslip fusion to start during VTOL front transition or even
on a multirotor with a vertical stabilizer and an airspeed sensor for example.
2025-01-22 09:33:16 +01:00
Jacob Dahl 1900d2c98f uavcan: fix hw_errors from mutex lock, hide ESC/Servo status if no function set (#23888) 2025-01-22 12:48:05 +13:00
Jacob Dahl a3215419d7 gz: remove model spawn offset (#24165) 2025-01-22 12:47:25 +13:00
Jacob Dahl 918eca8de4 gz: increase timeout for service request (#24164)
* gz: increase timeout for service request

* change error messages to warnings, specify retrying

* fix typo
2025-01-21 22:14:38 +01:00
Alex Klimaj 8d1bfb77c6 boards: ark fpv add gimbal module (#24229) 2025-01-21 08:59:37 -09:00
RomanBapst f36b45b2ff VehicleOpticalFlow: use 32bit integer for dt
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-01-21 16:48:33 +03:00
RomanBapst c7e494b8d9 VehicleImu: use 32 bit integer for dt
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-01-21 16:48:33 +03:00
RomanBapst 25e76883b7 Integrator: use 32bit integer to store dt to avoid overflow
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-01-21 16:48:33 +03:00
Matthias Grob af062c85eb Revert "FLightTaskAuto: limit nudging speed based on distance sensor"
This reverts commit 97cb933cff.
2025-01-21 09:59:47 +01:00
Marco Hauswirth 7a9608e54b increase EKF2_RNG_FOG for FW and VTOL 2025-01-20 14:43:30 -05:00
Marco Hauswirth 4a5aa1e947 Fix max-hagl restriction to position/altitude control (#23667)
* fix max-hagl restriction to position/altitude control

* max hagl vel restriction in ManAcc position mode

* use interpolate func, change naming

* simplyfied vertical vel limitation

* move velocity-constraint adjustment to StickAccelXY
2025-01-20 15:50:21 +01:00
Mathieu Bresciani 0d22905558 VTOL params: fix param name 2025-01-20 15:50:06 +01:00
Pedro Roque b09340cc98 Control Allocator: Add option for metric allocation (skip normalization) (#24199)
* add: metric allocation

* add: actual files

* rft: moved metric allocation to pseudo-inverse via flag with public method

* del: removed metric allocation test and added test in pseudo-inverse testing

* rft: deleted extra newline at the end of pseudo inverse test file

* feat: removed unnecessary log include
2025-01-20 13:30:51 +01:00
mahimayoga 65a8cc0e0a sf45: scale measured distance with pitch and roll.
Calls function from ObstacleMath library that accounts for the vehicle's attitude w.r.t the obstacle. Obstacles are assumed to be flat, vertical walls.
2025-01-20 11:11:29 +01:00
mahimayoga ab46502cbd obstacle-math: add unit tests for project_distance_on_horizontal_plane function. 2025-01-20 11:11:29 +01:00
mahimayoga 29f981f14c collision-prevention: extract rotation scaling function into new ObstacleMath library.
New library created for static and/or repeated code across collision prevention and driver files.
2025-01-20 11:11:29 +01:00
Daniel Agar b1ca0495e2 ekf2: yaw estimator additional validity checks 2025-01-20 09:45:41 +01:00
Balduin 1eb9434b8c stream ATTITUDE_QUATERNION in low bandwidth mode 2025-01-17 11:20:12 +01:00
Matthias Grob f693fab7c8 rc_update params: remove comment about default static mixing
Was added back in 2014:
7441efde47
2025-01-17 08:18:42 +01:00
alexklimaj 33841cf438 Update GPS submodule 2025-01-15 11:54:04 -05:00
bresch c99cb6e94b ekf2: do not auto-generate sideslip measurement jacobian
This is to trade a bit of CPU load for more flash space.
2025-01-15 11:05:50 -05:00
Matthias Grob e01fef755a Control allocation: make heli rpm control an optional build flag disabled by default
to save flash.
The rpm capture dirver is also disabled on default releases
2025-01-15 14:35:35 +01:00
Mathieu Bresciani 8ecb76aba2 [Multirotor] add yaw torque low pass filter (#24173)
co-authored-by: danielmellinger <107884356+danielmellinger@users.noreply.github.com>
co-authored-by: Eric Katzfey <eric.katzfey@modalai.com>
2025-01-15 14:02:28 +01:00
Jaeyoung Lim 974446c0e8 Make control allocation and actuator effectiveness a non-module-specific library (#24196)
* Remove more circular dependencies with ActuatorEffectiveness

* Separate vehicle specific actuator effectiveness

Keep actuator effectivenss in control allocator

* Remove test dependency for now

* Group library directories
Fix

* Change directory names

* Rebase fix
2025-01-15 10:12:29 +01:00
Minderring 3064a4ad4c boards configs: add airspeed driver for micoair743 aio and v2 2025-01-14 21:45:49 -05:00
PX4 BuildBot 9f8325e8e0 Update submodule mavlink to latest Wed Jan 15 00:39:11 UTC 2025
- mavlink in PX4/Firmware (fd5b52d4c53f35a520646a6c4ec75588f6b87e0f): https://github.com/mavlink/mavlink/commit/5e3a42b8f3f53038f2779f9f69bd64767b913bb8
    - mavlink current upstream: https://github.com/mavlink/mavlink/commit/619947d8bc29e80eecff18b0f4fecc42d9e171dd
    - Changes: https://github.com/mavlink/mavlink/compare/5e3a42b8f3f53038f2779f9f69bd64767b913bb8...619947d8bc29e80eecff18b0f4fecc42d9e171dd

    619947d8 2024-12-19 Hamish Willee - common.xml - PING fix (#2197)
2f44ceff 2024-12-18 Julian Oes - common: use camera ID for CAMERA_IMAGE_CAPTURED (#2196)
2025-01-14 21:45:04 -05:00
bresch 12a9087e92 ekf2: constrain max variance by zero innovation update
Clipping the variance of the covariance matrix has a destabilizing
effect as it increases the correlation between the states.
2025-01-14 21:42:33 -05:00
Ramon Roche 0723f75993 ci: move to px4 git tag versions 2025-01-14 13:10:56 -05:00
Matthias Grob bc92008885 RpmControl: Better consider the case where there's no rpm measurement (anymore) 2025-01-14 14:55:34 +01:00
Matthias Grob b584f8381c Helicopter defaults: don't auto disarm so quickly after spoolup 2025-01-14 14:55:34 +01:00
Matthias Grob 5e2848312d Commander: start timer for auto disarm after spoolup 2025-01-14 14:55:34 +01:00
Matthias Grob 2506bd3b5d RpmControl: simplify the entire control logic 2025-01-14 14:55:34 +01:00
Matthias Grob 1c4325db6d RpmControl: split into cpp source file fixing includes 2025-01-14 14:55:34 +01:00
Matthias Grob 2772ae7e0e RpmControl: maximum rpm outliers are now caught by RpmCapture 2025-01-14 14:55:34 +01:00
Matthias Grob ddd410e9d8 RpmControl: remove status message because it by now only contains redundant information 2025-01-14 14:55:34 +01:00
Matthias Grob 4050cedfaf RpmControl: call local message instance after message name following the convention 2025-01-14 14:55:34 +01:00
Matthias Grob cd0e04f8b0 RpmControl: name current timestamp now following the convention 2025-01-14 14:55:34 +01:00
oravla5 ee67e4bb28 RpmControl: class clean up 2025-01-14 14:55:34 +01:00
Matthias Grob 940fe45ba7 ControlAllocator: introduce helicopter rotor rpm controller 2025-01-14 14:55:34 +01:00
Matthias Grob 50092a7f67 NuttX: update submodule to branch px4_firmware_nuttx-10.3.0+ with "FlexSPI allow RWW" merged 2025-01-14 10:32:00 +01:00
alexklimaj e89a79b382 boards: disable multi ekf on all ark flight controllers 2025-01-14 02:29:07 -05:00
Silvan Fuhrer a16f7859ac boards: disable CONFIG_EKF2_AUX_GLOBAL_POSITION on some boards
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-14 02:19:49 -05:00
Silvan Fuhrer e4e975806f Enable CONFIG_EKF2_AUX_GLOBAL_POSITION by default
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-14 02:19:49 -05:00
Jacob Dahl 0fb8463b79 logger: always log can_interface_status (#24071)
* logger: always log can_interface_status

* logger: log topic can_interface_status using CONFIG_BOARD_UAVCAN_INTERFACES
2025-01-13 10:15:40 -07:00
mahimayoga 879e0ea9b1 MC-hte: use allocated thrust as input for hover thrust estimator.
Improves estimates on vehicles where thrust is often saturating.
2025-01-13 11:56:09 +01:00
mahimayoga 28fa044386 MC-stabilized: rescale thrust input to hover thrust at zero stick input
Use hover thrust estimate in stabilized mode to rescale stick inputs. Prevents vehicle from losing/gaining altitude when switching from position to stabilized mode.
2025-01-13 11:56:09 +01:00
Jaeyoung-Lim f5c05f6d01 Take 2: Cleanup circular dependencies ActuatorEffectiveness 2025-01-13 09:29:42 +01:00
Jaeyoung Lim 208d37e703 Remove circular dependency if control allocation (#24195)
... and actuator effectiveness
2025-01-10 16:58:15 +01:00
Balduin a231fafafa SIH: Add Standard VTOL Airframe (#24175)
* add standard vtol airframe to SIH.

mostly took changes from 4d930bde and applied to main.

generate_fw_aerodynamics now takes four arguments rather than using the
_u class member, because depending on vehicle type _u is used
differently.
2025-01-09 15:40:06 +01:00
Silvan Fuhrer 44b423f48d drivers: ulanding: description: fix link to user guide section (#24189)
Signed-off-by: Silvan <silvan@auterion.com>
2025-01-09 08:54:58 +01:00
Jari Nippula cbbbbc9dfa logger: fix file open issue if crypto algorithm is disabled
move init_logfile_encryption() call after the buffer start_log() call
to have log file already open while storing the header and key data to
the beginning of the file.
2025-01-09 07:45:09 +01:00
bresch ab70ae3252 ekf2: fix GNSS drift false alarm
In SIH, the GNSS signal is zero-mean, but apparently not symmetric. The
issue is that saturating such a signal creates an artificial bias. This
made the check fail as the bias was above the threshold.
2025-01-08 21:40:25 -05:00
Peter van der Perk e9536cb30b Tropic-community use flash as storage using LittleFS (#24158)
* Update NuttX
2025-01-08 21:35:08 -05:00
Matthias Grob b042f2101f system_params: clarify SYS_HAS_MAG description
after answering the questions:
Ah the value can be 2? Should I set the number of magnetometers the board has or include the external ones?
2025-01-08 21:24:00 -05:00
mahimayoga c3e370b946 MC land detector: fix parameter description for LNDMC_ROT_MAX 2025-01-08 18:03:35 +01:00
mahimayoga b4273bde25 FW land detector: Introduce max rotational speed condition (new param: LNDFW_ROT_MAX).
Checks that the filtered norm of the angular velocity is below LNDFW_ROT_MAX.
2025-01-08 18:03:35 +01:00
mahimayoga 18b4b18a75 FW land detector: do not check for groundspeed if invalid.
In case the local position speed estimate is not valid, it is assumed to be 0m/s and
thus check always passes.
2025-01-08 18:03:35 +01:00
alexklimaj 2625c5211b dronecan: don't init if can interface fails to init 2025-01-08 11:12:57 -05:00
Silvan Fuhrer 585e5d1482 MissionBase: remove unused param
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-08 09:31:55 +01:00
Silvan Fuhrer d98a706380 RTL fast reverse: enable precision landing
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-08 09:31:55 +01:00
Silvan Fuhrer 368bbfeb3b RTL params: make clear that RTL_PLD_MD does not apply for mission RTL destinations
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-08 09:31:55 +01:00
Silvan Fuhrer e29c86c81f rtl_direct: don't check RTL_PLD_MD param twice but use _mission_item.land_precision
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-08 09:31:55 +01:00
Silvan Fuhrer 0ecc8278b6 Navigator: RTL_direct: onyl start precision land if param is set to enable
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-08 09:31:55 +01:00
RomanBapst 1abc27dd1f remove fixed-wing condition from airspeed fusion condition
- enables airspeed fusion to begin during transition already
- airspeed fusion is started based on airspeed being above defined threshold

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2025-01-07 16:19:33 +01:00
bresch b1773df441 ekf2: fix comments about primary height sources
Having the xxx_hgt flag set only means that the sensor is fused for
altitude/height aiding. It's not necessarily the height reference.
2025-01-07 10:23:13 +01:00
ZeroOne-Aero 374e70c48f ZeroOne X6: add IST8310 support 2025-01-07 09:14:31 +01:00
Silvan 8070a9b362 Commander: remove not used include of blocks.hpp
Signed-off-by: Silvan <silvan@auterion.com>
2025-01-06 09:24:29 +01:00
Alex Klimaj 821558f9e3 boards: ark flow set SENS_FLOW_RATE default to 150 (#24170) 2025-01-03 11:45:33 -09:00
Alex Klimaj 1043aebf5d analog_battery: add option for filter (#23987) 2025-01-03 16:01:16 +01:00
bresch f1a339e7c6 fw-att: avoid multiple conversions 2025-01-03 15:07:52 +01:00
bresch 9bf5257e0e fw-att: fix wheel controller 2025-01-03 15:07:52 +01:00
Silvan Fuhrer 326d486397 SITL: remove setting CBRK_SUPPLY_CHK by default
This allows us to run battery failsafe tests again in SITL
wihtout having to change params first.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-03 14:07:15 +01:00
Silvan Fuhrer e2ea48bb79 Simulation: add SystemPowerSimulator to publish SystemPower.msg in sim
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-03 14:07:15 +01:00
Silvan Fuhrer eac12ee9ce BatterySimulation: remove unused _battery_pub
The simulated battery is published by the regular battery class.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2025-01-03 14:07:15 +01:00
Nicolas MARTIN 4fe6d69966 local position acceleration: use mean value between two publications (#24105)
To avoid aliasing on the ned acceleration, add an accumulation of acceleration to improve the downsampling
2025-01-03 12:43:39 +01:00
bresch c1589ddb18 ekf2-rng: do not continuously reset terrain in rng height ref
When the height reference datum is ground level (range finder height
ref), the terrain state is not updated through fusion and should stay at
a constant altitude.
2025-01-03 12:25:16 +01:00
Jacob Dahl 0b1838f233 test: add test for range finder fusion while on ground 2025-01-03 12:25:16 +01:00
Daniel Agar 81552fc036 uavcan: relax UAVCAN_RNG_MIN/UAVCAN_RNG_MAX defaults (#24140)
- this is optional sensor metadata that can be set if actually needed
2024-12-26 19:10:31 -07:00
Jacob Dahl fb2bdc0ecc boards: ark_fpv: add msp osd 2024-12-23 21:57:59 -05:00
Alex Klimaj 291300e167 ARK TESEO Bootloader Placeholder 2024-12-23 21:57:24 -05:00
Minderring 8d4663ed5a boards: add micoair743-v2 config files to PX4-Autopilot 2024-12-23 21:56:54 -05:00
Minderring 0b27200629 boards: fix some configs for micoair743 and aio 2024-12-23 21:55:52 -05:00
Matthias Grob 2968af7b63 Carzyflie: don't compile Navigator ADSB handling
I forgot to stage that change in the original change:
839010eeab
2024-12-23 21:55:08 -05:00
Mahima Yoga defccfa99b Collision Prevention: Scale obstacle distance with vehicle attitude for varying sensor orientations (#24107) 2024-12-20 14:47:22 +01:00
Roman Bapst b765769f50 Navigator: Set altitude acceptance radius to infinity when moving to land point after transition (#24115)
* Navigator: set alt acceptance radius to infinity
for land waypoint after backtransition -> avoid
vehicle with depleted battery from not reaching the alt
setpoint and getting stuck

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2024-12-20 09:21:32 +01:00
Matthias Grob 61961350f9 mavlink_receiver: don't publish out of range joystick input
Note that the MAVLink definition explicitly writes
"A value of INT16_MAX indicates that this axis is invalid."
which before this change was happily executed.
2024-12-19 17:59:41 +01:00
Matthias Grob 5cf85e320a offboardCheck: acceleration setpoints only require vehicle attitude control 2024-12-19 17:58:38 +01:00
Matthias Grob ad799b64b7 mc_pos_control: shorten parameter descriptions to a readable size 2024-12-19 16:12:43 +01:00
Matthias Grob 1239f0aaed FlightTaskTransition: Comment why using invalid horizontal velocity works 2024-12-19 16:00:21 +01:00
Matthias Grob 34bcc277a5 FlightTaskTransition: keep high decelration when overshooting the transition target 2024-12-19 16:00:21 +01:00
Matthias Grob 11d7dd41fd FlightTaskTransition: clean up and simplify 2024-12-19 16:00:21 +01:00
Matthias Grob 839010eeab Navigator: make ADSB handling optional 2024-12-19 15:30:34 +01:00
Silvan Fuhrer 367a8a7fc4 update gz submodule to get new tiltrotor sim
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-12-19 09:57:55 +01:00
Pernilla 1f48448beb Update other airframes with min max values different than default 2024-12-19 09:57:55 +01:00
Pernilla be42c7c88a Adding min-max angles to use for normalized servo outputs 2024-12-19 09:57:55 +01:00
Pernilla f1855de006 Adding tiltrotor model 2024-12-19 09:57:55 +01:00
Matthias Grob c69f96ec04 ADSB: replace last excess hrt_absolute_time() in the loop 2024-12-19 09:35:38 +01:00
Silvan Fuhrer 30e51cb80e ADSB: improve readability of unit tests
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-12-19 09:35:38 +01:00
Silvan Fuhrer 1a1fd59302 ADSB: pass now timestamp as arguemnt of send_traffic_warning()
Saves some flash and CPU by not having to call hrt_absolute_time().

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-12-19 09:35:38 +01:00
Silvan Fuhrer 741e3e8589 ADSB: pass now timestamp as arguemnt of get_traffic_state()
That enables us to time the unit tests better plus saves some flash and CPU.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-12-19 09:35:38 +01:00
Marco Hauswirth bdc6957c11 dont use BROACAST_MODE_ON during unit testing 2024-12-19 07:44:45 +01:00
Matthias Grob 077ade4f8f Add IO timer channel mode for RPM and also sync up rpi configuration to work with all these drivers 2024-12-19 07:30:25 +01:00
Matthias Grob b85ad98a98 Use defines instead of hardcoded magic values for maximum number of output channels and rpm filter time constant 2024-12-19 07:30:25 +01:00
Matthias Grob 8ce6ad6662 camera_capture: refactor to simplify capture channel initialization 2024-12-19 07:30:25 +01:00
Matthias Grob 267fa06da8 RPMCapture: fix copyright year, improve comments 2024-12-19 07:30:25 +01:00
Matthias Grob f4c8e0e35f RPMCapture: fix dt should not have a minimum which would limit to 6000rpm 2024-12-19 07:30:25 +01:00
Matthias Grob b7b384ab2e RPMCapture: add back filter reset on timeout 2024-12-19 07:30:25 +01:00
Matthias Grob d027f8bf39 RPMCapture: publish outliers in rpm message but don't update the filters and estimate 2024-12-19 07:30:25 +01:00
Matthias Grob 9ca06be4f5 RPMCapture: refactor to clarify scheduling 2024-12-19 07:30:25 +01:00
Matthias Grob c406e0a3a2 RPMCapture: refactor to clarify when an interrupt happened 2024-12-19 07:30:25 +01:00
Matthias Grob ec4ed75264 RPMCapture: define period as UINT32_MAX when timed out 2024-12-19 07:30:25 +01:00
Matthias Grob 825dc47fad RPMCapture: fix pulses per revolution parameter name, description, type -> use module params 2024-12-19 07:30:25 +01:00
oravla5 d31271c38e RPMCapture: added pulse per rev parameter. Do not publish if pulses are to fast 2024-12-19 07:30:25 +01:00
bresch 1b105c937d RpmControl: remove raw RPM spikes using median filter 2024-12-19 07:30:25 +01:00
Silvan Fuhrer f687e3d8a4 RPM capture: publish every 1s without new data
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-12-19 07:30:25 +01:00
Matthias Grob 6241db74db mavlink: stream RAW_RPM message for ONBOAR_LOW_BANDWIDTH 2024-12-19 07:30:25 +01:00
Matthias Grob 8486f74b2a RPMCapture: much better timeout scheduling
Not timing out based on a random interval but based
on the time after the last inerrupt.
2024-12-19 07:30:25 +01:00
Matthias Grob c463cc42d0 RPM: clean up message 2024-12-19 07:30:25 +01:00
Matthias Grob a60591378c RPMCapture: switch to PublicationMulti to be compatible with the existing rpm drivers 2024-12-19 07:30:25 +01:00
Matthias Grob 41b55724bc RPMCapture: Detect rpm sensing timeout 2024-12-19 07:30:25 +01:00
Matthias Grob 1bcdb3ef8c RPMCapture: add hardcoded rpm processing
Such that we can continue development on this part.
The implementation was already used before porting things into the RPM capture module.
2024-12-19 07:30:25 +01:00
Beat Küng 491ee01ac4 rpm_capture: add rpm capture driver, publising pwm_input (for now) 2024-12-19 07:30:25 +01:00
Matthias Grob ef823e5bb1 gz submodule: switch to hash on submodule main branch
after https://github.com/PX4/PX4-gazebo-models/pull/71 was merged
2024-12-18 18:06:37 +01:00
Perre 8a9391321d Adding gimbal rate in gz simulation (#24125)
* Adding gimbal rate in gz simulation

* add submodule
2024-12-18 16:25:12 +01:00
bresch 6b10f1ca12 ekf: update change indicator
The calculation of "alpha" in the accel_horiz and height_rate lowpass
filters is slightly different than before.
2024-12-18 14:11:08 +01:00
bresch 480c232bfd ekf2: use alpha filter class 2024-12-18 14:11:08 +01:00
bresch fa5a781e20 AlphaFilter: set time constant instead of alpha
Then the update function can set the dt at every iteration if needed
2024-12-18 14:11:08 +01:00
bresch 37401d6fd1 AlphaFilter: allow setting dt in update call 2024-12-18 14:11:08 +01:00
Stefano Colli 0561f6c9fc GZ: add gimbal simulation (#23382) 2024-12-18 12:15:03 +01:00
bresch 4a73195007 yaw_est: store attitude as quaternion instead of DCM
This saves flash and makes code simpler
2024-12-18 09:33:11 +01:00
Julian Oes 98fde4cbac gimbal: correctly set gimbal_device_id
When we use a gimbal connected via "RC", so PWM via the Aux channels, we
need to set the gimbal_device_id to 1 as per the protocol.

This was missing for GIMBAL_DEVICE_ATTITUDE_STATUS, so I added that, and
fixed the name of that variable while at it.
2024-12-18 07:51:40 +01:00
Beat Küng 9e9d352eb2 mavlink: update submodule
MAV_STANDARD_MODE_SAFE_RECOVERY and MAV_STANDARD_MODE_RETURN_HOME got
merged.
2024-12-18 07:12:36 +01:00
Beat Küng aca5a70964 standard_modes: add vehicle-type specific standard modes
See https://mavlink.io/en/messages/development.html#MAV_STANDARD_MODE.
The only standard mode that is not set is MAV_STANDARD_MODE_SAFE_RECOVERY,
as PX4 uses RTL for that (with configuration parameters).
2024-12-18 07:12:36 +01:00
Ramon Roche 90b968ba4e container: remove pr container push to registry 2024-12-17 22:33:05 -05:00
bresch 6969e5b6b4 ekf2: do not pre-compute airspeed Kalman gain
The generated code is not much faster than the simple matrix-vector
multiplication
2024-12-17 22:32:16 -05:00
Andrew Brahim e7145e7b44 uxrce_dds_client: include distance sensor in dds_topics.yaml
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
2024-12-17 22:28:40 -05:00
Daniel Agar 8a18e5b00c commander: accelerometer calibration respect rotation
- accel cal use Accelerometer calibration class to fully respect
   rotation (both internal and external sensors)
2024-12-17 22:26:01 -05:00
Jaeyoung Lim fd87cd682d Dynamically update ff gain for fw rate control (#24120) 2024-12-17 17:57:18 +01:00
723 changed files with 25196 additions and 10770 deletions
+4 -2
View File
@@ -94,7 +94,7 @@ jobs:
- name: Building [${{ matrix.group }}]
run: |
./Tools/ci/build_all_runner.sh ${{matrix.targets}}
./Tools/ci/build_all_runner.sh ${{matrix.targets}} ${{matrix.arch}}
- name: Arrange Build Artifacts
run: |
@@ -140,10 +140,12 @@ jobs:
release:
name: Create Release and Upload Artifacts
permissions:
contents: write
# runs-on: ubuntu-latest
runs-on: [runs-on,runner=1cpu-linux-x64,image=ubuntu22-full-x64,"run-id=${{ github.run_id }}",spot=false]
needs: [setup, group_targets]
if: startsWith(github.ref, 'refs/tags/v')
if: startsWith(github.ref, 'refs/tags/')
steps:
- name: Download Artifacts
uses: actions/download-artifact@v4
+16 -18
View File
@@ -16,9 +16,13 @@ on:
jobs:
build:
name: Build and Push Container
runs-on: [runs-on,runner=8cpu-linux-x64,image=ubuntu22-full-x64,"run-id=${{ github.run_id }}",spot=false]
name: Build and Push Container (${{ matrix.arch }})
strategy:
matrix:
arch: [x64, arm64]
runs-on: [runs-on,"runner=8cpu-linux-${{ matrix.arch }}","image=ubuntu24-full-${{ matrix.arch }}","run-id=${{ github.run_id }}",spot=false,extras=s3-cache]
steps:
- uses: runs-on/action@v1
- uses: actions/checkout@v4
with:
fetch-tags: true
@@ -32,13 +36,14 @@ jobs:
- name: Login to Docker Hub
uses: docker/login-action@v3
if: github.event_name != 'pull_request'
# if: ${{ startsWith(github.ref, 'refs/tags/') }}
with:
username: ${{ secrets.DOCKERHUB_USERNAME }}
password: ${{ secrets.DOCKERHUB_TOKEN }}
- name: Login to GitHub Container Registry
uses: docker/login-action@v3
# if: ${{ startsWith(github.ref, 'refs/tags/') }}
with:
registry: ghcr.io
username: ${{ github.actor }}
@@ -52,13 +57,7 @@ jobs:
ghcr.io/PX4/px4-dev
${{ (github.event_name != 'pull_request') && 'px4io/px4-dev' || '' }}
tags: |
type=semver,pattern={{version}}
type=semver,pattern={{major}}.{{minor}}
type=semver,pattern={{major}}
type=ref,event=branch,value=${{ steps.px4-tag.outputs.tag }},priority=700
type=ref,event=branch,suffix=-{{date 'YYYY-MM-DD'}},priority=600
type=ref,event=branch,suffix=,priority=500
type=ref,event=pr
type=raw,enable=true,value=${{ steps.px4-tag.outputs.tag }},priority=1000
- name: Set up Docker Buildx
uses: docker/setup-buildx-action@v3
@@ -70,12 +69,11 @@ jobs:
context: Tools/setup
tags: ${{ steps.meta.outputs.tags }}
labels: ${{ steps.meta.outputs.labels }}
platforms: |
linux/amd64
platforms: linux/${{ matrix.arch == 'x64' && 'amd64' || 'arm64' }}
load: true
push: false
cache-from: type=s3,blobs_prefix=cache/${{ github.repository }}/,manifests_prefix=cache/${{ github.repository }}/,region=${{ env.RUNS_ON_AWS_REGION }},bucket=${{ env.RUNS_ON_S3_BUCKET_CACHE }}
cache-to: type=s3,blobs_prefix=cache/${{ github.repository }}/,manifests_prefix=cache/${{ github.repository }}/,region=${{ env.RUNS_ON_AWS_REGION }},bucket=${{ env.RUNS_ON_S3_BUCKET_CACHE }},mode=max
cache-from: type=gha
cache-to: type=gha,mode=max
- name: Get Tag Name
id: tag_name
@@ -95,13 +93,13 @@ jobs:
- name: Push container image
uses: docker/build-push-action@v6
# if: ${{ startsWith(github.ref, 'refs/tags/') }}
with:
context: Tools/setup
tags: ${{ steps.meta.outputs.tags }}
labels: ${{ steps.meta.outputs.labels }}
platforms: |
linux/amd64
platforms: linux/${{ matrix.arch == 'x64' && 'amd64' || 'arm64' }}
provenance: mode=max
push: true
cache-from: type=s3,blobs_prefix=cache/${{ github.repository }}/,manifests_prefix=cache/${{ github.repository }}/,region=${{ env.RUNS_ON_AWS_REGION }},bucket=${{ env.RUNS_ON_S3_BUCKET_CACHE }}
cache-to: type=s3,blobs_prefix=cache/${{ github.repository }}/,manifests_prefix=cache/${{ github.repository }}/,region=${{ env.RUNS_ON_AWS_REGION }},bucket=${{ env.RUNS_ON_S3_BUCKET_CACHE }},mode=max
cache-from: type=gha
cache-to: type=gha,mode=max
+59 -50
View File
@@ -1,5 +1,10 @@
name: FLASH usage analysis
permissions:
contents: read
pull-requests: write
issues: write
on:
push:
branches:
@@ -83,59 +88,63 @@ jobs:
echo '${{ steps.bloaty-step.outputs.bloaty-summary-map }}' >> $GITHUB_OUTPUT
echo "$EOF" >> $GITHUB_OUTPUT
post_pr_comment:
name: Publish Results
runs-on: [runs-on,runner=1cpu-linux-x64,image=ubuntu24-full-x64,"run-id=${{ github.run_id }}",spot=false]
needs: [analyze_flash]
env:
V5X-SUMMARY-MAP-ABS: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v5x-bloaty-summary-map).vm-absolute) }}
V5X-SUMMARY-MAP-PERC: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v5x-bloaty-summary-map).vm-percentage) }}
V6X-SUMMARY-MAP-ABS: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v6x-bloaty-summary-map).vm-absolute) }}
V6X-SUMMARY-MAP-PERC: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v6x-bloaty-summary-map).vm-percentage) }}
if: ${{ github.event.pull_request }}
steps:
- name: Find Comment
uses: peter-evans/find-comment@v3
id: fc
with:
issue-number: ${{ github.event.pull_request.number }}
comment-author: 'github-actions[bot]'
body-includes: FLASH Analysis
# TODO:
# This part of the workflow is causing errors, we should find a way to fix this and enable this test again
# Track this issue https://github.com/PX4/PX4-Autopilot/issues/24408
#
#post_pr_comment:
#name: Publish Results
#runs-on: [runs-on,runner=1cpu-linux-x64,image=ubuntu24-full-x64,"run-id=${{ github.run_id }}",spot=false]
#needs: [analyze_flash]
#env:
#V5X-SUMMARY-MAP-ABS: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v5x-bloaty-summary-map).vm-absolute) }}
#V5X-SUMMARY-MAP-PERC: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v5x-bloaty-summary-map).vm-percentage) }}
#V6X-SUMMARY-MAP-ABS: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v6x-bloaty-summary-map).vm-absolute) }}
#V6X-SUMMARY-MAP-PERC: ${{ fromJSON(fromJSON(needs.analyze_flash.outputs.px4_fmu-v6x-bloaty-summary-map).vm-percentage) }}
#if: ${{ github.event.pull_request }}
#steps:
#- name: Find Comment
#uses: peter-evans/find-comment@v3
#id: fc
#with:
#issue-number: ${{ github.event.pull_request.number }}
#comment-author: 'github-actions[bot]'
#body-includes: FLASH Analysis
- name: Set Build Time
id: bt
run: |
echo "timestamp=$(date +'%Y-%m-%dT%H:%M:%S')" >> $GITHUB_OUTPUT
#- name: Set Build Time
#id: bt
#run: |
#echo "timestamp=$(date +'%Y-%m-%dT%H:%M:%S')" >> $GITHUB_OUTPUT
- name: Create or update comment
# This can't be moved to the job-level conditions, as GH actions don't allow a job-level if condition to access the env.
if: |
steps.fc.outputs.comment-id != '' ||
env.V5X-SUMMARY-MAP-ABS >= fromJSON(env.MIN_FLASH_POS_DIFF_FOR_COMMENT) ||
env.V5X-SUMMARY-MAP-ABS <= fromJSON(env.MIN_FLASH_NEG_DIFF_FOR_COMMENT) ||
env.V6X-SUMMARY-MAP-ABS >= fromJSON(env.MIN_FLASH_POS_DIFF_FOR_COMMENT) ||
env.V6X-SUMMARY-MAP-ABS <= fromJSON(env.MIN_FLASH_NEG_DIFF_FOR_COMMENT)
uses: peter-evans/create-or-update-comment@v4
with:
comment-id: ${{ steps.fc.outputs.comment-id }}
issue-number: ${{ github.event.pull_request.number }}
body: |
## 🔎 FLASH Analysis
<details>
<summary>px4_fmu-v5x [Total VM Diff: ${{ env.V5X-SUMMARY-MAP-ABS }} byte (${{ env.V5X-SUMMARY-MAP-PERC}} %)]</summary>
#- name: Create or update comment
## This can't be moved to the job-level conditions, as GH actions don't allow a job-level if condition to access the env.
#if: |
#steps.fc.outputs.comment-id != '' ||
#env.V5X-SUMMARY-MAP-ABS >= fromJSON(env.MIN_FLASH_POS_DIFF_FOR_COMMENT) ||
#env.V5X-SUMMARY-MAP-ABS <= fromJSON(env.MIN_FLASH_NEG_DIFF_FOR_COMMENT) ||
#env.V6X-SUMMARY-MAP-ABS >= fromJSON(env.MIN_FLASH_POS_DIFF_FOR_COMMENT) ||
#env.V6X-SUMMARY-MAP-ABS <= fromJSON(env.MIN_FLASH_NEG_DIFF_FOR_COMMENT)
#uses: peter-evans/create-or-update-comment@v4
#with:
#comment-id: ${{ steps.fc.outputs.comment-id }}
#issue-number: ${{ github.event.pull_request.number }}
#body: |
### 🔎 FLASH Analysis
#<details>
#<summary>px4_fmu-v5x [Total VM Diff: ${{ env.V5X-SUMMARY-MAP-ABS }} byte (${{ env.V5X-SUMMARY-MAP-PERC}} %)]</summary>
```
${{ needs.analyze_flash.outputs.px4_fmu-v5x-bloaty-output }}
```
</details>
#```
#${{ needs.analyze_flash.outputs.px4_fmu-v5x-bloaty-output }}
#```
#</details>
<details>
<summary>px4_fmu-v6x [Total VM Diff: ${{ env.V6X-SUMMARY-MAP-ABS }} byte (${{ env.V6X-SUMMARY-MAP-PERC }} %)]</summary>
#<details>
#<summary>px4_fmu-v6x [Total VM Diff: ${{ env.V6X-SUMMARY-MAP-ABS }} byte (${{ env.V6X-SUMMARY-MAP-PERC }} %)]</summary>
```
${{ needs.analyze_flash.outputs.px4_fmu-v6x-bloaty-output }}
```
</details>
#```
#${{ needs.analyze_flash.outputs.px4_fmu-v6x-bloaty-output }}
#```
#</details>
**Updated: _${{ steps.bt.outputs.timestamp }}_**
edit-mode: replace
#**Updated: _${{ steps.bt.outputs.timestamp }}_**
#edit-mode: replace
@@ -0,0 +1,52 @@
name: ROS Translation Node Tests
on:
push:
branches:
- 'main'
pull_request:
branches:
- '*'
defaults:
run:
shell: bash
jobs:
build_and_test:
name: Build and test
runs-on: [runs-on,runner=8cpu-linux-x64,image=ubuntu24-full-x64,"run-id=${{ github.run_id }}",spot=false]
strategy:
fail-fast: false
matrix:
config:
- {ros_version: "humble", ubuntu: "jammy"}
- {ros_version: "jazzy", ubuntu: "noble"}
container:
image: rostooling/setup-ros-docker:ubuntu-${{ matrix.config.ubuntu }}-latest
steps:
- name: Setup ROS 2 (${{ matrix.config.ros_version }})
uses: ros-tooling/setup-ros@v0.7
with:
required-ros-distributions: ${{ matrix.config.ros_version }}
- name: Checkout repository
uses: actions/checkout@v4
with:
fetch-depth: 0
# Workaround for https://github.com/actions/runner/issues/2033
- name: ownership workaround
run: git config --system --add safe.directory '*'
- name: Check .msg file versioning
if: github.event_name == 'pull_request'
run: |
./Tools/ci/check_msg_versioning.sh ${{ github.event.pull_request.base.sha }} ${{github.event.pull_request.head.sha}}
- name: Build and test
run: |
ros_ws=/ros_ws
mkdir -p $ros_ws/src
./Tools/copy_to_ros_ws.sh $ros_ws
cd $ros_ws
source /opt/ros/${{ matrix.config.ros_version }}/setup.sh
colcon build --cmake-args -DCMAKE_BUILD_TYPE=Release --symlink-install --event-handlers=console_cohesion+
source ./install/setup.sh
./build/translation_node/translation_node_unit_tests
+25
View File
@@ -131,6 +131,11 @@ CONFIG:
buildType: MinSizeRel
settings:
CONFIG: ark_can-flow_canbootloader
ark_can-flow-mr_canbootloader:
short: ark_can-flow-mr_canbootloader
buildType: MinSizeRel
settings:
CONFIG: ark_can-flow-mr_canbootloader
ark_can-gps_default:
short: ark_can-gps_default
buildType: MinSizeRel
@@ -166,6 +171,11 @@ CONFIG:
buildType: MinSizeRel
settings:
CONFIG: ark_septentrio-gps_canbootloader
ark_teseo-gps_canbootloader:
short: ark_teseo-gps_canbootloader
buildType: MinSizeRel
settings:
CONFIG: ark_teseo-gps_canbootloader
ark_cannode_default:
short: ark_cannode_default
buildType: MinSizeRel
@@ -301,6 +311,11 @@ CONFIG:
buildType: MiniSizeRel
settings:
CONFIG: matek_gnss-m9n-f4_default
micoair_h743_bootloader:
short: micoair_h743_bootloader
buildType: MinSizeRel
settings:
CONFIG: micoair_h743_bootloader
micoair_h743_default:
short: micoair_h743
buildType: MinSizeRel
@@ -316,6 +331,16 @@ CONFIG:
buildType: MinSizeRel
settings:
CONFIG: micoair_h743-aio_default
micoair_h743-v2_bootloader:
short: micoair_h743-v2_bootloader
buildType: MinSizeRel
settings:
CONFIG: micoair_h743-v2_bootloader
micoair_h743-v2_default:
short: micoair_h743-v2
buildType: MinSizeRel
settings:
CONFIG: micoair_h743-v2_default
modalai_fc-v1_default:
short: modalai_fc-v1
buildType: MinSizeRel
-1
View File
@@ -129,5 +129,4 @@
"yaml.schemas": {
"${workspaceFolder}/validation/module_schema.yaml": "${workspaceFolder}/src/modules/*/module.yaml"
},
"ros.distro": "humble"
}
Vendored
+2 -2
View File
@@ -235,9 +235,9 @@ pipeline {
sh('rm -f px4_msgs/srv/*.srv')
sh('rm -f px4_msgs/srv/versioned/*.srv')
sh('cp msg/*.msg px4_msgs/msg/')
sh('mkdir -p px4_msgs/msg/versioned && cp msg/versioned/*.msg px4_msgs/msg/versioned/')
sh('cp msg/versioned/*.msg px4_msgs/msg/ || true')
sh('cp srv/*.srv px4_msgs/srv/')
sh('mkdir -p px4_msgs/srv/versioned && cp srv/versioned/*.srv px4_msgs/srv/versioned/')
sh('cp srv/versioned/*.srv px4_msgs/srv/ || true')
sh('cd px4_msgs; git status; git add .; git commit -a -m "Update message definitions `date`" || true')
sh('cd px4_msgs; git push origin main || true')
sh('rm -rf px4_msgs')
-7
View File
@@ -73,13 +73,6 @@ menu "Toolchain"
help
relative path to the ROMFS root directory
config BOARD_ROOTFSDIR
string "Root directory"
depends on PLATFORM_POSIX
default "."
help
Configure the root directory in the file system for PX4 files
config BOARD_IO
string "IO board name"
default "px4_io-v2_default"
+42
View File
@@ -0,0 +1,42 @@
Maintainers
===========
See [the documentation on Maintainers](https://docs.px4.io/main/en/contribute/maintainers.html) to learn about the role of the maintainers and the process to become one.
**Active Maintainers**
| Name | Sector | GitHub | Chat | email
|-------------------------|--------|--------|------|----------------
| Lorenz Meier | Founder | [LorenzMeier][LorenzMeier] | | <lorenz@px4.io>
| Daniel Agar | Architecture | [dagar][dagar] | daniel_agar | <daniel@agar.ca>
| Beat Küng | Architecture | [bkueng][bkueng] | beatkueng | <beat-kueng@gmx.net>
| Ramón Roche | CI / Testing | [mrpollo][mrpollo] | rroche | <rroche@linuxfoundation.org>
| Mathieu Bresciani | State Estimation | [bresch][bresch] | mbresch |
| Paul Riseborough | State Estimation | [priseborough][priseborough] | |
| David Sidrane | RTOS / NuttX | [davids5][davids5] | david_s5 | <David.Sidrane@Nscdg.com>
| Jayoung Lim | Simulation | [Jaeyoung-Lim][Jaeyoung-Lim] | jaeyounglim. | <jalim@ethz.ch>
| Beniamino Pozzan | ROS 2 | [beniaminopozzan][beniaminopozzan] | beniaminopozzan | <beniamino.pozzan@gmail.com>
| Matthias Grob | Multirotor | [MaEtUgR][MaEtUgR] | maetugr |
| Silvan Fuhrer | Fixed-Wing / VTOL | [sfuhrer][sfuhrer] | sfuhrer |
| Christian Friedrich | Rover | [chfriedrich98][chfriedrich98] | christian982564 |
| Pedro Roque | Spacecraft | [Pedro-Roque][Pedro-Roque] | .pedroroque | <padr@kth.se>
**Documentation Maintainers**
| Name | GitHub | Chat | email
|------|--------|------|----------------------
| Hamish Willee | [hamishwillee][hamishwillee] | hamishwillee |
**Release Managers**
| Name | GitHub | Chat | email
|------|--------|------|----------------------
| Ramón Roche | [mrpollo][mrpollo] | rroche | <rroche@linuxfoundation.org>
| Daniel Agar | [dagar][dagar] | daniel_agar | <daniel@agar.ca>
**Retired Maintainers**
| Name | GitHub | Chat | email
|------|--------|------|----------------------
| | | |
+2 -5
View File
@@ -344,6 +344,7 @@ bootloaders_update: \
matek_h743-slim_bootloader \
micoair_h743_bootloader \
micoair_h743-aio_bootloader \
micoair_h743-v2_bootloader \
modalai_fc-v2_bootloader \
mro_ctrl-zero-classic_bootloader \
mro_ctrl-zero-h7_bootloader \
@@ -403,7 +404,7 @@ check_newlines:
# Testing
# --------------------------------------------------------------------
.PHONY: tests tests_coverage tests_mission tests_mission_coverage tests_offboard tests_avoidance
.PHONY: tests tests_coverage tests_mission tests_mission_coverage tests_offboard
.PHONY: rostest python_coverage
tests:
@@ -456,10 +457,6 @@ tests_offboard: rostest
@"$(SRC_DIR)"/test/rostest_px4_run.sh mavros_posix_tests_offboard_posctl.test
@"$(SRC_DIR)"/test/rostest_px4_run.sh mavros_posix_tests_offboard_rpyrt_ctl.test
tests_avoidance: rostest
@"$(SRC_DIR)"/test/rostest_avoidance_run.sh mavros_posix_test_avoidance.test
@"$(SRC_DIR)"/test/rostest_avoidance_run.sh mavros_posix_test_safe_landing.test
python_coverage:
@mkdir -p "$(SRC_DIR)"/build/python_coverage
@cd "$(SRC_DIR)"/build/python_coverage && cmake "$(SRC_DIR)" $(CMAKE_ARGS) -G"$(PX4_CMAKE_GENERATOR)" -DCONFIG=px4_sitl_default -DPYTHON_COVERAGE=ON
+11 -88
View File
@@ -17,17 +17,19 @@ PX4 is highly portable, OS-independent and supports Linux, NuttX and MacOS out o
* [VTOL](https://docs.px4.io/main/en/frames_vtol/)
* [Autogyro](https://docs.px4.io/main/en/frames_autogyro/)
* [Rover](https://docs.px4.io/main/en/frames_rover/)
* many more experimental types (Blimps, Boats, Submarines, High altitude balloons, etc)
* many more experimental types (Blimps, Boats, Submarines, High Altitude Balloons, Spacecraft, etc)
* Releases: [Downloads](https://github.com/PX4/PX4-Autopilot/releases)
## Releases
Release notes and supporting information for PX4 releases can be found on the [Developer Guide](https://docs.px4.io/main/en/releases/).
## Building a PX4 based drone, rover, boat or robot
The [PX4 User Guide](https://docs.px4.io/main/en/) explains how to assemble [supported vehicles](https://docs.px4.io/main/en/airframes/airframe_reference.html) and fly drones with PX4.
See the [forum and chat](https://docs.px4.io/main/en/#getting-help) if you need help!
The [PX4 User Guide](https://docs.px4.io/main/en/) explains how to assemble [supported vehicles](https://docs.px4.io/main/en/airframes/airframe_reference.html) and fly drones with PX4. See the [forum and chat](https://docs.px4.io/main/en/#getting-help) if you need help!
## Changing code and contributing
## Changing Code and Contributing
This [Developer Guide](https://docs.px4.io/main/en/development/development.html) is for software developers who want to modify the flight stack and middleware (e.g. to add new flight modes), hardware integrators who want to support new flight controller boards and peripherals, and anyone who wants to get PX4 working on a new (unsupported) airframe/vehicle.
@@ -35,7 +37,7 @@ Developers should read the [Guide for Contributions](https://docs.px4.io/main/en
See the [forum and chat](https://docs.px4.io/main/en/#getting-help) if you need help!
### Weekly Dev Call
## Weekly Dev Call
The PX4 Dev Team syncs up on a [weekly dev call](https://docs.px4.io/main/en/contribute/).
@@ -44,96 +46,17 @@ The PX4 Dev Team syncs up on a [weekly dev call](https://docs.px4.io/main/en/con
## Maintenance Team
Note: This is the source of truth for the active maintainers of PX4 ecosystem.
See the latest list of maintainers on [MAINTAINERS](MAINTAINERS.md) file at the root of the project.
| Sector | Maintainer |
|---|---|
| Founder | [Lorenz Meier](https://github.com/LorenzMeier) |
| Architecture | [Daniel Agar](https://github.com/dagar) / [Beat Küng](https://github.com/bkueng)|
| State Estimation | [Mathieu Bresciani](https://github.com/bresch) / [Paul Riseborough](https://github.com/priseborough) |
| OS/NuttX | [David Sidrane](https://github.com/davids5) |
| Drivers | [Daniel Agar](https://github.com/dagar) |
| Simulation | [Jaeyoung Lim](https://github.com/Jaeyoung-Lim) |
| ROS2 | [Beniamino Pozzan](https://github.com/beniaminopozzan) |
| Community QnA Call | [Ramon Roche](https://github.com/mrpollo) |
| [Documentation](https://docs.px4.io/main/en/) | [Hamish Willee](https://github.com/hamishwillee) |
| Vehicle Type | Maintainer |
|---|---|
| Multirotor | [Matthias Grob](https://github.com/MaEtUgR) |
| Fixed Wing | [Thomas Stastny](https://github.com/tstastny) |
| Hybrid VTOL | [Silvan Fuhrer](https://github.com/sfuhrer) |
| Rover | [Christian Friedrich](https://github.com/chfriedrich98) |
| Boat | x |
See also [maintainers list](https://px4.io/community/maintainers/) (px4.io) and the [contributors list](https://github.com/PX4/PX4-Autopilot/graphs/contributors) (Github). However it may be not up to date.
For the latest stats on contributors please see the latest stats for the Dronecode ecosystem in our project dashboard under [LFX Insights](https://insights.lfx.linuxfoundation.org/foundation/dronecode). For information on how to update your profile and affiliations please see the following support link on how to [Complete Your LFX Profile](https://docs.linuxfoundation.org/lfx/my-profile/complete-your-lfx-profile). Dronecode publishes a yearly snapshot of contributions and achievements on its [website under the Reports section](https://dronecode.org).
## Supported Hardware
Pixhawk standard boards and proprietary boards are shown below (discontinued boards aren't listed).
For the most up to date information, please visit [PX4 user Guide > Autopilot Hardware](https://docs.px4.io/main/en/flight_controller/).
### Pixhawk Standard Boards
These boards fully comply with Pixhawk Standard, and are maintained by the PX4-Autopilot maintainers and Dronecode team
* FMUv6X and FMUv6C
* [CUAV Pixahwk V6X (FMUv6X)](https://docs.px4.io/main/en/flight_controller/cuav_pixhawk_v6x.html)
* [Holybro Pixhawk 6X (FMUv6X)](https://docs.px4.io/main/en/flight_controller/pixhawk6x.html)
* [Holybro Pixhawk 6C (FMUv6C)](https://docs.px4.io/main/en/flight_controller/pixhawk6c.html)
* [Holybro Pix32 v6 (FMUv6C)](https://docs.px4.io/main/en/flight_controller/holybro_pix32_v6.html)
* FMUv5 and FMUv5X (STM32F7, 2019/20)
* [Pixhawk 4 (FMUv5)](https://docs.px4.io/main/en/flight_controller/pixhawk4.html)
* [Pixhawk 4 mini (FMUv5)](https://docs.px4.io/main/en/flight_controller/pixhawk4_mini.html)
* [CUAV V5+ (FMUv5)](https://docs.px4.io/main/en/flight_controller/cuav_v5_plus.html)
* [CUAV V5 nano (FMUv5)](https://docs.px4.io/main/en/flight_controller/cuav_v5_nano.html)
* [Auterion Skynode (FMUv5X)](https://docs.auterion.com/avionics/skynode)
* FMUv4 (STM32F4, 2015)
* [Pixracer](https://docs.px4.io/main/en/flight_controller/pixracer.html)
* [Pixhawk 3 Pro](https://docs.px4.io/main/en/flight_controller/pixhawk3_pro.html)
* FMUv3 (STM32F4, 2014)
* [Pixhawk 2](https://docs.px4.io/main/en/flight_controller/pixhawk-2.html)
* [Pixhawk Mini](https://docs.px4.io/main/en/flight_controller/pixhawk_mini.html)
* [CUAV Pixhack v3](https://docs.px4.io/main/en/flight_controller/pixhack_v3.html)
* FMUv2 (STM32F4, 2013)
* [Pixhawk](https://docs.px4.io/main/en/flight_controller/pixhawk.html)
### Manufacturer supported
These boards are maintained to be compatible with PX4-Autopilot by the Manufacturers.
* [ARK Electronics ARKV6X](https://docs.px4.io/main/en/flight_controller/ark_v6x.html)
* [CubePilot Cube Orange+](https://docs.px4.io/main/en/flight_controller/cubepilot_cube_orangeplus.html)
* [CubePilot Cube Orange](https://docs.px4.io/main/en/flight_controller/cubepilot_cube_orange.html)
* [CubePilot Cube Yellow](https://docs.px4.io/main/en/flight_controller/cubepilot_cube_yellow.html)
* [Holybro Durandal](https://docs.px4.io/main/en/flight_controller/durandal.html)
* [Airmind MindPX V2.8](http://www.mindpx.net/assets/accessories/UserGuide_MindPX.pdf)
* [Airmind MindRacer V1.2](http://mindpx.net/assets/accessories/mindracer_user_guide_v1.2.pdf)
* [Holybro Kakute F7](https://docs.px4.io/main/en/flight_controller/kakutef7.html)
### Community supported
These boards don't fully comply industry standards, and thus is solely maintained by the PX4 public community members.
### Experimental
These boards are not maintained by PX4 team nor Manufacturer, and is not guaranteed to be compatible with up to date PX4 releases.
* [Raspberry PI with Navio 2](https://docs.px4.io/main/en/flight_controller/raspberry_pi_navio2.html)
* [Bitcraze Crazyflie 2.0](https://docs.px4.io/main/en/complete_vehicles/crazyflie2.html)
## Project Roadmap
**Note: Outdated**
A high level project roadmap is available [here](https://github.com/orgs/PX4/projects/25).
For the most up to date information, please visit [PX4 User Guide > Autopilot Hardware](https://docs.px4.io/main/en/flight_controller/).
## Project Governance
The PX4 Autopilot project including all of its trademarks is hosted under [Dronecode](https://www.dronecode.org/), part of the Linux Foundation.
<a href="https://www.dronecode.org/" style="padding:20px" ><img src="https://mavlink.io/assets/site/logo_dronecode.png" alt="Dronecode Logo" width="110px"/></a>
<a href="https://www.linuxfoundation.org/projects" style="padding:20px;"><img src="https://mavlink.io/assets/site/logo_linux_foundation.png" alt="Linux Foundation Logo" width="80px" /></a>
<a href="https://www.dronecode.org/" style="padding:20px" ><img src="https://dronecode.org/wp-content/uploads/sites/24/2020/08/dronecode_logo_default-1.png" alt="Dronecode Logo" width="110px"/></a>
<div style="padding:10px">&nbsp;</div>
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
# Copyright (c) 2025 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -31,8 +31,4 @@
#
############################################################################
px4_add_library(RoverDifferentialGuidance
RoverDifferentialGuidance.cpp
)
target_include_directories(RoverDifferentialGuidance PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
add_subdirectory(init.d)
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2018 PX4 Development Team. All rights reserved.
# Copyright (c) 2025 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -31,9 +31,6 @@
#
############################################################################
px4_add_library(bezier
BezierQuad.cpp
BezierN.cpp
px4_add_romfs_files(
rcS
)
px4_add_unit_gtest(SRC BezierNTest.cpp LINKLIBS bezier)
+68
View File
@@ -0,0 +1,68 @@
#!/bin/sh
# Un comment and use set +e to ignore and set -e to enable 'exit on error control'
set +e
# Un comment the line below to help debug scripts by printing a trace of the script commands
#set -x
# PX4FMU startup script.
#
# NOTE: environment variable references:
# If the dollar sign ('$') is followed by a left bracket ('{') then the
# variable name is terminated with the right bracket character ('}').
# Otherwise, the variable name goes to the end of the argument.
#
#
# NOTE: COMMENT LINES ARE REMOVED BEFORE STORED IN ROMFS.
#
#------------------------------------------------------------------------------
set R /
#
# Print full system version.
#
ver all
#
# Set the parameter file the board supports params on
# MTD device.
#
if mft query -q -k MTD -s MTD_PARAMETERS -v /fs/mtd_params
then
set PARAM_FILE /fs/mtd_params
fi
#
# Load parameters.
#
# if the board has a storage for (factory) calibration data
if mft query -q -k MTD -s MTD_CALDATA -v /fs/mtd_caldata
then
param load /fs/mtd_caldata
fi
#
# Load parameters.
#
param select $PARAM_FILE
if ! param load
then
param reset_all
fi
#
# Try to mount the microSD card.
#
mount -t vfat /dev/mmcsd0 /fs/microsd
if [ $? = 0 ]
then
echo "SD card mounted at /fs/microsd"
else
echo "No SD card found"
fi
unset R
echo ""
echo "!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!"
echo "!!!!!! This is the PERFORMANCE TESTING firmware! WARNs and ERRORs are expected! !!!!!"
echo "!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!"
echo ""
@@ -16,10 +16,6 @@ param set-default SENS_EN_GPSSIM 1
param set-default SENS_EN_BAROSIM 1
param set-default SENS_EN_MAGSIM 1
# disable some checks to allow to fly:
# - without real battery
param set-default CBRK_SUPPLY_CHK 894281
# Square quadrotor X PX4 numbering
param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 1
@@ -16,12 +16,6 @@ param set-default SENS_EN_BAROSIM 1
param set-default SENS_EN_MAGSIM 1
param set-default SENS_EN_ARSPDSIM 1
# disable some checks to allow to fly:
# - with usb
param set-default CBRK_USB_CHK 197848
# - without real battery
param set-default CBRK_SUPPLY_CHK 894281
param set-default SIH_T_MAX 6
param set-default SIH_MASS 0.3
param set-default SIH_IXX 0.00402
@@ -33,18 +27,19 @@ param set-default SIH_KDV 0.2
param set-default SIH_VEHICLE_TYPE 1 # sih as fixed wing
param set-default RWTO_TKOFF 1 # enable takeoff from runway (as opposed to launched)
param set-default CA_AIRFRAME 1
param set-default CA_ROTOR_COUNT 1
param set-default CA_ROTOR0_PX 0.3
# SIH for now hardcodes this configuration which we need to match in the airframe files.
param set-default CA_SV_CS_COUNT 3
param set-default CA_SV_CS0_TRQ_R -0.5
param set-default CA_SV_CS0_TYPE 1
param set-default CA_SV_CS0_TRQ_R 1
param set-default CA_SV_CS0_TYPE 15 # single channel aileron
param set-default CA_SV_CS1_TRQ_P 1
param set-default CA_SV_CS1_TYPE 3
param set-default CA_SV_CS1_TYPE 3 # elevator
param set-default CA_SV_CS2_TRQ_Y 1
param set-default CA_SV_CS2_TYPE 4
param set-default CA_SV_CS2_TYPE 4 # rudder
param set-default PWM_MAIN_FUNC1 201
param set-default PWM_MAIN_FUNC2 202
param set-default PWM_MAIN_FUNC3 203
@@ -28,10 +28,6 @@ param set-default MC_PITCH_P 5
param set-default MAV_TYPE 19
# disable some checks to allow to fly:
# - without real battery
param set-default CBRK_SUPPLY_CHK 894281
param set-default SIH_T_MAX 2
param set-default SIH_Q_MAX 0.0165
param set-default SIH_MASS 0.2
@@ -0,0 +1,96 @@
#!/bin/sh
#
# @name SIH Standard VTOL
#
# @type Simulation
# @class VTOL
#
# @output Motor1 MC motor front right
# @output Motor2 MC motor back left
# @output Motor3 MC motor front left
# @output Motor4 MC motor back right
# @output Motor5 Forward thrust motor
# @output Servo1 Ailerons (single channel)
# @output Servo2 Elevator
# @output Servo3 Rudder
#
# @board px4_fmu-v2 exclude
#
. ${R}etc/init.d/rc.vtol_defaults
PX4_SIMULATOR=${PX4_SIMULATOR:=sihsim}
PX4_SIM_MODEL=${PX4_SIM_MODEL:=standard_vtol}
param set-default SENS_EN_GPSSIM 1
param set-default SENS_EN_BAROSIM 1
param set-default SENS_EN_MAGSIM 1
param set-default SENS_EN_ARSPDSIM 1
param set-default EKF2_GPS_DELAY 0
param set-default VT_TYPE 2
param set-default MPC_MAN_Y_MAX 60
param set-default MC_PITCH_P 5
param set-default CA_AIRFRAME 2
param set-default CA_ROTOR_COUNT 5
param set-default CA_ROTOR0_KM 0.05
param set-default CA_ROTOR0_PX 0.2
param set-default CA_ROTOR0_PY 0.2
param set-default CA_ROTOR1_KM 0.05
param set-default CA_ROTOR1_PX -0.2
param set-default CA_ROTOR1_PY -0.2
param set-default CA_ROTOR2_PX 0.2
param set-default CA_ROTOR2_PY -0.2
param set-default CA_ROTOR2_KM -0.05
param set-default CA_ROTOR3_PX -0.2
param set-default CA_ROTOR3_PY 0.2
param set-default CA_ROTOR3_KM -0.05
param set-default CA_ROTOR4_PX -0.3
param set-default CA_ROTOR4_KM 0.05
param set-default CA_ROTOR4_AX 1
param set-default CA_ROTOR4_AZ 0
# SIH for now hardcodes this configuration which we need to match in the airframe files.
param set-default CA_SV_CS_COUNT 3
param set-default CA_SV_CS0_TRQ_R 1
param set-default CA_SV_CS0_TYPE 15 # single channel aileron
param set-default CA_SV_CS1_TRQ_P 1
param set-default CA_SV_CS1_TYPE 3 # elevator
param set-default CA_SV_CS2_TRQ_Y 1
param set-default CA_SV_CS2_TYPE 4 # rudder
param set-default FW_AIRSPD_MIN 7
param set-default FW_AIRSPD_TRIM 10
param set-default FW_AIRSPD_MAX 12
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
param set-default PWM_MAIN_FUNC3 103
param set-default PWM_MAIN_FUNC4 104
param set-default PWM_MAIN_FUNC5 201
param set-default PWM_MAIN_FUNC6 202
param set-default PWM_MAIN_FUNC7 203
param set-default PWM_MAIN_FUNC8 105
param set-default MAV_TYPE 22
# set SYS_HITL to 2 to start the SIH and avoid sensors startup
# param set-default SYS_HITL 2
param set-default SENS_DPRES_OFF 0.001
param set SIH_T_MAX 2.0
param set SIH_Q_MAX 0.0165
param set SIH_MASS 0.2
# IXX and IZZ are inverted from the thesis as the body frame is pitched by 90 deg
param set SIH_IXX 0.00354
param set SIH_IYY 0.000625
param set SIH_IZZ 0.00300
param set SIH_IXZ 0
param set SIH_KDV 0.2
param set SIH_L_ROLL 0.2
# sih as standard vtol
param set SIH_VEHICLE_TYPE 3
@@ -1,32 +0,0 @@
#!/bin/sh
#
# @name 3DR Iris Quadrotor SITL (Obstacle Avoidance)
#
# @type Quadrotor Wide
#
. ${R}etc/init.d/rc.mc_defaults
param set-default CA_AIRFRAME 0
param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 0.1515
param set-default CA_ROTOR0_PY 0.245
param set-default CA_ROTOR0_KM 0.05
param set-default CA_ROTOR1_PX -0.1515
param set-default CA_ROTOR1_PY -0.1875
param set-default CA_ROTOR1_KM 0.05
param set-default CA_ROTOR2_PX 0.1515
param set-default CA_ROTOR2_PY -0.245
param set-default CA_ROTOR2_KM -0.05
param set-default CA_ROTOR3_PX -0.1515
param set-default CA_ROTOR3_PY 0.1875
param set-default CA_ROTOR3_KM -0.05
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
param set-default PWM_MAIN_FUNC3 103
param set-default PWM_MAIN_FUNC4 104
param set-default COM_OBS_AVOID 1
@@ -1,2 +0,0 @@
# shellcheck disable=SC2154
mavlink start -x -u 14558 -r 4000000 -m onboard -o 14541 -p # add mavlink stream for SDK
@@ -19,7 +19,6 @@ param set-default SENS_EN_BAROSIM 0
param set-default SENS_EN_MAGSIM 1
# Commander Parameters
param set-default COM_OBS_AVOID 0
param set-default COM_DISARM_LAND 0.5
# EKF2 parameters
@@ -11,29 +11,39 @@ PX4_SIM_MODEL=${PX4_SIM_MODEL:=r1_rover}
param set-default SIM_GZ_EN 1 # Gazebo bridge
# Rover parameters
param set-default NAV_ACC_RAD 0.5
# Differential Parameters
param set-default RD_WHEEL_TRACK 0.3
param set-default RD_MAX_ACCEL 5
param set-default RD_MAX_DECEL 10
param set-default RD_MAX_JERK 30
param set-default RD_MAX_THR_YAW_R 1.5
param set-default RD_YAW_RATE_P 0.25
param set-default RD_YAW_RATE_I 0.01
param set-default RD_YAW_P 5
param set-default RD_YAW_I 0.1
param set-default RD_MAX_SPEED 2
param set-default RD_MAX_THR_SPD 2.15
param set-default RD_SPEED_P 0.1
param set-default RD_SPEED_I 0.01
param set-default RD_MAX_YAW_RATE 180
param set-default RD_TRANS_DRV_TRN 0.349066
param set-default RD_TRANS_TRN_DRV 0.174533
param set-default RD_MAX_YAW_ACCEL 1000
# Pure pursuit parameters
param set-default PP_LOOKAHD_MAX 30
param set-default PP_LOOKAHD_MIN 2
# Rover Control Parameters
param set-default RO_ACCEL_LIM 5
param set-default RO_DECEL_LIM 10
param set-default RO_JERK_LIM 30
param set-default RO_MAX_THR_SPEED 2.1
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0.01
param set-default RO_YAW_RATE_P 0.25
param set-default RO_YAW_RATE_LIM 180
param set-default RO_YAW_ACCEL_LIM 120
param set-default RO_YAW_DECEL_LIM 1000
# Rover Attitude Control Parameters
param set-default RO_YAW_P 5
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 2
param set-default RO_SPEED_I 0.5
param set-default RO_SPEED_P 1
# Pure Pursuit parameters
param set-default PP_LOOKAHD_GAIN 1
param set-default PP_LOOKAHD_MAX 10
param set-default PP_LOOKAHD_MIN 1
# Simulated sensors
param set-default SENS_EN_GPSSIM 1
@@ -60,19 +60,25 @@ param set-default SIM_GZ_WH_REV 0 # no need to reverse any wheels
# controls in practical scenarios.
# Cutter deck blades clutch, PCA9685 servo channel 3, "RC FLAPS" (406) - leftmost switch, or "Servo 3" (203):
param set-default SIM_GZ_SV_FUNC3 203
param set-default SIM_GZ_SV_MIN3 0
param set-default SIM_GZ_SV_MAX3 1000
param set-default SIM_GZ_SV_DIS3 500
param set-default SIM_GZ_SV_FAIL3 500
param set-default SIM_GZ_SV_FUNC1 201
param set-default SIM_GZ_SV_MIN1 0
param set-default SIM_GZ_SV_MAX1 1000
param set-default SIM_GZ_SV_DIS1 500
param set-default SIM_GZ_SV_FAIL1 500
param set-default SIM_GZ_SV_MAXA1 90
param set-default SIM_GZ_SV_MINA1 -90
# Gas engine throttle, PCA9685 servo channel 4, "RC AUX1" (407) - left knob, or "Servo 4" (204):
# - on minimum when disarmed or failed:
param set-default SIM_GZ_SV_FUNC4 204
param set-default SIM_GZ_SV_MIN4 0
param set-default SIM_GZ_SV_MAX4 1000
param set-default SIM_GZ_SV_DIS4 500
param set-default SIM_GZ_SV_FAIL4 500
param set-default SIM_GZ_SV_FUNC2 202
param set-default SIM_GZ_SV_MIN2 0
param set-default SIM_GZ_SV_MAX2 1000
param set-default SIM_GZ_SV_DIS2 500
param set-default SIM_GZ_SV_FAIL2 500
param set-default SIM_GZ_SV_MAXA2 90
param set-default SIM_GZ_SV_MINA2 -90
param set-default CA_SV_CS_COUNT 2
# Controlling PCA9685 servos 5,6,7,8 directly via "Servo 5..8" setting, by publishing actuator_servos.control[]:
@@ -11,23 +11,33 @@ PX4_SIM_MODEL=${PX4_SIM_MODEL:=rover_ackermann}
param set-default SIM_GZ_EN 1 # Gazebo bridge
# Rover parameters
param set-default NAV_ACC_RAD 0.5
# Ackermann Parameters
param set-default RA_WHEEL_BASE 0.321
param set-default RA_ACC_RAD_GAIN 2
param set-default RA_ACC_RAD_MAX 3
param set-default RA_LAT_ACCEL_I 0.01
param set-default RA_LAT_ACCEL_P 0.1
param set-default RA_MAX_ACCEL 3
param set-default RA_MAX_DECEL 6
param set-default RA_MAX_JERK 15
param set-default RA_MAX_LAT_ACCEL 4
param set-default RA_MAX_SPEED 3
param set-default RA_MAX_STR_ANG 0.5236
param set-default RA_MAX_STR_RATE 360
param set-default RA_MAX_THR_SPEED 3.1
param set-default RA_SPEED_I 0.01
param set-default RA_SPEED_P 0.1
param set-default RA_WHEEL_BASE 0.321
param set-default RA_STR_RATE_LIM 360
# Rover Control Parameters
param set-default RO_ACCEL_LIM 3
param set-default RO_DECEL_LIM 6
param set-default RO_JERK_LIM 15
param set-default RO_MAX_THR_SPEED 3.1
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0.1
param set-default RO_YAW_RATE_P 1
param set-default RO_YAW_RATE_LIM 180
# Rover Attitude Control Parameters
param set-default RO_YAW_P 3
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 3
param set-default RO_SPEED_I 0.1
param set-default RO_SPEED_P 1
# Pure Pursuit parameters
param set-default PP_LOOKAHD_GAIN 1
@@ -47,5 +57,8 @@ param set-default SIM_GZ_WH_MAX1 200
param set-default SIM_GZ_WH_DIS1 100
# Steering
param set-default SIM_GZ_SV_MAXA1 30
param set-default SIM_GZ_SV_MINA1 -30
param set-default CA_SV_CS_COUNT 1
param set-default SIM_GZ_SV_FUNC1 201
param set-default SIM_GZ_SV_REV 1
@@ -11,28 +11,38 @@ PX4_SIM_MODEL=${PX4_SIM_MODEL:=r1_rover_mecanum}
param set-default SIM_GZ_EN 1 # Gazebo bridge
# Rover parameters
param set-default RM_WHEEL_TRACK 0.3
param set-default RM_YAW_RATE_I 0.1
param set-default RM_YAW_RATE_P 0.1
param set-default RM_MAX_ACCEL 3
param set-default RM_MAX_DECEL 5
param set-default RM_MAX_JERK 5
param set-default RM_MAX_SPEED 2
param set-default RM_MAX_THR_SPD 2.2
param set-default RM_MAX_THR_YAW_R 1.2
param set-default RM_YAW_P 5
param set-default RM_YAW_I 0.1
param set-default RM_MAX_YAW_RATE 120
param set-default RM_MAX_YAW_ACCEL 240
param set-default RM_MISS_VEL_GAIN 1
param set-default RM_SPEED_I 0.01
param set-default RM_SPEED_P 0.1
param set-default NAV_ACC_RAD 0.5
# Pure pursuit parameters
# Mecanum Parameters
param set-default RM_WHEEL_TRACK 0.3
param set-default RM_MAX_THR_YAW_R 1.2
param set-default RM_MISS_SPD_GAIN 1
# Rover Control Parameters
param set-default RO_ACCEL_LIM 3
param set-default RO_DECEL_LIM 5
param set-default RO_JERK_LIM 30
param set-default RO_MAX_THR_SPEED 2.1
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0.1
param set-default RO_YAW_RATE_P 0.1
param set-default RO_YAW_RATE_LIM 120
param set-default RO_YAW_ACCEL_LIM 240
param set-default RO_YAW_DECEL_LIM 1000
# Rover Attitude Control Parameters
param set-default RO_YAW_P 5
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 2
param set-default RO_SPEED_I 0.5
param set-default RO_SPEED_P 1
# Pure Pursuit parameters
param set-default PP_LOOKAHD_GAIN 0.5
param set-default PP_LOOKAHD_MAX 10
param set-default PP_LOOKAHD_MIN 1
param set-default PP_LOOKAHD_GAIN 0.5
# Simulated sensors
param set-default SENS_EN_GPSSIM 1
@@ -0,0 +1,23 @@
#!/bin/sh
#
# @name Gazebo x500 gimbal
#
# @type Quadrotor
#
PX4_SIM_MODEL=${PX4_SIM_MODEL:=x500_gimbal}
. ${R}etc/init.d-posix/airframes/4001_gz_x500
# Gimbal settings
param set-default MNT_MODE_IN 4
param set-default MNT_MODE_OUT 2
param set-default MNT_RC_IN_MODE 1
param set-default MNT_MAN_ROLL 1
param set-default MNT_MAN_PITCH 2
param set-default MNT_MAN_YAW 3
param set-default MNT_RANGE_ROLL 180
param set-default MNT_RANGE_PITCH 180
param set-default MNT_RANGE_YAW 720
@@ -0,0 +1,112 @@
#!/bin/sh
#
# @name VTOL Tiltrotor
#
# @type VTOL Tiltrotor
#
. ${R}etc/init.d/rc.vtol_defaults
PX4_SIMULATOR=${PX4_SIMULATOR:=gz}
PX4_GZ_WORLD=${PX4_GZ_WORLD:=default}
PX4_SIM_MODEL=${PX4_SIM_MODEL:=tiltrotor}
param set-default SIM_GZ_EN 1 # Gazebo bridge
param set-default SENS_EN_GPSSIM 1
param set-default SENS_EN_BAROSIM 0
param set-default SENS_EN_MAGSIM 1
param set-default SENS_EN_ARSPDSIM 0
param set-default MAV_TYPE 21
param set-default CA_AIRFRAME 3
param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 0.1515
param set-default CA_ROTOR0_PY 0.245
param set-default CA_ROTOR0_KM 0.05
param set-default CA_ROTOR1_PX -0.1515
param set-default CA_ROTOR1_PY -0.1875
param set-default CA_ROTOR1_KM 0.05
param set-default CA_ROTOR2_PX 0.1515
param set-default CA_ROTOR2_PY -0.245
param set-default CA_ROTOR2_KM -0.05
param set-default CA_ROTOR3_PX -0.1515
param set-default CA_ROTOR3_PY 0.1875
param set-default CA_ROTOR3_KM -0.05
param set-default CA_ROTOR0_TILT 1
param set-default CA_ROTOR2_TILT 2
param set-default CA_SV_TL0_MAXA 90
param set-default CA_SV_TL0_MINA 0
param set-default CA_SV_TL0_TD 0
param set-default CA_SV_TL0_CT 1
param set-default CA_SV_TL1_MAXA 90
param set-default CA_SV_TL1_MINA 0
param set-default CA_SV_TL1_TD 0
param set-default CA_SV_TL1_CT 1
param set-default CA_SV_CS0_TRQ_R -0.5
param set-default CA_SV_CS0_TYPE 1
param set-default CA_SV_CS1_TRQ_R 0.5
param set-default CA_SV_CS1_TYPE 2
param set-default CA_SV_CS2_TRQ_P 1
param set-default CA_SV_CS2_TYPE 3
param set-default CA_SV_CS_COUNT 3
param set-default CA_SV_TL_COUNT 2
param set-default SIM_GZ_EC_FUNC1 101
param set-default SIM_GZ_EC_FUNC2 102
param set-default SIM_GZ_EC_FUNC3 103
param set-default SIM_GZ_EC_FUNC4 104
param set-default SIM_GZ_EC_MIN1 10
param set-default SIM_GZ_EC_MIN2 10
param set-default SIM_GZ_EC_MIN3 10
param set-default SIM_GZ_EC_MIN4 10
param set-default SIM_GZ_EC_MAX1 1500
param set-default SIM_GZ_EC_MAX2 1500
param set-default SIM_GZ_EC_MAX3 1500
param set-default SIM_GZ_EC_MAX4 1500
param set-default SIM_GZ_SV_FUNC1 201
param set-default SIM_GZ_SV_FUNC2 202
param set-default SIM_GZ_SV_FUNC3 203
param set-default SIM_GZ_SV_FUNC4 204
param set-default SIM_GZ_SV_FUNC5 205
param set-default SIM_GZ_SV_MAXA4 90
param set-default SIM_GZ_SV_MINA4 0
param set-default SIM_GZ_SV_MAXA5 90
param set-default SIM_GZ_SV_MINA5 0
param set-default NPFG_PERIOD 12
param set-default FW_PR_FF 0.2
param set-default FW_PR_P 0.9
param set-default FW_PSP_OFF 2
param set-default FW_P_LIM_MIN -15
param set-default FW_RR_FF 0.1
param set-default FW_RR_P 0.3
param set-default FW_THR_TRIM 0.38
param set-default FW_THR_MAX 0.6
param set-default FW_THR_MIN 0.05
param set-default FW_T_CLMB_MAX 8
param set-default FW_T_SINK_MAX 2.7
param set-default FW_T_SINK_MIN 2.2
param set-default MC_AIRMODE 1
param set-default MC_YAWRATE_P 0.4
param set-default MC_YAWRATE_I 0.1
param set-default MPC_XY_VEL_P_ACC 3
param set-default MPC_XY_VEL_I_ACC 4
param set-default MPC_XY_VEL_D_ACC 0.1
param set-default MIS_TAKEOFF_ALT 10
param set-default VT_FWD_THRUST_EN 4
param set-default VT_FWD_THRUST_SC 0.6
param set-default VT_TILT_TRANS 0.6
param set-default VT_TYPE 1
@@ -0,0 +1,155 @@
#!/bin/sh
#
# @name 6DoF Spacecraft Model
#
# @type Freeflyer with 8 thrusters
#
# @maintainer Pedro Roque <padr@kth.se>
#
. ${R}etc/init.d/rc.sc_defaults
param set-default CA_AIRFRAME 15
param set-default MAV_TYPE 99
param set-default CA_THRUSTER_CNT 12
param set-default CA_R_REV 0
# param set-default FW_ARSP_MODE 1
# Auto to be provided by Custom Airframe
param set-default CA_METHOD 0
# disable attitude failure detection
param set-default FD_FAIL_P 0
param set-default FD_FAIL_R 0
# Set proper failsafes
param set-default COM_ACT_FAIL_ACT 0
param set-default COM_LOW_BAT_ACT 0
param set-default NAV_DLL_ACT 0
param set-default GF_ACTION 1
param set-default NAV_RCL_ACT 1
param set-default COM_POSCTL_NAVL 2
# Set thrusters
param set-default CA_THRUSTER0_PX -0.50
param set-default CA_THRUSTER0_PY 0.50
param set-default CA_THRUSTER0_PZ 0.0
param set-default CA_THRUSTER0_CT 0.237
param set-default CA_THRUSTER0_AX 0.0
param set-default CA_THRUSTER0_AY -1.0
param set-default CA_THRUSTER0_AZ 0.0
param set-default CA_THRUSTER1_PX 0.50
param set-default CA_THRUSTER1_PY 0.50
param set-default CA_THRUSTER1_PZ 0.0
param set-default CA_THRUSTER1_CT 0.237
param set-default CA_THRUSTER1_AX 0.0
param set-default CA_THRUSTER1_AY -1.0
param set-default CA_THRUSTER1_AZ 0.0
param set-default CA_THRUSTER2_PX 0.50
param set-default CA_THRUSTER2_PY -0.50
param set-default CA_THRUSTER2_PZ 0.0
param set-default CA_THRUSTER2_CT 0.237
param set-default CA_THRUSTER2_AX 0.0
param set-default CA_THRUSTER2_AY 1.0
param set-default CA_THRUSTER2_AZ 0.0
param set-default CA_THRUSTER3_PX -0.50
param set-default CA_THRUSTER3_PY -0.50
param set-default CA_THRUSTER3_PZ 0.0
param set-default CA_THRUSTER3_CT 0.237
param set-default CA_THRUSTER3_AX 0.0
param set-default CA_THRUSTER3_AY 1.0
param set-default CA_THRUSTER3_AZ 0.0
param set-default CA_THRUSTER4_PX -0.50
param set-default CA_THRUSTER4_PY 0.0
param set-default CA_THRUSTER4_PZ -0.50
param set-default CA_THRUSTER4_CT 0.237
param set-default CA_THRUSTER4_AX 1.0
param set-default CA_THRUSTER4_AY 0.0
param set-default CA_THRUSTER4_AZ 0.0
param set-default CA_THRUSTER5_PX 0.50
param set-default CA_THRUSTER5_PY 0.0
param set-default CA_THRUSTER5_PZ -0.50
param set-default CA_THRUSTER5_CT 0.237
param set-default CA_THRUSTER5_AX -1.0
param set-default CA_THRUSTER5_AY 0.0
param set-default CA_THRUSTER5_AZ 0.0
param set-default CA_THRUSTER6_PX 0.50
param set-default CA_THRUSTER6_PY 0.0
param set-default CA_THRUSTER6_PZ 0.50
param set-default CA_THRUSTER6_CT 0.237
param set-default CA_THRUSTER6_AX -1.0
param set-default CA_THRUSTER6_AY 0.0
param set-default CA_THRUSTER6_AZ 0.0
param set-default CA_THRUSTER7_PX -0.50
param set-default CA_THRUSTER7_PY 0.0
param set-default CA_THRUSTER7_PZ 0.50
param set-default CA_THRUSTER7_CT 0.237
param set-default CA_THRUSTER7_AX 1.0
param set-default CA_THRUSTER7_AY 0.0
param set-default CA_THRUSTER7_AZ 0.0
param set-default CA_THRUSTER8_PX 0.0
param set-default CA_THRUSTER8_PY -0.50
param set-default CA_THRUSTER8_PZ -0.50
param set-default CA_THRUSTER8_CT 0.237
param set-default CA_THRUSTER8_AX 0.0
param set-default CA_THRUSTER8_AY 0.0
param set-default CA_THRUSTER8_AZ 1.0
param set-default CA_THRUSTER9_PX 0.0
param set-default CA_THRUSTER9_PY 0.50
param set-default CA_THRUSTER9_PZ -0.50
param set-default CA_THRUSTER9_CT 0.237
param set-default CA_THRUSTER9_AX 0.0
param set-default CA_THRUSTER9_AY 0.0
param set-default CA_THRUSTER9_AZ 1.0
param set-default CA_THRUSTER10_PX 0.0
param set-default CA_THRUSTER10_PY 0.50
param set-default CA_THRUSTER10_PZ 0.50
param set-default CA_THRUSTER10_CT 0.237
param set-default CA_THRUSTER10_AX 0.0
param set-default CA_THRUSTER10_AY 0.0
param set-default CA_THRUSTER10_AZ -1.0
param set-default CA_THRUSTER11_PX 0.0
param set-default CA_THRUSTER11_PY -0.50
param set-default CA_THRUSTER11_PZ 0.50
param set-default CA_THRUSTER11_CT 0.237
param set-default CA_THRUSTER11_AX 0.0
param set-default CA_THRUSTER11_AY 0.0
param set-default CA_THRUSTER11_AZ -1.0
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
param set-default PWM_MAIN_FUNC3 103
param set-default PWM_MAIN_FUNC4 104
param set-default PWM_MAIN_FUNC5 105
param set-default PWM_MAIN_FUNC6 106
param set-default PWM_MAIN_FUNC7 107
param set-default PWM_MAIN_FUNC8 108
param set-default PWM_MAIN_FUNC9 109
param set-default PWM_MAIN_FUNC10 110
param set-default PWM_MAIN_FUNC11 111
param set-default PWM_MAIN_FUNC12 112
# PWM Simulation
param set PWM_SIM_PWM_MAX 10000
param set PWM_SIM_PWM_MIN 0
# Controller Tunings
param set-default SC_ROLLRATE_P 0.14
param set-default SC_PITCHRATE_P 0.14
param set-default SC_ROLLRATE_I 0.3
param set-default SC_PITCHRATE_I 0.3
param set-default SC_ROLLRATE_D 0.004
param set-default SC_PITCHRATE_D 0.004
@@ -0,0 +1,149 @@
#!/bin/sh
#
# @name 3DoF Spacecraft Model
#
# @type 2D Freeflyer with 8 thrusters - Planar motion
#
# @maintainer Pedro Roque <padr@kth.se>
#
. ${R}etc/init.d/rc.sc_defaults
PX4_SIMULATOR=${PX4_SIMULATOR:=gz}
PX4_GZ_WORLD=${PX4_GZ_WORLD:=default}
PX4_SIM_MODEL=${PX4_SIM_MODEL:=spacecraft_2d}
param set-default SIM_GZ_EN 1
param set-default SENS_EN_GPSSIM 1
param set-default SENS_EN_BAROSIM 1
param set-default SENS_EN_MAGSIM 1
param set-default COM_ARM_CHK_ESCS 0 # We don't have ESCs
param set-default FD_ESCS_EN 0 # We don't have ESCs - but maybe we need this later?
param set-default CA_AIRFRAME 14
param set-default MAV_TYPE 99
param set-default CA_THRUSTER_CNT 8
param set-default CA_R_REV 0
# param set-default FW_ARSP_MODE 1
# Auto to be provided by Custom Airframe
param set-default CA_METHOD 0 # 0 is PseudoInverse, 3 is Metric
# Set proper failsafes
param set-default COM_ACT_FAIL_ACT 0
param set-default COM_LOW_BAT_ACT 0
param set-default NAV_DLL_ACT 0
param set-default GF_ACTION 1
param set-default NAV_RCL_ACT 1
param set-default COM_POSCTL_NAVL 2
# disable attitude failure detection
param set-default FD_FAIL_P 0
param set-default FD_FAIL_R 0
param set-default CA_THRUSTER0_PX -0.12
param set-default CA_THRUSTER0_PY -0.12
param set-default CA_THRUSTER0_PZ 0.0
param set-default CA_THRUSTER0_CT 1.4
param set-default CA_THRUSTER0_AX 1.0
param set-default CA_THRUSTER0_AY 0.0
param set-default CA_THRUSTER0_AZ 0.0
param set-default CA_THRUSTER1_PX 0.12
param set-default CA_THRUSTER1_PY -0.12
param set-default CA_THRUSTER1_PZ 0.0
param set-default CA_THRUSTER1_CT 1.4
param set-default CA_THRUSTER1_AX -1.0
param set-default CA_THRUSTER1_AY 0.0
param set-default CA_THRUSTER1_AZ 0.0
param set-default CA_THRUSTER2_PX -0.12
param set-default CA_THRUSTER2_PY 0.12
param set-default CA_THRUSTER2_PZ 0.0
param set-default CA_THRUSTER2_CT 1.4
param set-default CA_THRUSTER2_AX 1.0
param set-default CA_THRUSTER2_AY 0.0
param set-default CA_THRUSTER2_AZ 0.0
param set-default CA_THRUSTER3_PX 0.12
param set-default CA_THRUSTER3_PY 0.12
param set-default CA_THRUSTER3_PZ 0.0
param set-default CA_THRUSTER3_CT 1.4
param set-default CA_THRUSTER3_AX -1.0
param set-default CA_THRUSTER3_AY 0.0
param set-default CA_THRUSTER3_AZ 0.0
param set-default CA_THRUSTER4_PX 0.12
param set-default CA_THRUSTER4_PY -0.12
param set-default CA_THRUSTER4_PZ 0.0
param set-default CA_THRUSTER4_CT 1.4
param set-default CA_THRUSTER4_AX 0.0
param set-default CA_THRUSTER4_AY 1.0
param set-default CA_THRUSTER4_AZ 0.0
param set-default CA_THRUSTER5_PX 0.12
param set-default CA_THRUSTER5_PY 0.12
param set-default CA_THRUSTER5_PZ 0.0
param set-default CA_THRUSTER5_CT 1.4
param set-default CA_THRUSTER5_AX 0.0
param set-default CA_THRUSTER5_AY -1.0
param set-default CA_THRUSTER5_AZ 0.0
param set-default CA_THRUSTER6_PX -0.12
param set-default CA_THRUSTER6_PY -0.12
param set-default CA_THRUSTER6_PZ 0.0
param set-default CA_THRUSTER6_CT 1.4
param set-default CA_THRUSTER6_AX 0.0
param set-default CA_THRUSTER6_AY 1.0
param set-default CA_THRUSTER6_AZ 0.0
param set-default CA_THRUSTER7_PX -0.12
param set-default CA_THRUSTER7_PY 0.12
param set-default CA_THRUSTER7_PZ 0.0
param set-default CA_THRUSTER7_CT 1.4
param set-default CA_THRUSTER7_AX 0.0
param set-default CA_THRUSTER7_AY -1.0
param set-default CA_THRUSTER7_AZ 0.0
param set-default SIM_GZ_TH_FUNC1 101
param set-default SIM_GZ_TH_FUNC2 102
param set-default SIM_GZ_TH_FUNC3 103
param set-default SIM_GZ_TH_FUNC4 104
param set-default SIM_GZ_TH_FUNC5 105
param set-default SIM_GZ_TH_FUNC6 106
param set-default SIM_GZ_TH_FUNC7 107
param set-default SIM_GZ_TH_FUNC8 108
param set-default SIM_GZ_TH_MIN1 0
param set-default SIM_GZ_TH_MIN2 0
param set-default SIM_GZ_TH_MIN3 0
param set-default SIM_GZ_TH_MIN4 0
param set-default SIM_GZ_TH_MIN5 0
param set-default SIM_GZ_TH_MIN6 0
param set-default SIM_GZ_TH_MIN7 0
param set-default SIM_GZ_TH_MIN8 0
param set-default SIM_GZ_TH_MAX1 10000
param set-default SIM_GZ_TH_MAX2 10000
param set-default SIM_GZ_TH_MAX3 10000
param set-default SIM_GZ_TH_MAX4 10000
param set-default SIM_GZ_TH_MAX5 10000
param set-default SIM_GZ_TH_MAX6 10000
param set-default SIM_GZ_TH_MAX7 10000
param set-default SIM_GZ_TH_MAX8 10000
# Controller Tunings
param set SC_YAWRATE_P 3.335
param set SC_YAWRATE_I 0.87
param set SC_YAWRATE_D 0.15
param set SC_YR_INT_LIM 0.2
param set SC_YAW_P 3.0
param set SPC_POS_P 0.20
param set SPC_VEL_P 6.55
param set SPC_VEL_I 0.0
param set SPC_VEL_D 0.0
param set SPC_VEL_MAX 12.0
@@ -39,8 +39,6 @@ px4_add_romfs_files(
1012_gazebo-classic_iris_rplidar
1013_gazebo-classic_iris_vision
1013_gazebo-classic_iris_vision.post
1014_gazebo-classic_iris_obs_avoid
1014_gazebo-classic_iris_obs_avoid.post
1015_gazebo-classic_iris_depth_camera
1016_gazebo-classic_iris_downward_depth_camera
1017_gazebo-classic_iris_opt_flow_mockup
@@ -91,6 +89,8 @@ px4_add_romfs_files(
4016_gz_x500_lidar_down
4017_gz_x500_lidar_front
4018_gz_quadtailsitter
4019_gz_x500_gimbal
4020_gz_tiltrotor
6011_gazebo-classic_typhoon_h480
6011_gazebo-classic_typhoon_h480.post
@@ -107,9 +107,13 @@ px4_add_romfs_files(
10040_sihsim_quadx
10041_sihsim_airplane
10042_sihsim_xvert
10043_sihsim_standard_vtol
17001_flightgear_tf-g1
17002_flightgear_tf-g2
71001_gazebo-classic_spacecraft_dart
71002_gz_spacecraft_2d
# [22000, 22999] Reserve for custom models
)
@@ -4,6 +4,9 @@
# Simulator IMU data provided at 250 Hz
param set-default IMU_INTEG_RATE 250
# For simulation, allow registering modes while armed for developer convenience
param set-default COM_MODE_ARM_CHK 1
if [ "$PX4_SIMULATOR" = "sihsim" ] || [ "$(param show -q SYS_AUTOSTART)" -eq "0" ]; then
echo "INFO [init] SIH simulator"
+7 -2
View File
@@ -153,8 +153,6 @@ fi
param set-default BAT1_N_CELLS 4
param set-default CBRK_SUPPLY_CHK 894281
# disable check, no CPU load reported on posix yet
param set-default COM_CPU_MAX -1
param set-default COM_RAM_MAX -1
@@ -247,6 +245,8 @@ then
battery_simulator start
fi
system_power_simulator start
tone_alarm start
rc_update start
manual_control start
@@ -337,6 +337,11 @@ then
payload_deliverer start
fi
if param compare -s ICE_EN 1
then
internal_combustion_engine_control start
fi
#user defined mavlink streams for instances can be in PATH
. px4-rc.mavlink
@@ -92,6 +92,13 @@ if(CONFIG_MODULES_ROVER_ACKERMANN)
)
endif()
if(CONFIG_MODULES_SPACECRAFT)
px4_add_romfs_files(
rc.sc_apps
rc.sc_defaults
)
endif()
if(CONFIG_MODULES_ROVER_MECANUM)
px4_add_romfs_files(
rc.rover_mecanum_apps
@@ -5,6 +5,15 @@
# @type Standard VTOL
# @class VTOL
#
# @output Motor1 MC motor front right
# @output Motor2 MC motor back left
# @output Motor3 MC motor front left
# @output Motor4 MC motor back right
# @output Motor5 Forward thrust motor
# @output Servo1 Aileron
# @output Servo2 Elevator
# @output Servo3 Rudder
#
# @maintainer Roman Bapst <roman@auterion.com>
#
# @board px4_fmu-v2 exclude
@@ -17,15 +17,16 @@ param set UAVCAN_ENABLE 0
param set-default CA_AIRFRAME 1
param set-default CA_ROTOR_COUNT 1
param set-default CA_ROTOR0_PX 0.3
param set-default CA_SV_CS_COUNT 3
param set-default CA_SV_CS0_TRQ_R -0.5
param set-default CA_SV_CS0_TYPE 1
param set-default CA_SV_CS1_TRQ_P 1
param set-default CA_SV_CS1_TYPE 3
param set-default CA_SV_CS2_TRQ_Y 1
param set-default CA_SV_CS2_TYPE 4
param set HIL_ACT_REV 1
# SIH for now hardcodes this configuration which we need to match in the airframe files.
param set-default CA_SV_CS_COUNT 3
param set-default CA_SV_CS0_TRQ_R 1
param set-default CA_SV_CS0_TYPE 15 # single channel aileron
param set-default CA_SV_CS1_TRQ_P 1
param set-default CA_SV_CS1_TYPE 3 # elevator
param set-default CA_SV_CS2_TRQ_Y 1
param set-default CA_SV_CS2_TYPE 4 # rudder
param set HIL_ACT_FUNC1 201
param set HIL_ACT_FUNC2 202
param set HIL_ACT_FUNC3 203
@@ -0,0 +1,92 @@
#!/bin/sh
#
# @name SIH Standard VTOL QuadPlane
#
# @type Simulation
# @class VTOL
#
# @output Motor1 MC motor front right
# @output Motor2 MC motor back left
# @output Motor3 MC motor front left
# @output Motor4 MC motor back right
# @output Motor5 Forward thrust motor
# @output Servo1 Ailerons (single channel)
# @output Servo2 Elevator
# @output Servo3 Rudder
#
# @board px4_fmu-v2 exclude
#
. ${R}etc/init.d/rc.vtol_defaults
param set UAVCAN_ENABLE 0
param set-default VT_TYPE 2
param set-default MPC_MAN_Y_MAX 60
param set-default MC_PITCH_P 5
param set-default CA_AIRFRAME 2
param set-default CA_ROTOR_COUNT 5
param set-default CA_ROTOR0_KM 0.05
param set-default CA_ROTOR0_PX 0.2
param set-default CA_ROTOR0_PY 0.2
param set-default CA_ROTOR1_KM 0.05
param set-default CA_ROTOR1_PX -0.2
param set-default CA_ROTOR1_PY -0.2
param set-default CA_ROTOR2_PX 0.2
param set-default CA_ROTOR2_PY -0.2
param set-default CA_ROTOR2_KM -0.05
param set-default CA_ROTOR3_PX -0.2
param set-default CA_ROTOR3_PY 0.2
param set-default CA_ROTOR3_KM -0.05
param set-default CA_ROTOR4_PX -0.3
param set-default CA_ROTOR4_KM 0.05
param set-default CA_ROTOR4_AX 1
param set-default CA_ROTOR4_AZ 0
# SIH for now hardcodes this configuration which we need to match in the airframe files.
param set-default CA_SV_CS_COUNT 3
param set-default CA_SV_CS0_TRQ_R 1
param set-default CA_SV_CS0_TYPE 15 # single channel aileron
param set-default CA_SV_CS1_TRQ_P 1
param set-default CA_SV_CS1_TYPE 3 # elevator
param set-default CA_SV_CS2_TRQ_Y 1
param set-default CA_SV_CS2_TYPE 4 # rudder
param set-default FW_AIRSPD_MIN 7
param set-default FW_AIRSPD_TRIM 10
param set-default FW_AIRSPD_MAX 12
param set-default HIL_ACT_FUNC1 101
param set-default HIL_ACT_FUNC2 102
param set-default HIL_ACT_FUNC3 103
param set-default HIL_ACT_FUNC4 104
param set-default HIL_ACT_FUNC5 201
param set-default HIL_ACT_FUNC6 202
param set-default HIL_ACT_FUNC7 203
param set-default HIL_ACT_FUNC8 105
param set-default MAV_TYPE 22
# set SYS_HITL to 2 to start the SIH and avoid sensors startup
param set-default SYS_HITL 2
# disable some checks to allow to fly:
# - without real battery
param set-default CBRK_SUPPLY_CHK 894281
param set-default SENS_DPRES_OFF 0.001
param set SIH_T_MAX 2.0
param set SIH_Q_MAX 0.0165
param set SIH_MASS 0.2
# IXX and IZZ are inverted from the thesis as the body frame is pitched by 90 deg
param set SIH_IXX 0.00354
param set SIH_IYY 0.000625
param set SIH_IZZ 0.00300
param set SIH_IXZ 0
param set SIH_KDV 0.2
param set SIH_L_ROLL 0.2
# sih as standard vtol
param set SIH_VEHICLE_TYPE 3
@@ -12,7 +12,6 @@
. ${R}etc/init.d/rc.mc_defaults
# Commander Parameters
param set-default COM_OBS_AVOID 1
param set-default COM_DISARM_LAND 0.5
# EKF2 parameters
@@ -12,7 +12,6 @@
. ${R}etc/init.d/rc.mc_defaults
# Commander Parameters
param set-default COM_OBS_AVOID 1
param set-default COM_DISARM_LAND 0.5
# EKF2 parameters
@@ -21,26 +21,37 @@ param set-default RBCLW_FUNC1 101
param set-default RBCLW_FUNC2 102
param set-default RBCLW_REV 1 # reverse right wheels
# Rover parameters
param set-default NAV_ACC_RAD 0.5
# Differential Parameters
param set-default RD_WHEEL_TRACK 0.3
param set-default RD_MAX_ACCEL 3
param set-default RD_MAX_DECEL 4
param set-default RD_MAX_JERK 5
param set-default RD_MAX_SPEED 1.6
param set-default RD_MAX_THR_SPD 1.9
param set-default RD_MAX_THR_YAW_R 0.7
param set-default RD_MAX_YAW_ACCEL 600
param set-default RD_MAX_YAW_RATE 250
param set-default RD_SPEED_P 0.1
param set-default RD_SPEED_I 0.01
param set-default RD_TRANS_DRV_TRN 0.785398
param set-default RD_TRANS_TRN_DRV 0.139626
param set-default RD_YAW_P 5
param set-default RD_YAW_I 0.1
param set-default RD_YAW_RATE_P 0.1
param set-default RD_YAW_RATE_I 0.01
# Pure pursuit parameters
# Rover Control Parameters
param set-default RO_ACCEL_LIM 3
param set-default RO_DECEL_LIM 4
param set-default RO_JERK_LIM 5
param set-default RO_MAX_THR_SPEED 1.9
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0.01
param set-default RO_YAW_RATE_P 0.1
param set-default RO_YAW_RATE_LIM 250
param set-default RO_YAW_ACCEL_LIM 600
param set-default RO_YAW_DECEL_LIM 600
# Rover Attitude Control Parameters
param set-default RO_YAW_P 5
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 1.6
param set-default RO_SPEED_I 0.01
param set-default RO_SPEED_P 0.1
# Pure Pursuit parameters
param set-default PP_LOOKAHD_GAIN 1
param set-default PP_LOOKAHD_MAX 10
param set-default PP_LOOKAHD_MIN 1
param set-default PP_LOOKAHD_GAIN 1
@@ -14,24 +14,33 @@
. ${R}etc/init.d/rc.rover_ackermann_defaults
param set-default BAT1_N_CELLS 3
# Rover parameters
param set-default NAV_ACC_RAD 0.5
# Ackermann Parameters
param set-default RA_WHEEL_BASE 0.321
param set-default RA_ACC_RAD_GAIN 2
param set-default RA_ACC_RAD_MAX 3
param set-default RA_LAT_ACCEL_I 0.01
param set-default RA_LAT_ACCEL_P 0.1
param set-default RA_MAX_ACCEL 1.5
param set-default RA_MAX_DECEL 10
param set-default RA_MAX_JERK 20
param set-default RA_MAX_LAT_ACCEL 3
param set-default RA_MAX_SPEED 2.5
param set-default RA_MAX_STR_ANG 0.5236
param set-default RA_MAX_STR_RATE 270
param set-default RA_MAX_THR_SPEED 2.8
param set-default RA_SPEED_I 0.01
param set-default RA_SPEED_P 0.1
param set-default RA_WHEEL_BASE 0.321
param set-default RA_STR_RATE_LIM 270
# Rover Control Parameters
param set-default RO_ACCEL_LIM 1.5
param set-default RO_DECEL_LIM 10
param set-default RO_JERK_LIM 20
param set-default RO_MAX_THR_SPEED 2.8
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0
param set-default RO_YAW_RATE_P 0
param set-default RO_YAW_RATE_LIM 0
# Rover Attitude Control Parameters
param set-default RO_YAW_P 0
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 2.5
param set-default RO_SPEED_I 0.01
param set-default RO_SPEED_P 0.1
# Pure pursuit parameters
param set-default PP_LOOKAHD_GAIN 1
@@ -0,0 +1,150 @@
#!/bin/sh
#
# @name KTH Space Robot
#
# @type Space Robot
# @class 2D Space Robot
#
# @maintainer DISCOWER
#
. ${R}etc/init.d/rc.sc_defaults
param set-default CA_AIRFRAME 14
param set-default MAV_TYPE 99
param set-default CA_THRUSTER_CNT 8
param set-default CA_R_REV 0
# Auto to be provided by Custom Airframe
param set-default CA_METHOD 0
# Set proper failsafes
param set-default COM_ACT_FAIL_ACT 0
param set-default COM_LOW_BAT_ACT 0
param set-default NAV_DLL_ACT 0
param set-default GF_ACTION 1
param set-default NAV_RCL_ACT 1
param set-default COM_POSCTL_NAVL 2
# Set Mocap Vision frame
param set EKF2_EV_CTRL 15
param set EKF2_HGT_REF 3
# disable attitude failure detection
param set-default FD_FAIL_P 0
param set-default FD_FAIL_R 0
param set-default CA_THRUSTER0_PX -0.12
param set-default CA_THRUSTER0_PY -0.12
param set-default CA_THRUSTER0_PZ 0.0
param set-default CA_THRUSTER0_CT 1.4
param set-default CA_THRUSTER0_AX 1.0
param set-default CA_THRUSTER0_AY 0.0
param set-default CA_THRUSTER0_AZ 0.0
param set-default CA_THRUSTER1_PX 0.12
param set-default CA_THRUSTER1_PY -0.12
param set-default CA_THRUSTER1_PZ 0.0
param set-default CA_THRUSTER1_CT 1.4
param set-default CA_THRUSTER1_AX -1.0
param set-default CA_THRUSTER1_AY 0.0
param set-default CA_THRUSTER1_AZ 0.0
param set-default CA_THRUSTER2_PX -0.12
param set-default CA_THRUSTER2_PY 0.12
param set-default CA_THRUSTER2_PZ 0.0
param set-default CA_THRUSTER2_CT 1.4
param set-default CA_THRUSTER2_AX 1.0
param set-default CA_THRUSTER2_AY 0.0
param set-default CA_THRUSTER2_AZ 0.0
param set-default CA_THRUSTER3_PX 0.12
param set-default CA_THRUSTER3_PY 0.12
param set-default CA_THRUSTER3_PZ 0.0
param set-default CA_THRUSTER3_CT 1.4
param set-default CA_THRUSTER3_AX -1.0
param set-default CA_THRUSTER3_AY 0.0
param set-default CA_THRUSTER3_AZ 0.0
param set-default CA_THRUSTER4_PX 0.12
param set-default CA_THRUSTER4_PY -0.12
param set-default CA_THRUSTER4_PZ 0.0
param set-default CA_THRUSTER4_CT 1.4
param set-default CA_THRUSTER4_AX 0.0
param set-default CA_THRUSTER4_AY 1.0
param set-default CA_THRUSTER4_AZ 0.0
param set-default CA_THRUSTER5_PX 0.12
param set-default CA_THRUSTER5_PY 0.12
param set-default CA_THRUSTER5_PZ 0.0
param set-default CA_THRUSTER5_CT 1.4
param set-default CA_THRUSTER5_AX 0.0
param set-default CA_THRUSTER5_AY -1.0
param set-default CA_THRUSTER5_AZ 0.0
param set-default CA_THRUSTER6_PX -0.12
param set-default CA_THRUSTER6_PY -0.12
param set-default CA_THRUSTER6_PZ 0.0
param set-default CA_THRUSTER6_CT 1.4
param set-default CA_THRUSTER6_AX 0.0
param set-default CA_THRUSTER6_AY 1.0
param set-default CA_THRUSTER6_AZ 0.0
param set-default CA_THRUSTER7_PX -0.12
param set-default CA_THRUSTER7_PY 0.12
param set-default CA_THRUSTER7_PZ 0.0
param set-default CA_THRUSTER7_CT 1.4
param set-default CA_THRUSTER7_AX 0.0
param set-default CA_THRUSTER7_AY -1.0
param set-default CA_THRUSTER7_AZ 0.0
param set-default PWM_AUX_TIM0 10
param set-default PWM_AUX_TIM1 10
param set-default PWM_AUX_TIM2 10
param set-default PWM_AUX_FUNC1 101
param set-default PWM_AUX_FUNC2 102
param set-default PWM_AUX_FUNC3 103
param set-default PWM_AUX_FUNC4 104
param set-default PWM_AUX_FUNC5 105
param set-default PWM_AUX_FUNC6 106
param set-default PWM_AUX_FUNC7 107
param set-default PWM_AUX_FUNC8 108
param set-default PWM_AUX_DIS1 0
param set-default PWM_AUX_DIS2 0
param set-default PWM_AUX_DIS3 0
param set-default PWM_AUX_DIS4 0
param set-default PWM_AUX_DIS5 0
param set-default PWM_AUX_DIS6 0
param set-default PWM_AUX_DIS7 0
param set-default PWM_AUX_DIS8 0
param set-default PWM_AUX_MIN1 0
param set-default PWM_AUX_MIN2 0
param set-default PWM_AUX_MIN3 0
param set-default PWM_AUX_MIN4 0
param set-default PWM_AUX_MIN5 0
param set-default PWM_AUX_MIN6 0
param set-default PWM_AUX_MIN7 0
param set-default PWM_AUX_MIN8 0
# BOARD_PWM_FREQ is downscaled by 10, thus PWM value is given in 10s of usec
param set-default PWM_AUX_MAX1 10000
param set-default PWM_AUX_MAX2 10000
param set-default PWM_AUX_MAX3 10000
param set-default PWM_AUX_MAX4 10000
param set-default PWM_AUX_MAX5 10000
param set-default PWM_AUX_MAX6 10000
param set-default PWM_AUX_MAX7 10000
param set-default PWM_AUX_MAX8 10000
# Controller Tunings
param set-default SC_ROLLRATE_P 0.14
param set-default SC_PITCHRATE_P 0.14
param set-default SC_ROLLRATE_I 0.3
param set-default SC_PITCHRATE_I 0.3
param set-default SC_ROLLRATE_D 0.004
param set-default SC_PITCHRATE_D 0.004
@@ -48,6 +48,7 @@ if(CONFIG_MODULES_SIMULATION_PWM_OUT_SIM)
1100_rc_quad_x_sih.hil
1101_rc_plane_sih.hil
1102_tailsitter_duo_sih.hil
1103_standard_vtol_sih.hil
)
endif()
@@ -24,7 +24,6 @@ param set-default COM_DISARM_PRFLT -1
param set-default EKF2_ARSP_THR 8
param set-default EKF2_FUSE_BETA 1
param set-default EKF2_GPS_CHECK 21
param set-default EKF2_MAG_ACCLIM 0
param set-default EKF2_REQ_EPH 10
param set-default EKF2_REQ_EPV 10
@@ -12,6 +12,7 @@ param set-default MAV_TYPE 4
param set-default COM_PREARM_MODE 2
param set-default COM_SPOOLUP_TIME 10
param set-default COM_DISARM_PRFLT 60
# No need for minimum collective pitch (or airmode) to keep torque authority
param set-default MPC_MANTHR_MIN 0
@@ -21,3 +21,6 @@ param set-default RTL_RETURN_ALT 30
param set-default RTL_DESCEND_ALT 10
param set-default GPS_UBX_DYNMODEL 6
# lower RNG_FOG since MC are expected to fly closer over obstacles
param set-default EKF2_RNG_FOG 1.0
+36
View File
@@ -0,0 +1,36 @@
#!/bin/sh
#
# Standard apps for sr. Attitude/Position estimator, Attitude/Position control.
#
# NOTE: Script variables are declared/initialized/unset in the rcS script.
#
# Start Spacecraft App
spacecraft start
# Estimator Group Selection
# ekf2 start &
# Start MicroDDS Client
# uxrce_dds_client start -t udp -h 192.168.0.1 -n spacebot2
# uxrce_dds_client start -t udp -p 8888
#
# Start Control Allocator
#
# sc_control_allocator start
#
# Start Spacecraft Rate Controller.
#
# sc_rate_control start
#
# Start Spacecraft Attitude Controller.
#
# sc_att_control start
#
# Start Spacecraft Position Controller.
#
# sc_pos_control start
+27
View File
@@ -0,0 +1,27 @@
#!/bin/sh
#
# NOTE: Script variables are declared/initialized/unset in the rcS script.
#
set VEHICLE_TYPE sc
# MAV_TYPE_QUADROTOR 2
#param set-default MAV_TYPE 12
# Set micro-dds-client to use ethernet and IP-address 192.168.0.1
param set-default UXRCE_DDS_AG_IP -1062731775
# Disable preflight disarm to not interfere with external launching
param set-default COM_DISARM_PRFLT -1
param set-default CBRK_SUPPLY_CHK 894281
param set-default COM_ARM_HFLT_CHK 0
#Missing params
param set-default CP_DIST -1.0
# Default to MoCap fusion
param set-default ATT_EXT_HDG_M 2
param set-default EKF2_EV_CTRL 15
param set-default EKF2_EV_DELAY 5
param set-default EKF2_GPS_CTRL 0
param set-default EKF2_HGT_REF 3
+82 -58
View File
@@ -302,6 +302,75 @@ else
. $FCONFIG
fi
#
# Sensors System (start before Commander so Preflight checks are properly run).
#
if param greater SYS_HITL 0
then
sensors start -h
# disable GPS
param set GPS_1_CONFIG 0
# start the simulator in hardware if needed
if param compare SYS_HITL 2
then
simulator_sih start
sensor_baro_sim start
sensor_mag_sim start
sensor_gps_sim start
sensor_agp_sim start
fi
else
#
# board sensors: rc.sensors
#
set BOARD_RC_SENSORS ${R}etc/init.d/rc.board_sensors
if [ -f $BOARD_RC_SENSORS ]
then
echo "Board sensors: ${BOARD_RC_SENSORS}"
. $BOARD_RC_SENSORS
fi
unset BOARD_RC_SENSORS
. ${R}etc/init.d/rc.sensors
if param compare -s BAT1_SOURCE 2
then
esc_battery start
fi
if ! param compare BAT1_SOURCE 1
then
battery_status start
fi
sensors start
fi
#
# state estimator selection
#
if param compare -s EKF2_EN 1
then
ekf2 start &
fi
if param compare -s LPE_EN 1
then
local_position_estimator start
fi
if param compare -s ATT_EN 1
then
attitude_estimator_q start
fi
#
# px4io
#
if px4io supported
then
# Check if PX4IO present and update firmware if needed.
@@ -354,6 +423,11 @@ else
then
pps_capture start
fi
# RPM capture driver
if param greater -s RPM_CAP_ENABLE 0
then
rpm_capture start
fi
# Camera capture driver
if param greater -s CAM_CAP_FBACK 0
then
@@ -364,79 +438,24 @@ else
fi
#
# Sensors System (start before Commander so Preflight checks are properly run).
# Commander needs to be this early for in-air-restarts.
# Commander
#
if param greater SYS_HITL 0
then
commander start -h
if ! pwm_out_sim start -m hil
then
tune_control play error
fi
sensors start -h
commander start -h
# disable GPS
param set GPS_1_CONFIG 0
# start the simulator in hardware if needed
if param compare SYS_HITL 2
then
simulator_sih start
sensor_baro_sim start
sensor_mag_sim start
sensor_gps_sim start
sensor_agp_sim start
fi
else
#
# board sensors: rc.sensors
#
set BOARD_RC_SENSORS ${R}etc/init.d/rc.board_sensors
if [ -f $BOARD_RC_SENSORS ]
then
echo "Board sensors: ${BOARD_RC_SENSORS}"
. $BOARD_RC_SENSORS
fi
unset BOARD_RC_SENSORS
. ${R}etc/init.d/rc.sensors
if param compare -s BAT1_SOURCE 2
then
esc_battery start
fi
if ! param compare BAT1_SOURCE 1
then
battery_status start
fi
sensors start
commander start
dshot start
pwm_out start
fi
#
# state estimator selection
if param compare -s EKF2_EN 1
then
ekf2 start &
fi
if param compare -s LPE_EN 1
then
local_position_estimator start
fi
if param compare -s ATT_EN 1
then
attitude_estimator_q start
fi
#
# Configure vehicle type specific parameters.
# Note: rc.vehicle_setup is the entry point for all vehicle type specific setup.
@@ -536,6 +555,11 @@ else
payload_deliverer start
fi
if param compare -s ICE_EN 1
then
internal_combustion_engine_control start
fi
#
# Optional board supplied extras: rc.board_extras
#
-3
View File
@@ -136,9 +136,6 @@ class TestHardwareMethods(unittest.TestCase):
def test_atomic_bitset(self):
self.assertTrue(do_test(self.TEST_DEVICE, self.TEST_BAUDRATE, "atomic_bitset"))
def test_bezier(self):
self.assertTrue(do_test(self.TEST_DEVICE, self.TEST_BAUDRATE, "bezier"))
def test_bitset(self):
self.assertTrue(do_test(self.TEST_DEVICE, self.TEST_BAUDRATE, "bitset"))
@@ -8,10 +8,12 @@ if [ $# -gt 0 ]; then
fi
exec find boards msg src platforms test \
-path msg/translation_node -prune -o \
-path platforms/nuttx/NuttX -prune -o \
-path platforms/qurt/dspal -prune -o \
-path src/drivers/ins/vectornav/libvnc -prune -o \
-path src/drivers/uavcan/libdronecan -prune -o \
-path src/drivers/uavcan/libuavcan -prune -o \
-path src/drivers/uavcan/uavcan_drivers/kinetis/driver/include/uavcan_kinetis -prune -o \
-path src/drivers/cyphal/libcanard -prune -o \
-path src/lib/crypto/monocypher -prune -o \
+76
View File
@@ -0,0 +1,76 @@
#! /bin/bash
# Copy a git diff between two commits if msg versioning is added
DIR=$( cd "$( dirname "${BASH_SOURCE[0]}" )" && pwd )
PX4_SRC_DIR="$DIR/.."
BASE_COMMIT="$1"
HEAD_COMMIT="$2"
if [ -z "${BASE_COMMIT}" ] || [ -z "${HEAD_COMMIT}" ]
then
echo "Usage: $0 <base_commit> <head_commit>"
exit 1
fi
failed=0
# Iterate git diff files between BASE_COMMIT and HEAD_COMMIT
modified_files="$(git --no-pager diff --no-color --name-only --diff-filter=M "${BASE_COMMIT}"..."${HEAD_COMMIT}")"
all_files="$( git --no-pager diff --no-color --name-only "${BASE_COMMIT}"..."${HEAD_COMMIT}")"
for file in ${modified_files}
do
if [[ "$file" == msg/versioned/*.msg ]]; then
echo "Modified msg file: ${file}"
# A modified versioned .msg file requires:
# - Incrementing the version
# - An old .msg version exists
# - A translation header exists and is included
# Ignore changes to comments or constants
content_a=$(git show "${BASE_COMMIT}:${file}" | grep -o '^[^#]*' | grep -v =)
content_b=$(git show "${HEAD_COMMIT}:${file}" | grep -o '^[^#]*' | grep -v =)
if [ "${content_a}" == "${content_b}" ]; then
echo "No version update required for ${file}"
continue
fi
diff=$(git --no-pager diff --no-color --diff-filter=M "${BASE_COMMIT}"..."${HEAD_COMMIT}" -- "${file}")
old_version=$(echo "${diff}" | sed -n 's/^-uint32 MESSAGE_VERSION = \([0-9]*\).*/\1/p')
new_version=$(echo "${diff}" | sed -n 's/^+uint32 MESSAGE_VERSION = \([0-9]*\).*/\1/p')
# Check that the version is incremented
if [ -z "${new_version}" ] || [ -z "${old_version}" ]; then
echo "ERROR: Missing version update for ${file}"
failed=1
else
if [ $((new_version-old_version)) -ne 1 ]; then
echo "ERROR: Version not incremented by +1 for ${file}"
failed=1
fi
fi
# Check that an old version exists
filename=$(basename -- "$file")
filename="${filename%.*}"
old_version_file="px4_msgs_old/msg/${filename}V${old_version}.msg"
if [[ "${all_files}" != *"${old_version_file}"* ]]; then
echo "ERROR: Old message version does not exist for ${file} (missing ${old_version_file})"
failed=1
fi
# Check that a translation header got added by checking for a modification to all_translations.h
# If it is changed, we assume a new header got added too, so we don't explicitly check for that
if [[ "${modified_files}" != *"translations/all_translations.h"* ]]; then
echo "ERROR: missing modification to translations/all_translations.h"
failed=1
fi
fi
done
if [ ${failed} -ne 0 ]; then
echo ""
echo "ERROR: missing message versioning due to changed .msg file(s) (see above)"
echo "Check the documentation under https://docs.px4.io/main/en/ros2/px4_ros2_msg_translation_node.html for how to add a new version"
exit 1
fi
+3 -6
View File
@@ -69,7 +69,7 @@ def process_target(px4board_file, target_name):
group = None
if px4board_file.endswith("default.px4board") or \
px4board_file.endswith("recovery.px4board") or \
px4board_file.endswith("performance-test.px4board") or \
px4board_file.endswith("bootloader.px4board"):
kconf.load_config(px4board_file, replace=True)
else: # Merge config with default.px4board
@@ -87,20 +87,17 @@ def process_target(px4board_file, target_name):
if platform not in excluded_platforms:
# get the container based on the platform and toolchain
container = 'ghcr.io/px4/px4-dev:main'
if platform == 'posix':
container = 'px4io/px4-dev-base-focal:2021-09-08'
group = 'base'
if toolchain:
if toolchain.startswith('aarch64'):
container = 'px4io/px4-dev-aarch64:2022-08-12'
group = 'aarch64'
elif toolchain == 'arm-linux-gnueabihf':
container = 'px4io/px4-dev-armhf:2023-06-26'
group = 'armhf'
else:
if verbose: print(f'unmatched toolchain: {toolchain}')
elif platform == 'nuttx':
container = 'px4io/px4-dev-nuttx-focal:2022-08-12'
group = 'nuttx'
else:
if verbose: print(f'unmatched platform: {platform}')
@@ -124,7 +121,7 @@ if(verbose):
# - Events
metadata_targets = ['airframe_metadata', 'parameters_metadata', 'extract_events']
grouped_targets['base'] = {}
grouped_targets['base']['container'] = 'px4io/px4-dev-base-focal:2021-09-08'
grouped_targets['base']['container'] = 'ghcr.io/px4/px4-dev:main'
grouped_targets['base']['manufacturers'] = {}
grouped_targets['base']['manufacturers']['px4'] = []
grouped_targets['base']['manufacturers']['px4'] += metadata_targets
+22 -19
View File
@@ -4,8 +4,9 @@ mkdir artifacts
cp **/**/*.px4 artifacts/
cp **/**/*.elf artifacts/
for build_dir_path in build/*/ ; do
build_dir_path=${build_dir_path::${#build_dir_path}-1}
build_dir=${build_dir_path#*/}
build_dir=${build_dir::${#build_dir}-1}
target_name=$build_dir
mkdir artifacts/$build_dir
find artifacts/ -maxdepth 1 -type f -name "*$build_dir*"
# Airframe
@@ -26,21 +27,23 @@ for build_dir_path in build/*/ ; do
echo "----------"
done
# general metadata
mkdir artifacts/_general/
cp artifacts/px4_sitl_default/airframes.xml artifacts/_general/
# Airframe
cp artifacts/px4_sitl_default/airframes.xml artifacts/_general/
# Parameters
cp artifacts/px4_sitl_default/parameters.xml artifacts/_general/
cp artifacts/px4_sitl_default/parameters.json artifacts/_general/
cp artifacts/px4_sitl_default/parameters.json.xz artifacts/_general/
# Actuators
cp artifacts/px4_sitl_default/actuators.json artifacts/_general/
cp artifacts/px4_sitl_default/actuators.json.xz artifacts/_general/
# Events
cp artifacts/px4_sitl_default/events/all_events.json.xz artifacts/_general/
# ROS 2 msgs
cp artifacts/px4_sitl_default/events/all_events.json.xz artifacts/_general/
# Module Docs
ls -la artifacts/_general/
if [ -d artifacts/px4_sitl_default ]; then
# general metadata
mkdir artifacts/_general/
cp artifacts/px4_sitl_default/airframes.xml artifacts/_general/
# Airframe
cp artifacts/px4_sitl_default/airframes.xml artifacts/_general/
# Parameters
cp artifacts/px4_sitl_default/parameters.xml artifacts/_general/
cp artifacts/px4_sitl_default/parameters.json artifacts/_general/
cp artifacts/px4_sitl_default/parameters.json.xz artifacts/_general/
# Actuators
cp artifacts/px4_sitl_default/actuators.json artifacts/_general/
cp artifacts/px4_sitl_default/actuators.json.xz artifacts/_general/
# Events
cp artifacts/px4_sitl_default/events/all_events.json.xz artifacts/_general/
# ROS 2 msgs
cp artifacts/px4_sitl_default/events/all_events.json.xz artifacts/_general/
# Module Docs
ls -la artifacts/_general/
fi
+33
View File
@@ -0,0 +1,33 @@
#! /bin/bash
# Copy msgs and the message translation node into a ROS workspace directory
DIR=$( cd "$( dirname "${BASH_SOURCE[0]}" )" && pwd )
PX4_SRC_DIR="$DIR/.."
WS_DIR="$1"
if [ ! -e "${WS_DIR}" ]
then
echo "Usage: $0 <ros_ws_dir>"
exit 1
fi
WS_DIR="$WS_DIR"/src
if [ ! -e "${WS_DIR}" ]
then
echo "'src' directory not found inside ROS workspace (${WS_DIR})"
exit 1
fi
cp -ar "${PX4_SRC_DIR}"/msg/translation_node "${WS_DIR}"
cp -ar "${PX4_SRC_DIR}"/msg/px4_msgs_old "${WS_DIR}"
PX4_MSGS_DIR="${WS_DIR}"/px4_msgs
if [ ! -e "${PX4_MSGS_DIR}" ]
then
git clone https://github.com/PX4/px4_msgs.git "${PX4_MSGS_DIR}"
rm -rf "${PX4_MSGS_DIR}"/msg/*.msg
rm -rf "${PX4_MSGS_DIR}"/msg/versioned/*.msg
rm -rf "${PX4_MSGS_DIR}"/srv/*.srv
fi
cp -ar "${PX4_SRC_DIR}"/msg/*.msg "${PX4_MSGS_DIR}"/msg
cp -ar "${PX4_SRC_DIR}"/msg/versioned/*.msg "${PX4_MSGS_DIR}"/msg
cp -ar "${PX4_SRC_DIR}"/srv/*.srv "${PX4_MSGS_DIR}"/srv
+1 -1
View File
@@ -47,6 +47,7 @@ CCACHE_DIR=${HOME}/.ccache
mkdir -p "${CCACHE_DIR}"
docker run -it --rm -w "${SRC_DIR}" \
--user="$(id -u):$(id -g)" \
--env=AWS_ACCESS_KEY_ID \
--env=AWS_SECRET_ACCESS_KEY \
--env=BRANCH_NAME \
@@ -54,7 +55,6 @@ docker run -it --rm -w "${SRC_DIR}" \
--env=CI \
--env=CODECOV_TOKEN \
--env=COVERALLS_REPO_TOKEN \
--env=LOCAL_USER_ID="$(id -u)" \
--env=PX4_ASAN \
--env=PX4_MSAN \
--env=PX4_TSAN \
+4
View File
@@ -40,6 +40,7 @@ exception_list = [
'DRIVERS_DISTANCE_SENSOR_SRF05', # Requires hardcoded GPIO_ULTRASOUND
'DRIVERS_PPS_CAPTURE', # Requires PPS GPIO config
'DRIVERS_PWM_INPUT', # Requires PWM config
'DRIVERS_RPM_CAPTURE', # Requires PPS GPIO config
'DRIVERS_TEST_PPM', # PIN config not portable
'DRIVERS_TATTU_CAN', # Broken needs fixing
'MODULES_REPLAY', # Fails on NuttX targets maybe force POSIX dependency?
@@ -52,6 +53,7 @@ exception_list = [
'SYSTEMCMDS_I2C_LAUNCHER', # undefined reference to `system',
'MODULES_MUORB_APPS', # Weird QURT/Posix package doesn't work on x86 px4 sitl
'MODULES_SIMULATION_SIMULATOR_SIH', # Causes compile errors
'MODULES_SPACECRAFT', # Clashes with Control Allocation (mom's spaghetti code)
]
exception_list_sitl = [
@@ -72,6 +74,8 @@ exception_list_sitl = [
'SYSTEMCMDS_I2CDETECT', # Not supported in SITL
'SYSTEMCMDS_DMESG', # Not supported in SITL
'SYSTEMCMDS_USB_CONNECTED', # Not supported in SITL
'SYSTEMCMDS_MFT_CFG', # Not supported in SITL
'MODULES_SPACECRAFT', # Clashes with Control Allocation (mom's spaghetti code)
]
def main():
+2 -3
View File
@@ -189,7 +189,7 @@ class uploader:
GET_CHIP = b'\x2c' # rev5+ , get chip version
SET_BOOT_DELAY = b'\x2d' # rev5+ , set boot delay
GET_CHIP_DES = b'\x2e' # rev5+ , get chip description in ASCII
GET_VERSION = b'\x2f' # rev5+ , get chip description in ASCII
GET_VERSION = b'\x2f' # rev5+ , get bootloader version in ASCII
CHIP_FULL_ERASE = b'\x40' # full erase of flash, rev6+
MAX_DES_LENGTH = 20
@@ -201,7 +201,6 @@ class uploader:
INFO_BOARD_ID = b'\x02' # board type
INFO_BOARD_REV = b'\x03' # board revision
INFO_FLASH_SIZE = b'\x04' # max firmware size in bytes
BL_VERSION = b'\x07' # get bootloader version, e.g. major.minor.patch.githash (up to 20 chars)
PROG_MULTI_MAX = 252 # protocol max is 255, must be multiple of 4
READ_MULTI_MAX = 252 # protocol max is 255
@@ -709,7 +708,7 @@ class uploader:
# https://github.com/PX4/Firmware/blob/master/src/drivers/boards/common/stm32/board_mcu_version.c#L125-L144
if self.fw_maxsize > fw.property('image_maxsize') and not force:
raise RuntimeError(f"Board can accept larger flash images ({self.fw_maxsize} bytes) than board config ({fw.property('image_maxsize')} bytes). Please use the correct board configuration to avoid lacking critical functionality.")
print(f"WARNING: Board can accept larger flash images ({self.fw_maxsize} bytes) than board config ({fw.property('image_maxsize')} bytes)")
else:
# If we're still on bootloader v4 on a Pixhawk, we don't know if we
# have the silicon errata and therefore need to flash px4_fmu-v2
+10 -16
View File
@@ -1,33 +1,27 @@
#!/bin/bash
echo "[docker-entrypoint.sh] Starting entrypoint"
GREEN='\033[0;32m'
NC='\033[0m' # No Color
FILE_DESCRIPTOR="${GREEN}[docker-entrypoint.sh]${NC}"
echo -e "$FILE_DESCRIPTOR Starting"
# Start virtual X server in the background
# - DISPLAY default is :99, set in dockerfile
# - Users can override with `-e DISPLAY=` in `docker run` command to avoid
# running Xvfb and attach their screen
if [[ -x "$(command -v Xvfb)" && "$DISPLAY" == ":99" ]]; then
echo "[docker-entrypoint.sh] Starting Xvfb"
echo -e "$FILE_DESCRIPTOR Starting Xvfb"
Xvfb :99 -screen 0 1600x1200x24+32 &
fi
# Check if the ROS_DISTRO is passed and use it
# to source the ROS environment
if [ -n "${ROS_DISTRO}" ]; then
echo "[docker-entrypoint.sh] ROS: ${ROS_DISTRO}"
echo -e "$FILE_DESCRIPTOR ROS: ${ROS_DISTRO}"
source "/opt/ros/$ROS_DISTRO/setup.bash"
fi
echo "[docker-entrypoint.sh] Working Directory: ${pwd}"
echo -e "$FILE_DESCRIPTOR ($( uname -m ))"
# Use the LOCAL_USER_ID if passed in at runtime
if [ -n "${LOCAL_USER_ID}" ]; then
echo "[docker-entrypoint.sh] Starting with: $LOCAL_USER_ID:user"
# modify existing user's id
usermod -u $LOCAL_USER_ID user
# run as user
# exec gosu user "$@"
exec "$@"
else
exec "$@"
fi
exec "$@"
+33 -15
View File
@@ -27,9 +27,12 @@ do
fi
done
echo "[ubuntu.sh] Starting..."
echo "[ubuntu.sh] arch: ${GREEN}$INSTALL_ARCH${NC}"
# detect if running in docker
if [ -f /.dockerenv ]; then
echo "Running within docker, installing initial dependencies";
echo "[ubuntu.sh] Running within docker, installing initial dependencies";
apt-get --quiet -y update && DEBIAN_FRONTEND=noninteractive apt-get --quiet -y install \
ca-certificates \
gnupg \
@@ -47,7 +50,7 @@ DIR=$( cd "$( dirname "${BASH_SOURCE[0]}" )" && pwd )
# check requirements.txt exists (script not run in source tree)
REQUIREMENTS_FILE="requirements.txt"
if [[ ! -f "${DIR}/${REQUIREMENTS_FILE}" ]]; then
echo "FAILED: ${REQUIREMENTS_FILE} needed in same directory as ubuntu.sh (${DIR})."
echo "[ubuntu.sh] FAILED: ${REQUIREMENTS_FILE} needed in same directory as ubuntu.sh (${DIR})."
return 1
fi
@@ -55,10 +58,8 @@ fi
# check ubuntu version
# otherwise warn and point to docker?
UBUNTU_RELEASE="`lsb_release -rs`"
echo "Ubuntu ${UBUNTU_RELEASE}"
echo
echo "Installing PX4 general dependencies"
echo "[ubuntu.sh] Ubuntu ${GREEN}${UBUNTU_RELEASE}${NC}"
echo "[ubuntu.sh] Installing PX4 general dependencies"
sudo apt-get update -y --quiet
sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
@@ -91,7 +92,7 @@ sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends i
# Python3 dependencies
echo
echo "Installing PX4 Python3 dependencies"
echo "[ubuntu.sh] Installing PX4 Python3 dependencies"
PYTHON_VERSION=$(python3 --version 2>&1 | awk '{print $2}')
REQUIRED_VERSION="3.11"
if [[ "$(printf '%s\n' "$REQUIRED_VERSION" "$PYTHON_VERSION" | sort -V | head -n1)" == "$REQUIRED_VERSION" ]]; then
@@ -109,17 +110,15 @@ fi
if [[ $INSTALL_NUTTX == "true" ]]; then
echo
echo "Installing NuttX dependencies"
echo "[ubuntu.sh] NuttX Installing Dependencies"
sudo apt-get update -y --quiet
sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
automake \
binutils-dev \
bison \
build-essential \
curl \
flex \
g++-multilib \
gcc-arm-none-eabi \
gcc-multilib \
gdb-multiarch \
genromfs \
gettext \
@@ -146,6 +145,25 @@ if [[ $INSTALL_NUTTX == "true" ]]; then
vim-common \
;
echo
echo "[ubuntu.sh] NuttX Installing Dependencies ($INSTALL_ARCH)"
if [[ "${INSTALL_ARCH}" == "x86_64" ]]; then
sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
g++-multilib \
gcc-arm-none-eabi \
gcc-multilib \
;
fi
if [[ "${INSTALL_ARCH}" == "aarch64" ]]; then
sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
g++-aarch64-linux-gnu \
g++-arm-linux-gnueabihf \
;
fi
if [ -n "$USER" ]; then
# add user to dialout group (serial port access)
sudo usermod -aG dialout $USER
@@ -156,7 +174,7 @@ fi
if [[ $INSTALL_SIM == "true" ]]; then
echo
echo "Installing PX4 simulation dependencies"
echo "[ubuntu.sh] Installing PX4 simulation dependencies"
# General simulation dependencies
sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
@@ -181,8 +199,8 @@ if [[ $INSTALL_SIM == "true" ]]; then
fi
else
# Expects Ubuntu 22.04 > by default
echo "Gazebo (Harmonic) will be installed"
echo "Earlier versions will be removed"
echo "[ubuntu.sh] Gazebo (Harmonic) will be installed"
echo "[ubuntu.sh] Earlier versions will be removed"
# Add Gazebo binary repository
sudo wget https://packages.osrfoundation.org/gazebo.gpg -O /usr/share/keyrings/pkgs-osrf-archive-keyring.gpg
echo "deb [arch=$(dpkg --print-architecture) signed-by=/usr/share/keyrings/pkgs-osrf-archive-keyring.gpg] http://packages.osrfoundation.org/gazebo/ubuntu-stable $(lsb_release -cs) main" | sudo tee /etc/apt/sources.list.d/gazebo-stable.list > /dev/null
+6 -1
View File
@@ -107,8 +107,13 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(6);
up_mdelay(100);
}
}
@@ -0,0 +1,5 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT=""
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_BOOTLOADERS=y
+13
View File
@@ -0,0 +1,13 @@
{
"board_id": 88,
"magic": "PX4FWv1",
"description": "Firmware for the ARK Flow MR board",
"image": "",
"build_time": 0,
"summary": "ARKFLOWMR",
"version": "0.1",
"image_size": 0,
"image_maxsize": 2080768,
"git_identity": "",
"board_revision": 0
}
@@ -0,0 +1,20 @@
#!/bin/sh
#
# board sensors init
#------------------------------------------------------------------------------
param set-default IMU_GYRO_RATEMAX 1000
param set-default SENS_FLOW_RATE 150
param set-default SENS_IMU_CLPNOTI 0
param set-default SENS_AFBR_S_RATE 25
param set-default SENS_AFBR_L_RATE 10
param set-default SENS_AFBR_THRESH 8
param set-default SENS_AFBR_HYSTER 2
# Internal SPI
paa3905 -s start -Y 180
iim42653 -R 0 -s start
afbrs50 start
@@ -0,0 +1,57 @@
#
# This file is autogenerated: PLEASE DO NOT EDIT IT.
#
# You can use "make menuconfig" to make any modifications to the installed .config file.
# You can then do "make savedefconfig" to generate a new defconfig file that includes your
# modifications.
#
CONFIG_ARCH="arm"
CONFIG_ARCH_BOARD_CUSTOM=y
CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/ark/can-flow-mr/nuttx-config"
CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
CONFIG_ARCH_CHIP="stm32"
CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F412CE=y
CONFIG_ARCH_INTERRUPTSTACK=4096
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BINFMT_DISABLE=y
CONFIG_BOARDCTL=y
CONFIG_BOARD_LOOPSPERMSEC=16717
CONFIG_DEBUG_FULLOPT=y
CONFIG_DEBUG_SYMBOLS=y
CONFIG_DEBUG_TCBINFO=y
CONFIG_DEFAULT_SMALL=y
CONFIG_DISABLE_MOUNTPOINT=y
CONFIG_EXPERIMENTAL=y
CONFIG_FDCLONE_DISABLE=y
CONFIG_FDCLONE_STDIO=y
CONFIG_HAVE_CXX=y
CONFIG_HAVE_CXXINITIALIZE=y
CONFIG_IDLETHREAD_STACKSIZE=4096
CONFIG_INIT_STACKSIZE=4096
CONFIG_LIBC_FLOATINGPOINT=y
CONFIG_LIBC_LONG_LONG=y
CONFIG_LIBC_STRERROR=y
CONFIG_MM_REGIONS=2
CONFIG_NAME_MAX=0
CONFIG_NUNGET_CHARS=0
CONFIG_PREALLOC_TIMERS=0
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_RAM_SIZE=262144
CONFIG_RAM_START=0x20010000
CONFIG_RAW_BINARY=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
CONFIG_SIG_SIGUSR1_ACTION=y
CONFIG_SIG_SIGUSR2_ACTION=y
CONFIG_STACK_COLORATION=y
CONFIG_START_DAY=30
CONFIG_START_MONTH=11
CONFIG_STDIO_DISABLE_BUFFERING=y
CONFIG_STM32_FLASH_CONFIG_G=y
CONFIG_STM32_NOEXT_VECTORS=y
CONFIG_STM32_TIM8=y
CONFIG_TASK_NAME_SIZE=0
CONFIG_USEC_PER_TICK=1000
@@ -0,0 +1,136 @@
/************************************************************************************
* configs/px4fmu/include/board.h
* include/arch/board/board.h
*
* Copyright (C) 2009 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
************************************************************************************/
#include "board_dma_map.h"
#ifndef __ARCH_BOARD_BOARD_H
#define __ARCH_BOARD_BOARD_H
#include <nuttx/config.h>
#ifndef __ASSEMBLY__
# include <stdint.h>
#endif
#include <stm32.h>
/* HSI - 8 MHz RC factory-trimmed
* LSI - 32 KHz RC
* HSE - 8 MHz Crystal
* LSE - not installed
*/
#define STM32_BOARD_USEHSE 1
#define STM32_BOARD_XTAL 8000000
#define STM32_HSE_FREQUENCY STM32_BOARD_XTAL
#define STM32_HSI_FREQUENCY 16000000ul
#define STM32_LSI_FREQUENCY 32000
/* Main PLL Configuration */
#define STM32_PLLCFG_PLLM RCC_PLLCFG_PLLM(8)
#define STM32_PLLCFG_PLLN RCC_PLLCFG_PLLN(384)
#define STM32_PLLCFG_PLLP RCC_PLLCFG_PLLP_4
#define STM32_PLLCFG_PLLQ RCC_PLLCFG_PLLQ(8)
#define STM32_PLLCFG_PLLR RCC_PLLCFG_PLLR(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SM RCC_PLLI2SCFGR_PLLI2SM(16)
#define STM32_RCC_PLLI2SCFGR_PLLI2SN RCC_PLLI2SCFGR_PLLI2SN(192)
#define STM32_RCC_PLLI2SCFGR_PLLI2SQ RCC_PLLI2SCFGR_PLLI2SQ(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SR RCC_PLLI2SCFGR_PLLI2SR(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SSRC RCC_PLLI2SCFGR_PLLI2SSRC(0) /* HSE or HSI depending on PLLSRC of PLLCFGR*/
#define STM32_RCC_DCKCFGR2_CK48MSEL RCC_DCKCFGR2_CK48MSEL_PLL
#define STM32_RCC_DCKCFGR2_FMPI2C1SEL RCC_DCKCFGR2_FMPI2C1SEL_APB
#define STM32_RCC_DCKCFGR2_SDIOSEL RCC_DCKCFGR2_SDIOSEL_48MHZ
#define STM32_SYSCLK_FREQUENCY 96000000ul
/* AHB clock (HCLK) is SYSCLK (96MHz) */
#define STM32_RCC_CFGR_HPRE RCC_CFGR_HPRE_SYSCLK /* HCLK = SYSCLK / 1 */
#define STM32_HCLK_FREQUENCY STM32_SYSCLK_FREQUENCY
#define STM32_BOARD_HCLK STM32_HCLK_FREQUENCY /* Same as above, to satisfy compiler */
/* APB1 clock (PCLK1) is HCLK/2 (48MHz) */
#define STM32_RCC_CFGR_PPRE1 RCC_CFGR_PPRE1_HCLKd2 /* PCLK1 = HCLK / 2 */
#define STM32_PCLK1_FREQUENCY (STM32_HCLK_FREQUENCY/2)
/* Timers driven from APB1 will be twice PCLK1 (see page 112 of reference manual) */
#define STM32_APB1_TIM2_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM3_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM4_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM5_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM12_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM13_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM14_CLKIN (2*STM32_PCLK1_FREQUENCY)
/* APB2 clock (PCLK2) is HCLK (96MHz) */
#define STM32_RCC_CFGR_PPRE2 RCC_CFGR_PPRE2_HCLK /* PCLK2 = HCLK */
#define STM32_PCLK2_FREQUENCY (STM32_HCLK_FREQUENCY)
/* Timers driven from APB2 will be PCLK2 since no prescale division */
#define STM32_APB2_TIM1_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM8_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM9_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM10_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM11_CLKIN (STM32_PCLK2_FREQUENCY)
/* Timer Frequencies, if APBx is set to 1, frequency is same to APBx otherwise frequency is 2xAPBx. */
#define BOARD_TIM2_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM3_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM4_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM5_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM6_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM7_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM8_FREQUENCY (2 * STM32_PCLK2_FREQUENCY)
/* Alternate function pin selections ************************************************/
/* UARTs */
#define GPIO_USART2_RX GPIO_USART2_RX_1
#define GPIO_USART2_TX GPIO_USART2_TX_1
/* CAN */
#define GPIO_CAN1_RX GPIO_CAN1_RX_1
#define GPIO_CAN1_TX GPIO_CAN1_TX_1
/* SPI */
#define GPIO_SPI1_MISO GPIO_SPI1_MISO_1
#define GPIO_SPI1_MOSI GPIO_SPI1_MOSI_1
#define GPIO_SPI1_SCK GPIO_SPI1_SCK_1
#define GPIO_SPI2_MISO GPIO_SPI2_MISO_1 /* PB14 */
#define GPIO_SPI2_MOSI GPIO_SPI2_MOSI_1 /* PB15 */
#define GPIO_SPI2_SCK GPIO_SPI2_SCK_1 /* PB10 */
#endif /* __ARCH_BOARD_BOARD_H */
@@ -0,0 +1,44 @@
/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#pragma once
// DMA1 Channel/Stream Selections
//--------------------------------------------//---------------------------//----------------
#define DMACHAN_SPI2_RX DMAMAP_SPI2_RX // DMA1, Stream 3, Channel 0
#define DMACHAN_SPI2_TX DMAMAP_SPI2_TX // DMA1, Stream 4, Channel 0
// DMA2 Channel/Stream Selections
//--------------------------------------------//---------------------------//----------------
#define DMACHAN_SPI1_RX DMAMAP_SPI1_RX_2 // DMA2, Stream 2, Channel 3
#define DMACHAN_SPI1_TX DMAMAP_SPI1_TX_2 // DMA2, Stream 5, Channel 3
@@ -0,0 +1,149 @@
#
# This file is autogenerated: PLEASE DO NOT EDIT IT.
#
# You can use "make menuconfig" to make any modifications to the installed .config file.
# You can then do "make savedefconfig" to generate a new defconfig file that includes your
# modifications.
#
# CONFIG_DISABLE_ENVIRON is not set
# CONFIG_DISABLE_PSEUDOFS_OPERATIONS is not set
# CONFIG_DISABLE_PTHREAD is not set
# CONFIG_NSH_DISABLEBG is not set
# CONFIG_NSH_DISABLESCRIPT is not set
# CONFIG_NSH_DISABLE_CAT is not set
# CONFIG_NSH_DISABLE_CD is not set
# CONFIG_NSH_DISABLE_CP is not set
# CONFIG_NSH_DISABLE_DATE is not set
# CONFIG_NSH_DISABLE_DF is not set
# CONFIG_NSH_DISABLE_ECHO is not set
# CONFIG_NSH_DISABLE_ENV is not set
# CONFIG_NSH_DISABLE_EXEC is not set
# CONFIG_NSH_DISABLE_EXPORT is not set
# CONFIG_NSH_DISABLE_FREE is not set
# CONFIG_NSH_DISABLE_GET is not set
# CONFIG_NSH_DISABLE_HELP is not set
# CONFIG_NSH_DISABLE_ITEF is not set
# CONFIG_NSH_DISABLE_KILL is not set
# CONFIG_NSH_DISABLE_LOOPS is not set
# CONFIG_NSH_DISABLE_LS is not set
# CONFIG_NSH_DISABLE_MKDIR is not set
# CONFIG_NSH_DISABLE_MOUNT is not set
# CONFIG_NSH_DISABLE_MV is not set
# CONFIG_NSH_DISABLE_PS is not set
# CONFIG_NSH_DISABLE_PSSTACKUSAGE is not set
# CONFIG_NSH_DISABLE_PWD is not set
# CONFIG_NSH_DISABLE_RM is not set
# CONFIG_NSH_DISABLE_RMDIR is not set
# CONFIG_NSH_DISABLE_SEMICOLON is not set
# CONFIG_NSH_DISABLE_SET is not set
# CONFIG_NSH_DISABLE_SLEEP is not set
# CONFIG_NSH_DISABLE_SOURCE is not set
# CONFIG_NSH_DISABLE_TEST is not set
# CONFIG_NSH_DISABLE_TIME is not set
# CONFIG_NSH_DISABLE_UMOUNT is not set
# CONFIG_NSH_DISABLE_UNSET is not set
# CONFIG_NSH_DISABLE_USLEEP is not set
CONFIG_ARCH="arm"
CONFIG_ARCH_BOARD_CUSTOM=y
CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/ark/can-flow-mr/nuttx-config"
CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
CONFIG_ARCH_CHIP="stm32"
CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F412CE=y
CONFIG_ARCH_INTERRUPTSTACK=768
CONFIG_ARCH_STACKDUMP=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
CONFIG_BOARD_ASSERT_RESET_VALUE=0
CONFIG_BOARD_LOOPSPERMSEC=16717
CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_BUILTIN=y
CONFIG_DEBUG_FULLOPT=y
CONFIG_DEBUG_HARDFAULT_ALERT=y
CONFIG_DEBUG_SYMBOLS=y
CONFIG_DEBUG_TCBINFO=y
CONFIG_DEFAULT_SMALL=y
CONFIG_FDCLONE_STDIO=y
CONFIG_FS_CROMFS=y
CONFIG_FS_ROMFS=y
CONFIG_GRAN=y
CONFIG_GRAN_INTR=y
CONFIG_HAVE_CXX=y
CONFIG_HAVE_CXXINITIALIZE=y
CONFIG_IDLETHREAD_STACKSIZE=750
CONFIG_INIT_ENTRYPOINT="nsh_main"
CONFIG_INIT_STACKSIZE=2624
CONFIG_LIBC_FLOATINGPOINT=y
CONFIG_LIBC_LONG_LONG=y
CONFIG_LIBC_MAX_EXITFUNS=1
CONFIG_MEMSET_64BIT=y
CONFIG_MEMSET_OPTSPEED=y
CONFIG_MM_REGIONS=2
CONFIG_NAME_MAX=40
CONFIG_NSH_ARCHINIT=y
CONFIG_NSH_ARGCAT=y
CONFIG_NSH_BUILTIN_APPS=y
CONFIG_NSH_CMDPARMS=y
CONFIG_NSH_CROMFSETC=y
CONFIG_NSH_LINELEN=128
CONFIG_NSH_MAXARGUMENTS=15
CONFIG_NSH_NESTDEPTH=8
CONFIG_NSH_QUOTE=y
CONFIG_NSH_ROMFSETC=y
CONFIG_NSH_ROMFSSECTSIZE=128
CONFIG_NSH_VARS=y
CONFIG_PREALLOC_TIMERS=50
CONFIG_PTHREAD_MUTEX_ROBUST=y
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_RAM_SIZE=262144
CONFIG_RAM_START=0x20000000
CONFIG_RAW_BINARY=y
CONFIG_READLINE_CMD_HISTORY=y
CONFIG_READLINE_TABCOMPLETION=y
CONFIG_SCHED_HPWORK=y
CONFIG_SCHED_HPWORKPRIORITY=254
CONFIG_SCHED_HPWORKSTACKSIZE=3000
CONFIG_SCHED_INSTRUMENTATION=y
CONFIG_SCHED_INSTRUMENTATION_EXTERNAL=y
CONFIG_SCHED_INSTRUMENTATION_SWITCH=y
CONFIG_SCHED_WAITPID=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
CONFIG_SIG_SIGUSR1_ACTION=y
CONFIG_SIG_SIGUSR2_ACTION=y
CONFIG_SIG_SIGWORK=4
CONFIG_STACK_COLORATION=y
CONFIG_START_DAY=30
CONFIG_START_MONTH=11
CONFIG_STDIO_BUFFER_SIZE=32
CONFIG_STM32_ADC1=y
CONFIG_STM32_DISABLE_IDLE_SLEEP_DURING_DEBUG=y
CONFIG_STM32_DMA1=y
CONFIG_STM32_DMA2=y
CONFIG_STM32_FLASH_CONFIG_G=y
CONFIG_STM32_FLASH_PREFETCH=y
CONFIG_STM32_FLOWCONTROL_BROKEN=y
CONFIG_STM32_JTAG_SW_ENABLE=y
CONFIG_STM32_PWR=y
CONFIG_STM32_SERIALBRK_BSDCOMPAT=y
CONFIG_STM32_SERIAL_DISABLE_REORDERING=y
CONFIG_STM32_SPI1=y
CONFIG_STM32_SPI1_DMA=y
CONFIG_STM32_SPI1_DMA_BUFFER=2048
CONFIG_STM32_SPI2=y
CONFIG_STM32_SPI2_DMA=y
CONFIG_STM32_SPI2_DMA_BUFFER=2048
CONFIG_STM32_TIM8=y
CONFIG_STM32_USART2=y
CONFIG_STM32_USART_BREAKS=y
CONFIG_STM32_WWDG=y
CONFIG_SYSTEM_NSH=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_USART2_BAUD=57600
CONFIG_USART2_RXBUFSIZE=600
CONFIG_USART2_SERIAL_CONSOLE=y
CONFIG_USART2_TXBUFSIZE=1100
CONFIG_USEC_PER_TICK=1000
@@ -0,0 +1,134 @@
/****************************************************************************
* nuttx-config/scripts/canbootloader_script.ld
*
* Copyright (C) 2015 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/* The STM32F412 has 1M of FLASH beginning at address 0x0800:0000 and
* 256Kb of SRAM. SRAM is split up into three blocks:
*
* 1) 112Kb of SRAM beginning at address 0x2000:0000
* 2) 16Kb of SRAM beginning at address 0x2001:c000
* 3) 64Kb of SRAM beginning at address 0x2002:0000
* 4) 64Kb of TCM SRAM beginning at address 0x1000:0000
*
* When booting from FLASH, FLASH memory is aliased to address 0x0000:0000
* where the code expects to begin execution by jumping to the entry point in
* the 0x0800:0000 address range.
*
* The first 0x10000 of flash is reserved for the bootloader.
*/
MEMORY
{
flash (rx) : ORIGIN = 0x08000000, LENGTH = 32K
sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K
}
OUTPUT_ARCH(arm)
ENTRY(__start) /* treat __start as the anchor for dead code stripping */
EXTERN(_vectors) /* force the vectors to be included in the output */
/*
* Ensure that abort() is present in the final object. The exception handling
* code pulled in by libgcc.a requires it (and that code cannot be easily avoided).
*/
EXTERN(abort)
SECTIONS
{
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
*(.text .text.*)
*(.fixup)
*(.gnu.warning)
*(.rodata .rodata.*)
*(.gnu.linkonce.t.*)
*(.got)
*(.gcc_except_table)
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
/*
* Init functions (static constructors and the like)
*/
.init_section : {
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
.ARM.extab : {
*(.ARM.extab*)
} > flash
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
.data : {
_sdata = ABSOLUTE(.);
*(.data .data.*)
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
.bss : {
_sbss = ABSOLUTE(.);
*(.bss .bss.*)
*(.gnu.linkonce.b.*)
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
.stabstr 0 : { *(.stabstr) }
.stab.excl 0 : { *(.stab.excl) }
.stab.exclstr 0 : { *(.stab.exclstr) }
.stab.index 0 : { *(.stab.index) }
.stab.indexstr 0 : { *(.stab.indexstr) }
.comment 0 : { *(.comment) }
.debug_abbrev 0 : { *(.debug_abbrev) }
.debug_info 0 : { *(.debug_info) }
.debug_line 0 : { *(.debug_line) }
.debug_pubnames 0 : { *(.debug_pubnames) }
.debug_aranges 0 : { *(.debug_aranges) }
}
@@ -0,0 +1,146 @@
/****************************************************************************
* scripts/ld.script
*
* Copyright (C) 2011 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/* The STM32F412 has 1M of FLASH beginning at address 0x0800:0000 and
* 256Kb of SRAM. SRAM is split up into three blocks:
*
* 1) 112Kb of SRAM beginning at address 0x2000:0000
* 2) 16Kb of SRAM beginning at address 0x2001:c000
* 3) 64Kb of SRAM beginning at address 0x2002:0000
* 4) 64Kb of TCM SRAM beginning at address 0x1000:0000
*
* When booting from FLASH, FLASH memory is aliased to address 0x0000:0000
* where the code expects to begin execution by jumping to the entry point in
* the 0x0800:0000 address range.
*
* The first 0x10000 of flash is reserved for the bootloader.
*/
MEMORY
{
flash (rx) : ORIGIN = 0x08010000, LENGTH = 928K
sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K
}
OUTPUT_ARCH(arm)
ENTRY(__start) /* treat __start as the anchor for dead code stripping */
EXTERN(_vectors) /* force the vectors to be included in the output */
/*
* Ensure that abort() is present in the final object. The exception handling
* code pulled in by libgcc.a requires it (and that code cannot be easily avoided).
*/
EXTERN(abort)
EXTERN(_bootdelay_signature)
SECTIONS
{
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
. = ALIGN(8);
/*
* This section positions the app_descriptor_t used
* by the make_can_boot_descriptor.py tool to set
* the application image's descriptor so that the
* uavcan bootloader has the ability to validate the
* image crc, size etc
*/
KEEP(*(.app_descriptor))
*(.text .text.*)
*(.fixup)
*(.gnu.warning)
*(.rodata .rodata.*)
*(.gnu.linkonce.t.*)
*(.got)
*(.gcc_except_table)
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
/*
* Init functions (static constructors and the like)
*/
.init_section : {
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
.ARM.extab : {
*(.ARM.extab*)
} > flash
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
.data : {
_sdata = ABSOLUTE(.);
*(.data .data.*)
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
.bss : {
_sbss = ABSOLUTE(.);
*(.bss .bss.*)
*(.gnu.linkonce.b.*)
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
.stabstr 0 : { *(.stabstr) }
.stab.excl 0 : { *(.stab.excl) }
.stab.exclstr 0 : { *(.stab.exclstr) }
.stab.index 0 : { *(.stab.index) }
.stab.indexstr 0 : { *(.stab.indexstr) }
.comment 0 : { *(.comment) }
.debug_abbrev 0 : { *(.debug_abbrev) }
.debug_info 0 : { *(.debug_info) }
.debug_line 0 : { *(.debug_line) }
.debug_pubnames 0 : { *(.debug_pubnames) }
.debug_aranges 0 : { *(.debug_aranges) }
}
+65
View File
@@ -0,0 +1,65 @@
############################################################################
#
# Copyright (c) 2020 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
# are met:
#
# 1. Redistributions of source code must retain the above copyright
# notice, this list of conditions and the following disclaimer.
# 2. Redistributions in binary form must reproduce the above copyright
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
if("${PX4_BOARD_LABEL}" STREQUAL "canbootloader")
add_library(drivers_board
boot_config.h
boot.c
led.c
)
target_link_libraries(drivers_board
PRIVATE
nuttx_arch
nuttx_drivers
canbootloader
)
target_include_directories(drivers_board PRIVATE ${PX4_SOURCE_DIR}/platforms/nuttx/src/canbootloader)
else()
add_library(drivers_board
can.c
init.c
led.c
spi.cpp
)
target_link_libraries(drivers_board
PRIVATE
arch_spi
drivers__led # drv_led_start
nuttx_arch
nuttx_drivers
px4_layer
)
endif()
+95
View File
@@ -0,0 +1,95 @@
/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file board_config.h
*
* board internal definitions
*/
#pragma once
#include <px4_platform_common/px4_config.h>
#include <nuttx/compiler.h>
#include <stdint.h>
/* CAN Silent mode control */
#define GPIO_CAN1_SILENT_S0 /* PB11 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN11)
/* CAN termination software control */
#define GPIO_CAN1_TERMINATION /* PB13 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN13)
#define GPIO_CAN_TERM GPIO_CAN1_TERMINATION
/* Boot config */
#define GPIO_BOOT_CONFIG /* PC15 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTC|GPIO_PIN15|GPIO_EXTI)
/* LEDs are driven with open drain to support Anode to 5V or 3.3V */
#define GPIO_TIM1_CH1 /* PA8 */ (GPIO_TIM1_CH1_1|GPIO_OPENDRAIN|GPIO_SPEED_2MHz)
#define GPIO_TIM1_CH2 /* PA9 */ (GPIO_TIM1_CH2_1|GPIO_OPENDRAIN|GPIO_SPEED_2MHz)
#define GPIO_TIM1_CH3 /* PA10 */ (GPIO_TIM1_CH3_1|GPIO_OPENDRAIN|GPIO_SPEED_2MHz)
#define BROADCOM_AFBR_S50_S2PI_SPI_BUS 2
#define BROADCOM_AFBR_S50_S2PI_CS /* PB12 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN12)
#define BROADCOM_AFBR_S50_S2PI_IRQ /* PB4 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN4|GPIO_EXTI)
#define BROADCOM_AFBR_S50_S2PI_CLK /* PB10 */ GPIO_SPI2_SCK_1
#define BROADCOM_AFBR_S50_S2PI_MOSI /* PB15 */ GPIO_SPI2_MOSI_1
#define BROADCOM_AFBR_S50_S2PI_MISO /* PB14 */ GPIO_SPI2_MISO_1
#define FLASH_BASED_PARAMS
/* High-resolution timer */
#define HRT_TIMER 3 /* use timer 3 for the HRT */
#define HRT_TIMER_CHANNEL 4 /* use capture/compare channel 4 */
#define PX4_GPIO_INIT_LIST { \
GPIO_BOOT_CONFIG, \
GPIO_CAN1_TX, \
GPIO_CAN1_RX, \
GPIO_CAN1_SILENT_S0, \
GPIO_CAN1_TERMINATION, \
}
__BEGIN_DECLS
#define BOARD_HAS_N_S_RGB_LED 1
#define BOARD_MAX_LEDS BOARD_HAS_N_S_RGB_LED
#ifndef __ASSEMBLY__
extern void stm32_spiinitialize(void);
#include <px4_platform_common/board_common.h>
#endif /* __ASSEMBLY__ */
__END_DECLS
+188
View File
@@ -0,0 +1,188 @@
/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
* Author: Ben Dyer <ben_dyer@mac.com>
* Pavel Kirienko <pavel.kirienko@zubax.com>
* David Sidrane <david_s5@nscdg.com>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/****************************************************************************
* Included Files
****************************************************************************/
#include <px4_config.h>
#include <stdint.h>
#include "boot_config.h"
#include "board.h"
#include <debug.h>
#include <string.h>
#include <arch/board/board.h>
#include <nuttx/board.h>
#include "led.h"
/************************************************************************************
* Name: stm32_boardinitialize
*
* Description:
* All STM32 architectures must provide the following entry point. This entry point
* is called early in the initialization -- after all memory has been configured
* and mapped but before any devices have been initialized.
*
************************************************************************************/
__EXPORT void stm32_boardinitialize(void)
{
putreg32(getreg32(STM32_RCC_APB1ENR) | RCC_APB1ENR_CAN1EN, STM32_RCC_APB1ENR);
stm32_configgpio(GPIO_CAN1_RX);
stm32_configgpio(GPIO_CAN1_TX);
stm32_configgpio(GPIO_CAN1_SILENT_S0);
stm32_configgpio(GPIO_CAN1_TERMINATION);
putreg32(getreg32(STM32_RCC_APB1RSTR) | RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
putreg32(getreg32(STM32_RCC_APB1RSTR) & ~RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
#if defined(OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO)
stm32_configgpio(GPIO_GETNODEINFO_JUMPER);
#endif
}
/************************************************************************************
* Name: board_deinitialize
*
* Description:
* This function is called by the bootloader code prior to booting
* the application. Is should place the HW into an benign initialized state.
*
************************************************************************************/
void board_deinitialize(void)
{
putreg32(getreg32(STM32_RCC_APB1RSTR) | RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
}
/****************************************************************************
* Name: board_get_product_name
*
* Description:
* Called to retrieve the product name. The returned value is a assumed
* to be written to a pascal style string that will be length prefixed
* and not null terminated
*
* Input Parameters:
* product_name - A pointer to a buffer to write the name.
* maxlen - The maximum number of charter that can be written
*
* Returned Value:
* The length of characters written to the buffer.
*
****************************************************************************/
uint8_t board_get_product_name(uint8_t *product_name, size_t maxlen)
{
DEBUGASSERT(maxlen > UAVCAN_STRLEN(HW_UAVCAN_NAME));
memcpy(product_name, HW_UAVCAN_NAME, UAVCAN_STRLEN(HW_UAVCAN_NAME));
return UAVCAN_STRLEN(HW_UAVCAN_NAME);
}
/****************************************************************************
* Name: board_get_hardware_version
*
* Description:
* Called to retrieve the hardware version information. The function
* will first initialize the the callers struct to all zeros.
*
* Input Parameters:
* hw_version - A pointer to a uavcan_hardwareversion_t.
*
* Returned Value:
* Length of the unique_id
*
****************************************************************************/
size_t board_get_hardware_version(uavcan_HardwareVersion_t *hw_version)
{
memset(hw_version, 0, sizeof(uavcan_HardwareVersion_t));
hw_version->major = HW_VERSION_MAJOR;
hw_version->minor = HW_VERSION_MINOR;
return board_get_mfguid(*(mfguid_t *) hw_version->unique_id);
}
/****************************************************************************
* Name: board_indicate
*
* Description:
* Provides User feedback to indicate the state of the bootloader
* on board specific hardware.
*
* Input Parameters:
* indication - A member of the uiindication_t
*
* Returned Value:
* None
*
****************************************************************************/
#define led(n, code, r , g , b, h) {.red = (r),.green = (g), .blue = (b),.hz = (h)}
typedef begin_packed_struct struct led_t {
uint8_t red;
uint8_t green;
uint8_t blue;
uint8_t hz;
} end_packed_struct led_t;
static const led_t i2l[] = {
led(0, off, 0, 0, 0, 0),
led(1, reset, 128, 128, 128, 30),
led(2, autobaud_start, 0, 128, 0, 1),
led(3, autobaud_end, 0, 128, 0, 2),
led(4, allocation_start, 0, 0, 64, 2),
led(5, allocation_end, 0, 128, 64, 3),
led(6, fw_update_start, 32, 128, 64, 3),
led(7, fw_update_erase_fail, 32, 128, 32, 3),
led(8, fw_update_invalid_response, 64, 0, 0, 1),
led(9, fw_update_timeout, 64, 0, 0, 2),
led(a, fw_update_invalid_crc, 64, 0, 0, 4),
led(b, jump_to_app, 0, 128, 0, 10),
};
void board_indicate(uiindication_t indication)
{
rgb_led(i2l[indication].red,
i2l[indication].green,
i2l[indication].blue,
i2l[indication].hz);
}
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/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/*
* @file boot_config.h
*
* bootloader definitions that configures the behavior and options
* of the Boot loader
* This file is relies on the parent folder's boot_config.h file and defines
* different usages of the hardware for bootloading
*/
#pragma once
/************************************************************************************
* Included Files
************************************************************************************/
/* Bring in the board_config.h definitions
* todo:make this be pulled in from a targed's build
* files in nuttx*/
#include "board_config.h"
#include "uavcan.h"
#include <nuttx/compiler.h>
#include <stdint.h>
#include <stm32_flash.h>
/****************************************************************************
* Pre-processor Definitions
****************************************************************************/
#define OPT_PREFERRED_NODE_ID ANY_NODE_ID
//todo:wrap OPT_x in in ifdefs for command line definitions
#define OPT_TBOOT_MS 3000
#define OPT_NODE_STATUS_RATE_MS 800
#define OPT_NODE_INFO_RATE_MS 50
#define OPT_BL_NUMBER_TIMERS 7
/*
* This Option set is set to 1 ensure a provider of firmware has an
* opportunity update the node's firmware.
* This Option is the default policy and can be overridden by
* a jumper
* When this Policy is set, the node will ignore tboot and
* wait indefinitely for a GetNodeInfo request before booting.
*
* OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO_INVERT is used to allow
* the polarity of the jumper to be True Active
*
* wait OPT_WAIT_FOR_GETNODEINFO OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO
* Jumper
* yes 1 0 x
* yes 1 1 Active
* no 1 1 Not Active
* no 0 0 X
* yes 0 1 Active
* no 0 1 Not Active
*
*/
#define OPT_WAIT_FOR_GETNODEINFO 0
#define OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO 1
#define OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO_INVERT 1
#define OPT_ENABLE_WD 1
#define OPT_RESTART_TIMEOUT_MS 20000
/* Reserved for the Booloader */
#define OPT_BOOTLOADER_SIZE_IN_K (1024*64)
/* Reserved for the application out of the total
* system flash minus the BOOTLOADER_SIZE_IN_K
*/
#define OPT_APPLICATION_RESERVER_IN_K 0
#define OPT_APPLICATION_IMAGE_OFFSET OPT_BOOTLOADER_SIZE_IN_K
#define OPT_APPLICATION_IMAGE_LENGTH (FLASH_SIZE-(OPT_BOOTLOADER_SIZE_IN_K+OPT_APPLICATION_RESERVER_IN_K))
#define FLASH_BASE STM32_FLASH_BASE
#define FLASH_SIZE STM32_FLASH_SIZE
#define APPLICATION_LOAD_ADDRESS (FLASH_BASE + OPT_APPLICATION_IMAGE_OFFSET)
#define APPLICATION_SIZE (FLASH_SIZE-OPT_APPLICATION_IMAGE_OFFSET)
#define APPLICATION_LAST_8BIT_ADDRRESS ((uint8_t *)((APPLICATION_LOAD_ADDRESS+APPLICATION_SIZE)-sizeof(uint8_t)))
#define APPLICATION_LAST_32BIT_ADDRRESS ((uint32_t *)((APPLICATION_LOAD_ADDRESS+APPLICATION_SIZE)-sizeof(uint32_t)))
#define APPLICATION_LAST_64BIT_ADDRRESS ((uint64_t *)((APPLICATION_LOAD_ADDRESS+APPLICATION_SIZE)-sizeof(uint64_t)))
/* If this board uses big flash that have large sectors */
#define OPT_USE_YIELD
/* Bootloader Option*****************************************************************
*
*/
#define GPIO_GETNODEINFO_JUMPER (GPIO_BOOT_CONFIG & ~GPIO_EXTI)
+130
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/****************************************************************************
*
* Copyright (C) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file can.c
*
* Board-specific CAN functions.
*/
/************************************************************************************
* Included Files
************************************************************************************/
#include <px4_platform_common/px4_config.h>
#include <errno.h>
#include <debug.h>
#include <nuttx/can/can.h>
#include <arch/board/board.h>
#include "chip.h"
#include "arm_internal.h"
#include "stm32.h"
#include "stm32_can.h"
#include "board_config.h"
#ifdef CONFIG_CAN
/************************************************************************************
* Pre-processor Definitions
************************************************************************************/
/* Configuration ********************************************************************/
#if defined(CONFIG_STM32_CAN1) && defined(CONFIG_STM32_CAN2)
# warning "Both CAN1 and CAN2 are enabled. Assuming only CAN1."
# undef CONFIG_STM32_CAN2
#endif
#ifdef CONFIG_STM32_CAN1
# define CAN_PORT 1
#else
# define CAN_PORT 2
#endif
/************************************************************************************
* Private Functions
************************************************************************************/
/************************************************************************************
* Public Functions
************************************************************************************/
int can_devinit(void);
/************************************************************************************
* Name: can_devinit
*
* Description:
* All STM32 architectures must provide the following interface to work with
* examples/can.
*
************************************************************************************/
int can_devinit(void)
{
static bool initialized = false;
struct can_dev_s *can;
int ret;
/* Check if we have already initialized */
if (!initialized) {
/* Call stm32_caninitialize() to get an instance of the CAN interface */
can = stm32_caninitialize(CAN_PORT);
if (can == NULL) {
canerr("ERROR: Failed to get CAN interface\n");
return -ENODEV;
}
/* Register the CAN driver at "/dev/can0" */
ret = can_register("/dev/can0", can);
if (ret < 0) {
canerr("ERROR: can_register failed: %d\n", ret);
return ret;
}
/* Now we are initialized */
initialized = true;
}
return OK;
}
#endif
+147
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/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file init.c
*
* board specific early startup code. This file implements the
* board_app_initialize() function that is called early by nsh during startup.
*
* Code here is run before the rcS script is invoked; it should start required
* subsystems and perform board-specific initialization.
*/
#include <px4_platform_common/px4_config.h>
#include <px4_platform_common/tasks.h>
#include <stdbool.h>
#include <stdio.h>
#include <string.h>
#include <debug.h>
#include <errno.h>
#include <syslog.h>
#include <nuttx/board.h>
#include <stm32.h>
#include "board_config.h"
#include "led.h"
#include <stm32_uart.h>
#include <arch/board/board.h>
#include <drivers/drv_hrt.h>
#include <drivers/drv_board_led.h>
#include <drivers/drv_watchdog.h>
#include <systemlib/px4_macros.h>
#include <px4_platform_common/init.h>
#include <px4_platform/gpio.h>
# if defined(FLASH_BASED_PARAMS)
# include <parameters/flashparams/flashfs.h>
#endif
/************************************************************************************
* Name: stm32_boardinitialize
*
* Description:
* All STM32 architectures must provide the following entry point. This entry point
* is called early in the initialization -- after all memory has been configured
* and mapped but before any devices have been initialized.
*
************************************************************************************/
__EXPORT void stm32_boardinitialize(void)
{
watchdog_init();
/* configure pins */
const uint32_t gpio[] = PX4_GPIO_INIT_LIST;
px4_gpio_init(gpio, arraySize(gpio));
// Configure SPI all interfaces GPIO & enable power.
stm32_spiinitialize();
}
/****************************************************************************
* Name: board_app_initialize
*
* Description:
* Perform application specific initialization. This function is never
* called directly from application code, but only indirectly via the
* (non-standard) boardctl() interface using the command BOARDIOC_INIT.
*
* Input Parameters:
* arg - The boardctl() argument is passed to the board_app_initialize()
* implementation without modification. The argument has no
* meaning to NuttX; the meaning of the argument is a contract
* between the board-specific initalization logic and the the
* matching application logic. The value cold be such things as a
* mode enumeration value, a set of DIP switch switch settings, a
* pointer to configuration data read from a file or serial FLASH,
* or whatever you would like to do with it. Every implementation
* should accept zero/NULL as a default configuration.
*
* Returned Value:
* Zero (OK) is returned on success; a negated errno value is returned on
* any failure to indicate the nature of the failure.
*
****************************************************************************/
__EXPORT int board_app_initialize(uintptr_t arg)
{
px4_platform_init();
#if defined(FLASH_BASED_PARAMS)
static sector_descriptor_t params_sector_map[] = {
{2, 16 * 1024, 0x08008000},
{3, 16 * 1024, 0x0800C000},
{0, 0, 0},
};
/* Initialize the flashfs layer to use heap allocated memory */
int result = parameter_flashfs_init(params_sector_map, NULL, 0);
if (result != OK) {
syslog(LOG_ERR, "[boot] FAILED to init params in FLASH %d\n", result);
}
#endif // FLASH_BASED_PARAMS
/* Configure the HW based on the manifest */
//px4_platform_configure();
return OK;
}
+124
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@@ -0,0 +1,124 @@
/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file led.c
*
* LED backend.
*/
#include <px4_platform_common/px4_config.h>
#include <stdbool.h>
#include "chip.h"
#include "stm32_gpio.h"
#include "board_config.h"
#include <nuttx/board.h>
#include <arch/board/board.h>
#include "led.h"
#define TMR_BASE STM32_TIM1_BASE
#define TMR_FREQUENCY STM32_APB2_TIM1_CLKIN
#define TMR_REG(o) (TMR_BASE+(o))
void rgb_led(int r, int g, int b, int freqs)
{
long fosc = TMR_FREQUENCY;
long prescale = 2048;
long p1s = fosc / prescale;
long p0p5s = p1s / 2;
uint16_t val;
static bool once = 0;
if (!once) {
once = 1;
/* Enabel Clock to Block */
modifyreg32(STM32_RCC_APB2ENR, 0, RCC_APB2ENR_TIM1EN);
/* Reload */
val = getreg16(TMR_REG(STM32_BTIM_EGR_OFFSET));
val |= ATIM_EGR_UG;
putreg16(val, TMR_REG(STM32_BTIM_EGR_OFFSET));
/* Set Prescaler STM32_TIM_SETCLOCK */
putreg16(prescale, TMR_REG(STM32_BTIM_PSC_OFFSET));
/* Enable STM32_TIM_SETMODE*/
putreg16(ATIM_CR1_CEN | ATIM_CR1_ARPE, TMR_REG(STM32_BTIM_CR1_OFFSET));
putreg16((ATIM_CCMR_MODE_PWM1 << ATIM_CCMR1_OC1M_SHIFT) | ATIM_CCMR1_OC1PE |
(ATIM_CCMR_MODE_PWM1 << ATIM_CCMR1_OC2M_SHIFT) | ATIM_CCMR1_OC2PE, TMR_REG(STM32_GTIM_CCMR1_OFFSET));
putreg16((ATIM_CCMR_MODE_PWM1 << ATIM_CCMR2_OC3M_SHIFT) | ATIM_CCMR2_OC3PE, TMR_REG(STM32_GTIM_CCMR2_OFFSET));
putreg16(ATIM_CCER_CC3E | ATIM_CCER_CC3P |
ATIM_CCER_CC2E | ATIM_CCER_CC2P |
ATIM_CCER_CC1E | ATIM_CCER_CC1P, TMR_REG(STM32_GTIM_CCER_OFFSET));
stm32_configgpio(GPIO_TIM1_CH1);
stm32_configgpio(GPIO_TIM1_CH2);
stm32_configgpio(GPIO_TIM1_CH3);
/* master output enable = on */
putreg16(ATIM_BDTR_MOE, (TMR_REG(STM32_ATIM_BDTR_OFFSET)));
}
long p = freqs == 0 ? p1s : p1s / freqs;
putreg32(p, TMR_REG(STM32_BTIM_ARR_OFFSET));
p = freqs == 0 ? p1s + 1 : p0p5s / freqs;
putreg32((r * p) / 255, TMR_REG(STM32_GTIM_CCR1_OFFSET));
putreg32((g * p) / 255, TMR_REG(STM32_GTIM_CCR2_OFFSET));
putreg32((b * p) / 255, TMR_REG(STM32_GTIM_CCR3_OFFSET));
val = getreg16(TMR_REG(STM32_BTIM_CR1_OFFSET));
if (freqs == 0) {
val &= ~ATIM_CR1_CEN;
} else {
val |= ATIM_CR1_CEN;
}
putreg16(val, TMR_REG(STM32_BTIM_CR1_OFFSET));
}
+37
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@@ -0,0 +1,37 @@
/****************************************************************************
*
* Copyright (C) 2015 PX4 Development Team. All rights reserved.
* Author: David Sidrane<david_s5@nscdg.com>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
__BEGIN_DECLS
void rgb_led(int r, int g, int b, int freqs);
__END_DECLS
+48
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@@ -0,0 +1,48 @@
/****************************************************************************
*
* Copyright (C) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include <px4_arch/spi_hw_description.h>
#include <drivers/drv_sensor.h>
#include <nuttx/spi/spi.h>
constexpr px4_spi_bus_t px4_spi_buses[SPI_BUS_MAX_BUS_ITEMS] = {
initSPIBus(SPI::Bus::SPI1, {
initSPIDevice(DRV_IMU_DEVTYPE_IIM42653, SPI::CS{GPIO::PortB, GPIO::Pin0}, SPI::DRDY{GPIO::PortB, GPIO::Pin1}),
initSPIDevice(DRV_FLOW_DEVTYPE_PAA3905, SPI::CS{GPIO::PortB, GPIO::Pin5}, SPI::DRDY{GPIO::PortB, GPIO::Pin2}),
}),
initSPIBus(SPI::Bus::SPI2, {
initSPIDevice(DRV_DEVTYPE_UNUSED, SPI::CS{GPIO::PortB, GPIO::Pin12}, SPI::DRDY{GPIO::PortB, GPIO::Pin4}),
}),
};
static constexpr bool unused = validateSPIConfig(px4_spi_buses);
@@ -0,0 +1,17 @@
# UAVCAN boot loadable Module ID
set(uavcanblid_sw_version_major ${PX4_VERSION_MAJOR})
set(uavcanblid_sw_version_minor ${PX4_VERSION_MINOR})
add_definitions(
-DAPP_VERSION_MAJOR=${uavcanblid_sw_version_major}
-DAPP_VERSION_MINOR=${uavcanblid_sw_version_minor}
)
set(uavcanblid_hw_version_major 0)
set(uavcanblid_hw_version_minor 88)
set(uavcanblid_name "\"org.ark.can-flow-mr\"")
add_definitions(
-DHW_UAVCAN_NAME=${uavcanblid_name}
-DHW_VERSION_MAJOR=${uavcanblid_hw_version_major}
-DHW_VERSION_MINOR=${uavcanblid_hw_version_minor}
)
@@ -4,6 +4,7 @@
#------------------------------------------------------------------------------
param set-default IMU_GYRO_RATEMAX 1000
param set-default SENS_FLOW_RATE 150
param set-default SENS_IMU_CLPNOTI 0
# Internal SPI
+1 -1
View File
@@ -4,7 +4,7 @@
#------------------------------------------------------------------------------
param set-default CBRK_IO_SAFETY 0
param set-default MBE_ENABLE 1
param set-default MBE_ENABLE 0
param set-default SENS_IMU_CLPNOTI 0
safety_button start
@@ -7,7 +7,7 @@ param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_SUB_MBD 1
param set-default CANNODE_SUB_RTCM 1
param set-default GPS_1_GNSS 63
param set-default MBE_ENABLE 1
param set-default MBE_ENABLE 0
param set-default SENS_IMU_CLPNOTI 0
safety_button start
@@ -3,6 +3,7 @@
# board specific defaults
#------------------------------------------------------------------------------
param set-default MBE_ENABLE 0
param set-default SENS_IMU_CLPNOTI 0
pwm_out start
@@ -3,6 +3,8 @@
# board specific defaults
#------------------------------------------------------------------------------
param set-default EKF2_MULTI_IMU 0
# Mavlink ethernet (CFG 1000)
param set-default MAV_2_CONFIG 1000
param set-default MAV_2_BROADCAST 1
@@ -17,6 +19,7 @@ param set-default SENS_EN_INA228 0
param set-default SENS_EN_INA226 1
param set-default SENS_EN_THERMAL 1
param set-default SENS_IMU_MODE 1
param set-default SENS_IMU_TEMP 10.0
#param set-default SENS_IMU_TEMP_FF 0.0
#param set-default SENS_IMU_TEMP_I 0.025
@@ -145,10 +145,11 @@ CONFIG_NETDB_DNSCLIENT=y
CONFIG_NETDB_DNSCLIENT_ENTRIES=8
CONFIG_NETDB_DNSSERVER_NOADDR=y
CONFIG_NETDEV_PHY_IOCTL=y
CONFIG_NETINIT_DHCPC=y
CONFIG_NETMAN_FALLBACK_IPADDR=0xC0A80004
CONFIG_NETINIT_DNS=y
CONFIG_NETINIT_DNSIPADDR=0xA290AFE
CONFIG_NETINIT_DRIPADDR=0xA290AFE
CONFIG_NETINIT_IPADDR=0xC0A80004
CONFIG_NETINIT_DNSIPADDR=0xC0A800FE
CONFIG_NETINIT_DRIPADDR=0xC0A80001
CONFIG_NETINIT_MONITOR=y
CONFIG_NETINIT_THREAD=y
CONFIG_NETINIT_THREAD_PRIORITY=49
+6 -1
View File
@@ -150,8 +150,13 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(6);
up_mdelay(100);
}
}
+2
View File
@@ -18,6 +18,7 @@ CONFIG_DRIVERS_IMU_INVENSENSE_IIM42653=y
CONFIG_DRIVERS_IMU_MURATA_SCH16T=y
CONFIG_COMMON_LIGHT=y
CONFIG_COMMON_MAGNETOMETER=y
CONFIG_DRIVERS_OSD_MSP_OSD=y
CONFIG_DRIVERS_PWM_OUT=y
CONFIG_COMMON_RC=y
CONFIG_DRIVERS_UAVCAN=y
@@ -35,6 +36,7 @@ CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y
CONFIG_MODULES_LAND_DETECTOR=y
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+3
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@@ -176,6 +176,9 @@
#define BOARD_BATTERY1_V_DIV (21.0f) // (20k + 1k) / 1k = 21
#define BOARD_BATTERY_ADC_VOLTAGE_FILTER_S 0.075f
#define BOARD_BATTERY_ADC_CURRENT_FILTER_S 0.125f
#define ADC_SCALED_PAYLOAD_SENSE ADC_SCALED_12V_CHANNEL
/* HW has to large of R termination on ADC todo:change when HW value is chosen */
+6 -1
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@@ -145,8 +145,13 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(6);
up_mdelay(100);
}
}
+2 -1
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@@ -32,10 +32,11 @@ then
param set-default SENS_TEMP_ID 2490378
fi
param set-default EKF2_MULTI_IMU 2
param set-default EKF2_MULTI_IMU 0
param set-default EKF2_OF_CTRL 1
param set-default EKF2_OF_N_MIN 0.05
param set-default EKF2_RNG_A_HMAX 25
param set-default EKF2_RNG_QLTY_T 0.1
param set-default SENS_FLOW_RATE 150
param set-default SENS_IMU_MODE 1
@@ -32,7 +32,7 @@ CONFIG_BOARD_LOOPSPERMSEC=95150
CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_CDCACM=y
CONFIG_CDCACM_IFLOWCONTROL=y
CONFIG_CDCACM_PRODUCTID=0x0039
CONFIG_CDCACM_PRODUCTID=0x003A
CONFIG_CDCACM_PRODUCTSTR="ARK BL Pi6X.x"
CONFIG_CDCACM_RXBUFSIZE=600
CONFIG_CDCACM_TXBUFSIZE=12000
+1 -1
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@@ -76,7 +76,7 @@ CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_BUILTIN=y
CONFIG_CDCACM=y
CONFIG_CDCACM_IFLOWCONTROL=y
CONFIG_CDCACM_PRODUCTID=0x0039
CONFIG_CDCACM_PRODUCTID=0x003A
CONFIG_CDCACM_PRODUCTSTR="ARK Pi6X.x"
CONFIG_CDCACM_RXBUFSIZE=600
CONFIG_CDCACM_TXBUFSIZE=12000
+6 -1
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@@ -141,8 +141,13 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(6);
up_mdelay(100);
}
}
@@ -6,7 +6,7 @@
param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_SUB_MBD 1
param set-default CANNODE_SUB_RTCM 1
param set-default MBE_ENABLE 1
param set-default MBE_ENABLE 0
param set-default SENS_IMU_CLPNOTI 0
safety_button start
@@ -0,0 +1,5 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT=""
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_BOOTLOADERS=y
+13
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@@ -0,0 +1,13 @@
{
"board_id": 86,
"magic": "PX4FWv1",
"description": "Firmware for the ARK Teseo GPS board",
"image": "",
"build_time": 0,
"summary": "ARKTESEOGPS",
"version": "0.1",
"image_size": 0,
"image_maxsize": 2080768,
"git_identity": "",
"board_revision": 0
}
@@ -0,0 +1,14 @@
#!/bin/sh
#
# board specific defaults
#------------------------------------------------------------------------------
param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_SUB_MBD 1
param set-default CANNODE_SUB_RTCM 1
param set-default MBE_ENABLE 0
param set-default SENS_IMU_CLPNOTI 0
tone_alarm start
ekf2 start

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