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228 Commits

Author SHA1 Message Date
Daniel Agar 3fff512ec0 new standalone drivers/system_power (split out of adc)
- system_power portion of drivers/adc split into a new standalone module (drivers/system_power)
 - additional availability flags added to system_power.msg so we know what boards even support (previously certain flags were faked if not available)
 - drivers/system_power scheduled at minimum rate by default, but now also scheduled immediately on any relevant GPIO events
 - now instead of running at 100 Hz with heavily reduced logging we can run at a minimal rate, log at full rate, and catch relevant changes immediately
2021-01-16 14:20:54 -05:00
Silvan Fuhrer cee4016665 Preflight checks: Airspeed checks update
-check for valid airspeed_validated (declared valid plus updated less than 1s ago)
-added param (COM_ARM_ARSP_EN) to enable/disable check for max airspeed for arming set max
airspeed limit to half of stall airspeed

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-16 10:26:55 -05:00
Can Berk Durmus ba9611621d Retune Typhoon H480 PID 2021-01-16 09:32:09 +01:00
David Sidrane 1c0ed74d6a platforms/nuttx/NuttX/nuttx net backports 2021-01-15 11:44:21 -08:00
Beat Küng ade3871bee adc: add support for multiple sensor voltage channels 2021-01-15 10:57:20 -05:00
Beat Küng e2337a34eb system_power: add comp_5v_valid and can1_gps1_5v_valid
And fill it in from the v5x GPIO expander.
2021-01-15 10:57:20 -05:00
Beat Küng 704a82aaa6 gpio: extend support for /dev/gp* GPIO's
Note that there's a small CLI interface change.
2021-01-15 10:57:20 -05:00
Beat Küng 88fe047556 px4/v5x: enable mcp23009 GPIO driver 2021-01-15 10:57:20 -05:00
Beat Küng 3e4b8763a5 nuttx: add mcp23009 gpio driver 2021-01-15 10:57:20 -05:00
Beat Küng e1983381e7 rcS: add SYS_PARAM_VER to param reset_all exception list
Avoids an extra reboot when resetting the airframe
2021-01-15 10:57:20 -05:00
Matej Frančeškin ba6a8080ea mavlink: don't respond to MAV_CMD_REQUEST_MESSAGE if component doesn't match
PX4 is responding with NACK to MAV_CMD_REQUEST_MESSAGE from a GCS to
payload-manager which confuses a GCS.
PX4 shouldn't respond to commands that are not broadcasted or specificaly
addressed to it.
2021-01-15 10:57:20 -05:00
Beat Küng 26e8c231b0 v5x,v6x: move mtd_caldata after mtd_id partition
to avoid losing factory calibration params on existing setups
2021-01-15 10:57:20 -05:00
Lorenz Meier a282f3df8d CLI test: Disable by default on NuttX
First target is to enable this for POSIX tests and then later to roll them out to NuttX.
2021-01-15 10:57:20 -05:00
Lorenz Meier 03e9e10847 Add CLI tests for basic soak testing
This is in no way a complete test suite but is intended as a starting point to get minimal
test coverage for CLI handling tests in. This is necessary to QA the CLI handling
(e.g. removal of commands) and to ensure that we are exercising these code paths in
stack check and alike tests.
2021-01-15 10:57:20 -05:00
Julian Oes 5ae5c03c66 mavlink: handle param4/5 from mission_item_int
It turns out that we did not properly handle param4 and param5 if they
are transferred using mission_item_int if the frame is
MAV_FRAME_MISSION.
2021-01-15 10:57:20 -05:00
Beat Küng 12ebbd995d bmp388: wait a bit longer to schedule first cycle after reset 2021-01-15 10:57:20 -05:00
Beat Küng 529c3112ac bmp388: quiet if startup fails (no sensor on bus) 2021-01-15 10:57:20 -05:00
David Sidrane 1e7dfe227a stm32_common:board_hw_rev_ver Use Analog resistor detection
When the VER_DRIVE and REV_DRIVE are the same GPIO
   we need to use Analog detection.
2021-01-15 10:57:20 -05:00
Jakub Kákona b87dd317d4 airframes: add new airframe for ThunderFly TF-G2 autogyro (#16551)
Co-authored-by: Roman Dvorak <romandvorak@mlab.cz>
2021-01-15 13:54:17 +01:00
Thomas df41c99b61 make failsafe handling consistent over all VTOL types 2021-01-15 09:19:07 +03:00
Thomas 38e46ff341 Rename VtolAttitudeControl::abort_front_transition(const char *reason) to VtolAttitudeControl::quadchute(const char *reason) 2021-01-15 09:19:07 +03:00
Thomas Stauber 40fbfdc054 Undo make format change
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2021-01-15 09:19:07 +03:00
Thomas 83ddb77a5f delete excess empty lines 2021-01-15 09:19:07 +03:00
Thomas b90fafd5cd Fix quadchute logic so that it also works during back transition 2021-01-15 09:19:07 +03:00
Daniel Agar 420ceb76fc cmake: NuttX generated vscode launch.json requires DEBUG_DEVICE found 2021-01-14 10:32:26 -05:00
SalimTerryLi 1ee98417f8 scumaker pilotpi updates
* replace default mag with qmc5883l
* fix rotation and quiet startup
* fixedwing script & Multi-EKF cfg
* set default params only when initial startup
2021-01-14 09:16:13 -05:00
Daniel Agar 52b07a932a github actions build and store cannode uavcan firmware 2021-01-14 08:52:38 -05:00
RomanBapst 96dfa7fc71 ROMFS: set cruise throttle correctly for all gazebo vtol configs
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-14 09:58:37 +03:00
Silvan Fuhrer 0633c3956f ROMFS: improve tuning of tailsitter VTOL SITL
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-14 09:58:37 +03:00
Silvan Fuhrer 6104fe8932 ROMFS: improve tuning of tiltrotor VTOL SITL
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-14 09:58:37 +03:00
Silvan Fuhrer 2ce310925c ROMFS: improve tuning of standard VTOL SITL
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-14 09:58:37 +03:00
Daniel Agar e96571b45d uavcannode: GPS working on cuav_can-gps-v1
- use sensor_gps directly from sensor rather than vehicle_gps_position (aggregated value)
2021-01-13 22:06:46 -05:00
Daniel Agar d8e8e23947 vscode: add cuav_can-gps-v1_canbootloader variant 2021-01-13 22:06:46 -05:00
Daniel Agar 58909b208d boards: cuav can-gps-v1 add safety button and LED 2021-01-13 22:06:46 -05:00
Daniel Agar a894ca30e8 cmake: add STM32F412CE debug helper 2021-01-13 22:06:46 -05:00
David Sidrane 529841ba7c make_can_boot_descriptor:Get padding math correct 2021-01-13 22:06:46 -05:00
David Sidrane 1ac70cc72f can-gps-v1:Correct Memory size used by app and bootloader size 2021-01-13 22:06:46 -05:00
David Sidrane d04216aa48 Nuttx with stmf412 fixes 2021-01-13 22:06:46 -05:00
David Sidrane 618bd5978a can-gps-v1:canbootloader SAFETY is GETNODEINFO_JUMPER 2021-01-13 22:06:46 -05:00
David Sidrane 2deef30d12 canbootloader:Add 48Mhz CAN Clock Settings 2021-01-13 22:06:46 -05:00
David Sidrane 177109a1af can-gps-v1:LED Trimming 2021-01-13 22:06:46 -05:00
David Sidrane 54abd997de canbootloader:Update to use NuttX 2021-01-13 22:06:46 -05:00
David Sidrane 271f87f8d2 canbootloader:Fixed Warning 2021-01-13 22:06:46 -05:00
David Sidrane 238c28d458 SK6812 Led driver 2021-01-13 22:06:46 -05:00
David Sidrane 85bd04f0c7 can-gps-v1:canbootloader Fixed 2021-01-13 22:06:46 -05:00
David Sidrane 3e08fd6682 can-gps-v1: Removed GPIO_CAN_CTRL 2021-01-13 22:06:46 -05:00
David Sidrane c2c92cb2c8 can-gps-v1: Added LED pin 2021-01-13 22:06:46 -05:00
David Sidrane cdae8bf168 can-gps-v1:Fixed Clock 2021-01-13 22:06:46 -05:00
Daniel Agar a0d8d5ac74 sensors/vehicle_gps_position: untangle and remove unnecessary state 2021-01-13 20:17:49 -05:00
Daniel Agar bc8ec5d1f5 uavcannode: support optical_flow 2021-01-13 19:35:28 -05:00
RomanBapst 47364ce8d6 updated tuning for gazebo plane airframe config
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst f05599caff tecs: use speed derivative provided by local position
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
Silvan Fuhrer b230bbfe88 ROMFS: remove outdated TECS parameter from configs
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-13 21:21:07 +03:00
RomanBapst e546584555 tecs: moved trivial getter methods to header file
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
Roman Bapst 701c105ab6 Update src/lib/tecs/TECS.cpp
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst fa559aef43 TECS: stop learing integrator if airspeed is not available, but don't zero it
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst d4d1c0fe01 TECS: some cosmetics
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst 97cc1e25dd TECS: hande pitch and throttle integrator saturation consistently
- don't decay integrator during saturation but prevent it from being learned
into the direction which causes more actuator saturation

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst 77627a08ca TECS: don't allow speed height weights to be larger than one
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
Silvan Fuhrer dca89763b3 TECS: apply FW_LND_THRTC_SC to altitude error time constant
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-13 21:21:07 +03:00
Silvan Fuhrer 3d3ff75495 TECS: update some params to latest results from flight testing
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-13 21:21:07 +03:00
Silvan Fuhrer 3102b9f071 TECS: remove throttle integral limits
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-13 21:21:07 +03:00
RomanBapst 987c320825 TECS: removed unused parameter
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst 5c4c2c240c tecs: dot not clip throttle integrator during saturation but only allow
it to propagate into a direction which does not saturate

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
Silvan Fuhrer 2ca4269464 TECS: separate integral gains for throttle and pitch loops
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-13 21:21:07 +03:00
Silvan Fuhrer 72dfb2078a TECS: adapt params to new control structure
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-13 21:21:07 +03:00
RomanBapst 01f891618b TECS: move to new control loop architecture
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst 447e14906c TECS: log more TECS states to enable better analysis
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst 8823f5e1ec TECS: added method to get SKE weighting
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
RomanBapst d0e8b882a2 TECS: added alpha filter classes to energy rate and tas derivative
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 21:21:07 +03:00
xdwgood cabb50a67b 13001_caipirinha_vtol:Ensure that the max/min pwm changes take effect 2021-01-13 11:32:01 +01:00
Julian Kent be0f5a7fe4 Fix implicit float->double conversions in tests 2021-01-13 10:26:10 +01:00
Julian Kent 2d6758a39d Cleanup of dataman mocks and check interval definition 2021-01-13 10:26:10 +01:00
Julian Kent a97a4d8bb8 Fix enum and param update 2021-01-13 10:26:10 +01:00
Julian Kent c745c8bb45 Small navigator refactor/cleanup 2021-01-13 10:26:10 +01:00
Julian Kent 04d859e36e Fix test failure from parameter autosave starting WQ 2021-01-13 10:26:10 +01:00
RomanBapst f97dcde4e2 GeofenceBreachAvoidanceTest: added tests for max dist to home
Signed-off-by: Julian Kent <julian@auterion.com>
2021-01-13 10:26:10 +01:00
RomanBapst 3fa15cec91 GeofenceBreachAvoidance: improve behavior when using max dist to home option
- ensure that the vehicle is loitering with sufficient clearance to the boundary

Signed-off-by: Julian Kent <julian@auterion.com>
2021-01-13 10:26:10 +01:00
Julian Kent a5dfa0c803 Add helper function for decel distances
Co-authored-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 10:26:10 +01:00
RomanBapst 0ac597fba8 Use new GeofenceBreachAvoidance from Navigator
Signed-off-by: Julian Kent <julian@auterion.com>
2021-01-13 10:26:10 +01:00
RomanBapst e536868104 Add GeofenceBreachAvoidance class
Signed-off-by: Julian Kent <julian@auterion.com>
2021-01-13 10:26:10 +01:00
Julian Kent 8622c21496 Move VelocitySmoothing to new motion_planning library
Co-authored-by: RomanBapst <bapstroman@gmail.com>
2021-01-13 10:26:10 +01:00
Jannik Beyerstedt 3834690c4b Add parameter to select the set of used GNSS systems 2021-01-13 08:33:07 +01:00
JacobCrabill 917fef546a uavcan: Remove single-GNSS limitation from UavcanGnssBridge 2021-01-12 22:04:52 -05:00
Daniel Agar a57b9f9381 delete drv_baro.h, drv_mag.h, drv_range_finder.h, drv_device.h and purge UAVCAN CDev usage 2021-01-12 22:04:52 -05:00
Daniel Agar 7f5fae91b0 boards: mro ctrl zero f7 fix default power module calibration 2021-01-12 16:51:05 -05:00
Jaeyoung-Lim 16b1b220fd Fix roslaunch multivehicle regression caused by #16497 2021-01-12 21:19:36 +01:00
Beat Küng daaf8b61dc drivers: remove ism330dlc
not used anymore
2021-01-12 09:55:59 -05:00
Beat Küng 9f5dee2ecf v5x/v6x: update IMU sensors (remove ISM330DLC) 2021-01-12 09:55:59 -05:00
Daniel Agar 48f125f150 estimated IMU bias preflight checks
- commander preflightcheck use estimator_sensor_bias message instead of EKF state index magic number
 - ekf2 publish estimated bias limits in estimator_sensor_bias
 - preflightcheck only error if bias estimate exceeds half of configured limit (delete COM_ARM_EKF_AB and COM_ARM_EKF_GB parameters)
2021-01-12 09:09:42 +01:00
TSC21 7c95e99156 tools: make sure that uORB type names found as part of field names are not capitalized as ROS types 2021-01-12 09:05:59 +01:00
Daniel Agar cb74cb8692 boards: enable CONFIG_ARMV7M_LAZYFPU everywhere 2021-01-12 09:04:38 +01:00
Daniel Agar abec2bd8df msg: estimator_status_flags shorten fields
- previously this message exceeded the logger total field length (1500 bytes)
2021-01-11 11:49:51 -05:00
Daniel Agar 04f9ada500 ekf2: selector improve fallback selection when the primary becomes unhealthy
- if an ekf instance becomes unhealthy prefer switching to the next best healthy instance on a different IMU
2021-01-11 09:38:26 -05:00
Daniel Agar 967d35a6b6 rate limit most parameter_update subscriptions
- parameter updates can be quite expensive because they trigger nearly all modules to reload all of their parameters immediately
 - limit modules from updating faster than once per second
2021-01-10 21:09:15 -05:00
Daniel Agar 70e503cb91 rotation: use Dcmf for all rotations that aren't direct swaps
- increase optimization to ${MAX_CUSTOM_OPT_LEVEL} (max per board)
2021-01-10 18:08:41 -05:00
TSC21 06b733bb86 msg: rtps: improve verbosity when the the client is not capable of parsing a specific ID 2021-01-10 22:22:22 +01:00
TSC21 3f1c303b16 msg: rtps: improve verbosity when the the agent is not capable of parsing a specific ID 2021-01-10 22:22:22 +01:00
bazooka joe 9b9163813d avoid re-initiate RTL or land in battery emergency
if the mode is already running
2021-01-10 21:19:52 +01:00
Nicolas de Palezieux 6260c164e7 fmu v4: make starting mavlink on WIFI port configurable and make it start by default 2021-01-10 21:16:02 +01:00
Nicolas de Palezieux 653b7c0007 fmu v4: add option to run DShot telemetry on UART usually used for the ESP WIFI module 2021-01-10 21:16:02 +01:00
Matthias Grob 3cc8e7a210 commander_params: Make multicopter only COM_RC_OVERRIDE more visible 2021-01-10 21:12:09 +01:00
TSC21 cef3d36af2 simulator: delete PublicationMulti ptrs for sensor_gps 2021-01-10 19:58:54 +01:00
Daniel Agar f73d93ef6c ekf2: selector improve status reporting
- publish estimator_selector_status at minimal rate or immediately on change
 - log all estimator_selector_status updates
2021-01-10 19:25:53 +01:00
Matthias Grob 2fc212e064 geofence_params: clarify EKF vs baro altitude source 2021-01-10 18:40:58 +01:00
Hamish Willee d5c8d0a233 GF_ALTMODE: Update in line with Lorenz feedback 2021-01-10 18:40:58 +01:00
Hamish Willee d43444fce7 geofence: GF_ALTMODE clarification 2021-01-10 18:40:58 +01:00
Muesli_Reep fe7908feb0 Simulator: Added remote host option (#15443)
* Added an option to the Simulator module to connect to remote Gazebo servers.

This is usefull when the Gazebo simulation is running on a different host than the PX4 instance.
For example, we are running instances of PX4 with a companion application in multiple Dockers, for swarming simulations, which then connect to a remote Gazebo server.

A "-t" input argument has been added and can be called from the rcS startup script as: simulator start -t "192.168.178.122" $simulator_tcp_port

* _tcp_remote_ipaddr defaults to nullptr. This way testing against nullptr it can be determined if localhost or remote host is desired by the user.
* Documented the option in usage().

Signed-off-by: Peter Blom <peterblom.mail@gmail.com>
2021-01-10 18:37:37 +01:00
Daniel Agar 763c3b8fda boards: start enabling multi-EKF by default on F7/H7 2021-01-10 17:56:34 +01:00
Jaeyoung-Lim b3257c0bf2 Support relative altitude for offboard global position setpoints
Previously the coordinate_frame flag for setpoint_target_global_int message was not handled, resulting in the vehicle to not handle altitude correctly. This commit handles the relative altitude correctly.
2021-01-10 17:54:53 +01:00
Daniel Agar 662f177830 ekf2: multi instance numbering consistent with uORB publication instances 2021-01-09 13:20:26 -05:00
Daniel Agar c3fc96fd42 uORB::PublicationMulti add get_instance() 2021-01-09 13:20:26 -05:00
PX4 BuildBot 0398a936e3 Update submodule ecl to latest Sat Jan 9 16:06:23 UTC 2021
- ecl in PX4/Firmware (c6af260a41): https://github/commit/c212975abe83bf462bc512288ba30358f9a17865
    - ecl current upstream: https://github/commit/99575d73e10aad06eb7d5b6415ea2db4151c5045
    - Changes: https://github/compare/c212975abe83bf462bc512288ba30358f9a17865...99575d73e10aad06eb7d5b6415ea2db4151c5045

    99575d7 2021-01-09 Paul Riseborough - EKF: Add bad accel bias checking for EV and range finder height use cases
ff3c0a6 2021-01-08 Paul Riseborough - EKF: Fix bug preventing recovery from bad delta velocity bias estimates
c25c97f 2021-01-08 priseborough - [AUTO COMMIT] update change indication
9641810 2021-01-08 Paul Riseborough - test: Allow for larger vel variance growth due to dvel bias variance
1b1c049 2021-01-08 Paul Riseborough - test: Update unit test to match expected behaviour
dd259a2 2021-01-07 Paul Riseborough - EKF: Don't modify accel bias states and variances when inhibited
3e1f2d8 2021-01-07 Paul Riseborough - EKF: Set dvel bias variance to stored value when state is inactive
2021-01-09 12:57:25 -05:00
Daniel Agar c6af260a41 log_message increase queue depth 2->4 2021-01-09 11:04:32 -05:00
Jaeyoung-Lim d42e57a066 Update sitl_gazebo to latest
This PR updates sitl_gazebo to latest
2021-01-08 21:33:22 -05:00
Daniel Agar b9a721726d sensors/vehicle_magnetometer: respect calibration offset update success
- the magnetometer calibration offset setter returns false if the new offset change is negligible
2021-01-08 15:34:48 -05:00
Mohamed Abdelkader Zahana 80dd841cad Update launch files to enable multi-video stream in SITL (#16497)
* Update launch files to support multi-video stream in SITL

* Pass extra args to jinja_gen.py inside gazebo_sitl_multiple_run.sh to enable multi-video streaming
2021-01-08 19:29:47 +01:00
Silvan Fuhrer 706f806943 VTOL: standard VTOL and Tiltrotor manual MC throttle during transition
This sets the throttle of the Multicopter actuators to the throttle stick position
while in Stabilized, Acro or Manual mode.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-08 10:28:00 +01:00
xdwgood 802c68a62e Do not run transition flight task when not enable altitude control 2021-01-08 10:28:00 +01:00
Daniel Agar bf330a51b2 sensors/vehicle_magnetometer: reduce offset update message length to fit 2021-01-08 01:22:31 -05:00
Thies Lennart Alff eb60479e4c UUV introduce param to skip controller (#15706)
* added skip_ctrl param to uuv

* fixed formatting
2021-01-08 06:50:40 +01:00
PX4 BuildBot 064511c2df Update submodule flightgear_bridge to latest Fri Jan 8 00:39:45 UTC 2021
- flightgear_bridge in PX4/Firmware (168468c12a): https://github.com/PX4/PX4-FlightGear-Bridge/commit/44b51d5b1ccc6679e82090e24177ed73a3d4f5de
    - flightgear_bridge current upstream: https://github.com/PX4/PX4-FlightGear-Bridge/commit/7c2c623da9f5dcb3f01d32830af1a2ed958de363
    - Changes: https://github.com/PX4/PX4-FlightGear-Bridge/compare/44b51d5b1ccc6679e82090e24177ed73a3d4f5de...7c2c623da9f5dcb3f01d32830af1a2ed958de363

    7c2c623 2021-01-06 slimonslimon - Switch Ign-math to Eigen3 (#5)
2021-01-07 21:21:02 -05:00
PX4 BuildBot 168468c12a Update submodule ecl to latest Thu Jan 7 12:50:52 UTC 2021
- ecl in PX4/Firmware (c999734463c9b23c6b56670d5242ca4496f9e6ef): https://github/commit/03fed323ab950125114eb34309d3a79119e572ee
    - ecl current upstream: https://github/commit/c212975abe83bf462bc512288ba30358f9a17865
    - Changes: https://github/compare/03fed323ab950125114eb34309d3a79119e572ee...c212975abe83bf462bc512288ba30358f9a17865

    c212975 2021-01-06 bresch - rng height: reset to baro using common logic
2021-01-07 12:08:21 -05:00
Daniel Agar 88f8da27ef save learned mag bias per sensor (Multi-EKF support)
- handle saving the mag bias per sensor (across all estimator instances using that mag) in sensors/vehicle_magnetometer
 - this is now saving back to the actual mag calibration CAL_MAGn_OFF{X,Y,Z}
 - ekf2 reset mag mag bias on any magnetometer or calibration change
 - use Kalman filter scheme to update stored mag bias parameters using all available bias estimates for that sensor

Co-authored-by: Paul Riseborough <gncsolns@gmail.com>
2021-01-07 09:54:13 -05:00
Matthias Grob 537ee5b19b FlightTaskOrbit: smooth yaw like in missions 2021-01-07 13:31:05 +01:00
Matthias Grob 44606ca872 FlightTaskOrbit: further simplify circling yaw setpoint calculation
The whole angle adding and pi wrap was just necessary because the
correct atan2 arguments were never completely thought through.
2021-01-07 13:31:05 +01:00
Matthias Grob f435bea57c state_machine_helper: orbit failsafe just with data link loss
RC is like the comment says not required.
2021-01-07 13:31:05 +01:00
Matthias Grob 6b8fa417e1 SlewRate: Add SlewRateYaw handling [-pi,pi] wraps 2021-01-07 13:31:05 +01:00
Daniel Agar 6c9072720e invensense/icm42688p: use full 20 bit data, increase ODR, disable all filters 2021-01-06 17:03:39 -05:00
Jaeyoung-Lim d2b0f63e1f Handle offboard mode with acceleration setpoints
The case when acceleration setpoints were being passed in offboard mode was triggering control_climbrate_mode. This prevented the vehicle from taking off, since it made the vehicle skip the rampup phase of the takeoff
This commit fixes this by handling the case properly
2021-01-06 20:38:18 +01:00
garfieldG 3fb8f5df62 drivers/lsm303agr: fixed bug incorrectly assembling signed 16 bit integer from bytes 2021-01-05 21:37:08 -05:00
PX4 BuildBot 01e3f0d586 Update submodule matrix to latest Tue Jan 5 12:40:51 UTC 2021
- matrix in PX4/Firmware (fd97e28019fa9c665d9b3c6995098dd51b4ab022): https://github/commit/15e54ceda176f05e1ae38e71692d15cafb9e3a62
    - matrix current upstream: https://github/commit/054f8b12f4da79767df6e05bb1d2cc8d679b99f3
    - Changes: https://github/compare/15e54ceda176f05e1ae38e71692d15cafb9e3a62...054f8b12f4da79767df6e05bb1d2cc8d679b99f3

    054f8b1 2021-01-04 Julian Kent - Use a single inverse implementation for a single matrix size
2021-01-05 19:24:42 -05:00
PX4 BuildBot ff82911d86 Update submodule ecl to latest Tue Jan 5 12:40:47 UTC 2021
- ecl in PX4/Firmware (824f78466ac4e32aecd6bda785e95eb348e1b31e): https://github/commit/78ce46f00777f07d24c31bdc5e2edb203be2c0f4
    - ecl current upstream: https://github/commit/03fed323ab950125114eb34309d3a79119e572ee
    - Changes: https://github/compare/78ce46f00777f07d24c31bdc5e2edb203be2c0f4...03fed323ab950125114eb34309d3a79119e572ee

    03fed32 2021-01-05 Paul Riseborough - EKF: Fix formatting
31fca9c 2021-01-05 Paul Riseborough - EKF: Update GPS loss message
c65cf13 2020-12-15 Paul Riseborough - EKF; Treat combined sideslip and airspeed as a horizontal aiding source
211c84c 2021-01-04 bresch - Rng finder unit test: cover "un-stuck" logic
2021-01-05 19:23:25 -05:00
Paul Riseborough 64ed96bd95 ekf2: Correct airspeed used by EKF for calibration errors 2021-01-05 19:22:53 -05:00
Daniel Agar b94e346488 Update submodule sitl_gazebo to latest Tue Jan 5 12:40:40 UTC 2021 (#16493)
- sitl_gazebo in PX4/Firmware (850d0bc588): https://github.com/PX4/PX4-SITL_gazebo/commit/054e0a1be67b715ca1802397082e7814a1427f52
    - sitl_gazebo current upstream: https://github.com/PX4/PX4-SITL_gazebo/commit/44de4acc3f9cf9e44db58006f99ea190d217017a
    - Changes: https://github.com/PX4/PX4-SITL_gazebo/compare/054e0a1be67b715ca1802397082e7814a1427f52...44de4acc3f9cf9e44db58006f99ea190d217017a

    44de4ac 2021-01-02 Lorenz Meier - Update README.md

Co-authored-by: PX4 BuildBot <bot@px4.io>
2021-01-05 19:34:11 +01:00
Silvan Fuhrer 850d0bc588 vtol_type: remvoe const from function declaration
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-04 15:32:00 +01:00
RomanBapst 0871f0f52d vtol: refactor of maximum pwm value settings for main and alternate motors
- main motors are the ones which are meant to be used as propulsion in fw mode
- alternate motors are the ones usually meant to be switched off in fw mode

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 15:32:00 +01:00
Daniel Agar bc1e9f72f7 Jenkins hardware temporarily remove px4_fmu-v2 2021-01-04 09:30:47 -05:00
Silvan Fuhrer 92634e7549 RTL: during climb, set NAV_CMD_WAYPOINT for RW modes, NAV_CMD_LOITER_TO_ALT for FW
Do not use LOITER_TO_ALT for rotary wing mode as it would then always climb to
at least MIS_LTRMIN_ALT, even if current clib altitude is below
(e.g. RTL immediately after take off)

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-04 11:58:16 +01:00
Silvan Fuhrer 0b86c11c66 FW POS: remove setting of curr_sp to LOITER if next wp invalid
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-04 11:58:16 +01:00
Silvan Fuhrer 55a1d090a1 RTL: use NAV_CMD_LOITER_TO_ALT for Climb state
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-04 11:58:16 +01:00
RomanBapst 68f27ba7b7 navigator: deactivate line following after backt-ransition and before landing
- especially when there are strong winds it's better to just go straight
to the landing point instead of trying to follow the planned path

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst b63f756745 navigator: don't execute land pattern if vtol in rotary wing mode
- if vtol and in rotary wing mode then don't execute the mission landing
because it's designed to be flow as a fixed wing
- if vtol and in rotary wing mode and mission land is available then fly directly
to landing point and don't go home!

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst 6c3f413379 mission: reset work_item_type during mission inactivation
- this fixes a race condition which happens when an RTL is triggered
during the final approach of a mission landing. In that case the mission inactive
method is never called.

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst b63f202b3c various fixed for bugs encountered during testing
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst cfb3cdc82f rtl: use math namespace
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst 94d3ab28ee rtl: fixed computation of return altitude when mission landing is available
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst 12875f7869 mission: when land start marker present, look for loiter to altitude item
instead of using the previous waypoint as landing target
- the previous waypoint could be miles away

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst e0c394a00b mission: fixed bug in computation of landing altitude
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst a4a03e86da mission: be more intelligent about saying that we are on a mission landing
- previously the decision of being on a landing pattern was taken by just
looking at the current mission index. However, even if the current mission
index indicates a landing pattern the vehicle could be at an arbitrary location, far
from being established on the pattern.

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst 29c3ce6d5d reworked RTL cone implementation
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst dad5ce1e41 rtl: set proper acceptance radius for move_to_land item
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst 6ff95ae645 RTL: implement proper RTL sequence for VTOL
- descend to RTL descend altitude
- transition
- move to land waypoint
- loiter and then land

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst 197a21a22e rtl: for fixed wing (also vtol) make the descend state of RTL use type
NAV_CMD_LOITER_TO_ALT

- this allows vtol to track the loiter circle during the transition instead
of trying to fly to the landing position

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst bb2826ad27 rtl: for vtol first desend down to RTL descend altitude before doing a transition
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
RomanBapst e81d5daa66 rtl: if very close to home then do not descend if higher than RTL_DESCEND_ALT
before reaching home

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-04 11:58:16 +01:00
Silvan Fuhrer 7c727edc3f Simple mixer: add output slew rate
This adds the option to limit the rate of change (slew rate) of an output that's mixed by a simple mixer.
To enable it, a positive number has to be added at the end (6th number) of the output scaler line of the mixer,
specifying the min rise time of this output.
E.g. O:      10000  10000      0 -10000  10000 20000 for a rise time of 2s, resp. a max slew rate of 0.5s^-1.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2021-01-04 11:32:22 +01:00
Daniel Agar 98cff94702 px4_work_queue: directly support SITL lockstep
- the purpose is to ensure that every WorkItem (and WorkItems scheduled
by WorkItems) is allowed to run to completion every step
 - per workqueue register a lockstep component whenever a work item is
added (if not already registered)
 - once the work queue is empty unregister component
2021-01-04 09:38:05 +01:00
PX4 BuildBot 8c71ecd97e Update submodule ecl to latest Sat Jan 2 12:39:29 UTC 2021
- ecl in PX4/Firmware (03925cc70fd13c15a5dfe8ecc5653b91098ac68d): https://github/commit/18f334f4dbca61e3bcd1743c22cf820b5a8ff7ef
    - ecl current upstream: https://github/commit/78ce46f00777f07d24c31bdc5e2edb203be2c0f4
    - Changes: https://github/compare/18f334f4dbca61e3bcd1743c22cf820b5a8ff7ef...78ce46f00777f07d24c31bdc5e2edb203be2c0f4

    78ce46f 2020-12-19 Kamil Ritz - Removing Matlab derivation
2021-01-02 11:54:56 -05:00
RomanBapst d502292d07 mission: for vtol takeoff don't use next waypoint as target during transition
- this caused the navigator to use the next waypoint (after the vtol takeoff item)
to be used as target during the transition. If the altitude of that waypoint
was much higher than the takeoff altitude then there were FOH effects
after the transition which caused the vehicle to first descend before
climbing again.

Signed-off-by: RomanBapst <bapstroman@gmail.com>
2021-01-02 02:18:59 +01:00
PX4 BuildBot a1b81df445 Update submodule sitl_gazebo to latest Fri Jan 1 12:39:16 UTC 2021
- sitl_gazebo in PX4/Firmware (a444d2610a): https://github.com/PX4/PX4-SITL_gazebo/commit/ca6c738fff30c516a5d2b9866ad268826a9ff0ff
    - sitl_gazebo current upstream: https://github.com/PX4/PX4-SITL_gazebo/commit/054e0a1be67b715ca1802397082e7814a1427f52
    - Changes: https://github.com/PX4/PX4-SITL_gazebo/compare/ca6c738fff30c516a5d2b9866ad268826a9ff0ff...054e0a1be67b715ca1802397082e7814a1427f52

    054e0a1 2021-01-01 pjdewitte - Jinja generation: add protection against accidental overwriting (#682)
869225e 2020-12-31 JaeyoungLim - Fix lightsource for high fidelity worlds (#680)
2021-01-01 21:57:05 +01:00
Lorenz Meier 0bdae5745a Update dsm.cpp
Fix documentation comment (reported by @Roman-, thanks!)
2021-01-01 15:30:25 +01:00
Lorenz Meier 9409122638 RC tests: Add new test file
This file is using a PX4IO-bound receiver on a DX9
2021-01-01 14:26:36 +01:00
Lorenz Meier 8d6239f11f PX4IO: Use DSM frame drops
These will now be reported the same as on SBUS.
2021-01-01 14:26:36 +01:00
Lorenz Meier 47fcf97442 DSM: Report frame drops
Frame drops were measured but not reported on PX4IO.
2021-01-01 14:26:36 +01:00
Lorenz Meier 00e6d11dfa PX Uploader: Disable windowed mode
The windowed mode has been added for Windows targets originally. It gets very often incorrectly detected and slows down flashing considerably. This even applies to serial links. We are disabling it now in most circumstances.
2021-01-01 14:26:36 +01:00
Daniel Agar 95dd2f7e8d rc/dsm: remove system field check, add new validity checks
- unfortunately we can't depend on the system field due to potential
external binding and non-genuine Spektrum equipment
 - reject any DSM frame with duplicate channels
 - add 16 channel mask
 - tighten valid PWM range 990-2010us (±100% travel is 1102-1898µs)
 - update RCTest rejected frame count
2021-01-01 14:26:36 +01:00
Daniel Agar d7b89ecc86 boards: px4/fmu-v5 disable px4io in rc.board_defaults
- avoid keeping this kind of logic in the common rcS
2021-01-01 14:12:26 +01:00
Lorenz Meier a444d2610a Spektrum passive power: Only use if present 2020-12-31 13:22:52 +01:00
Lorenz Meier 641cc33d79 RC input: Always report DSM state 2020-12-31 13:22:52 +01:00
Lorenz Meier e85afb22a5 FMUv5: Default Spektrum power to passive 2020-12-31 13:22:52 +01:00
Lorenz Meier cc34d4601d FMUv5: Support passive power controls
This ensures that FMU-side power controls are not interfering with IO-side power controls of DSM receivers if they happen to be OR-ed in the schematics
2020-12-31 13:22:52 +01:00
Lorenz Meier 6529e1444f RC input: Better monitoring
The output is now less confusing in terms of which protocol is currently active.
2020-12-31 13:22:52 +01:00
Lorenz Meier af28a298e5 DSM driver: Add option for passive power controls 2020-12-31 13:22:52 +01:00
Lorenz Meier 4237c8be25 Commander: Do not acknowledge binding
This is now done in the respective modules directly and based on implementation and execution state.
2020-12-31 13:22:52 +01:00
Lorenz Meier 2d1551e5bf PX4IO: Acknowledge binding 2020-12-31 13:22:52 +01:00
Lorenz Meier 8445a08bff RC input: Acknowledge binding (or indicate that feature is not implemented) 2020-12-31 13:22:52 +01:00
Lorenz Meier 44bdd5456f PX4IO: Bind if not armed
DSM binding was disabled before if safety was off, which on a lot of multicopters is today the default. The logic is now checking instead for wether the system is armed.
2020-12-31 13:22:52 +01:00
Lorenz Meier a34e57a4cc Simulator: Increase stack, publication affinity
This commit increases the send thread stack size and changes the thread affinity of the lockstep clocking topic. It also improves verbosity in case error states occur.
2020-12-31 01:05:30 +01:00
Lorenz Meier fda63f802e Tone alarm: Adjust log levels
The earlier log levels represented normal operation scenarios as errors, this aligns the log levels.
2020-12-31 01:05:30 +01:00
Lorenz Meier 3cc53f551d MAVSDK tests: Use full system timeout off
Depending on loop iterations for timeouts is not accurate, as usleep behavior depends on the system load and asking for a 0 ms sleep can potentially return immediately.
2020-12-31 01:05:30 +01:00
Lorenz Meier e27d80abc4 Camera feedback: Indicate success
If the feedback module is loaded then we want to provide capture feedback.
2020-12-30 23:36:47 +01:00
Daniel Agar 404f74f996 boards: mro/pixracerpro add flight_mode_manager 2020-12-30 10:25:08 -05:00
RomanBapst fe2e299046 FlightModeManager: small rebase change
Signed-off-by: RomanBapst <bapstroman@gmail.com>
2020-12-30 10:25:08 -05:00
Matthias Grob e92795b474 Temporary logging addition to debug CI 2020-12-30 10:25:08 -05:00
Matthias Grob fafbb687d8 FlightModeManager: fix integral reset on ground
This information could also be used for yaw and integral
resets of the lower level controllers.
2020-12-30 10:25:08 -05:00
Matthias Grob 7de288877a MulticoperPositionControl: 3rd pass get rid of zombie members 2020-12-30 10:25:08 -05:00
Matthias Grob 62ada2e2dc FlightModeManager: restore weathervane calls
I had to do an extra subscription to the vehicle attitude.
I don't know how to test this.
2020-12-30 10:25:08 -05:00
Matthias Grob aa888223f0 FlightModeManager: fix takeoff state in stabilized mode 2020-12-30 10:25:08 -05:00
Matthias Grob 8edb06e94f FlightModeManager: make sure emergency failsafe works 2020-12-30 10:25:08 -05:00
Matthias Grob 8329208b84 FlightModeManager: fix takeoff ramp from zero 2020-12-30 10:25:08 -05:00
Matthias Grob 88c274b3cd MulticopterPositionControl: 2nd pass to move to FlightModeManager 2020-12-30 10:25:08 -05:00
Matthias Grob f52bad87e2 mc_pos_control: separate out flight_tasks (into FlightModeManager) 2020-12-30 10:25:08 -05:00
Matthias Grob 7545249215 Add flight_mode_manager to all targets with mc_pos_control 2020-12-30 10:25:08 -05:00
Matthias Grob fa7170bc4f Add FlightModeManager
to separate out setpoint generation from controllers
2020-12-30 10:25:08 -05:00
Daniel Agar 49d4cc7d5b commander: CMD_NAV_LAND/CMD_NAV_PRECLAND reply RESULT_ACCEPTED unless transition is denied 2020-12-30 12:05:41 +01:00
Benjamin Linne 80068093d6 add esc_battery module to modalai/fc-v1 build 2020-12-29 23:41:22 -05:00
Daniel Agar 91f5f26618 commander: main_state_transition call trivial style fixes 2020-12-30 00:26:14 +01:00
Daniel Agar 4f62355dec msg: new estimator_status_flags message for more accessible ekf2 status logging
- log all estimator (ekf2) flags as separate booleans in a new dedicated low rate message (only publishes at 1 Hz or immediately on any change)
 - this is a bit verbose, but it avoids the duplicate bit definitions we currently have across PX4 msgs, ecl analysis script, flight review, and many other custom tools and it's much easier for casual log review in FlightPlot, PlotJuggler, csv, etc
 - for compatibility I've left estimator_status filter_fault_flags, innovation_check_flags, and solution_status_flags in place, but they can gradually be removed as tooling is updated

Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>
2020-12-29 11:27:21 -05:00
Lorenz Meier ddc1f964d2 Mac OS CI: Harden against intermittent install failures 2020-12-28 23:43:57 +01:00
Lorenz Meier 565da15f2f MAVSDK test: Increase timeout 2020-12-28 22:04:08 +01:00
Lorenz Meier 7510e6ba0a FMUv2: Exclude rarely used configurations 2020-12-28 21:02:03 +01:00
Lorenz Meier 53711926ab FMUv2: Exclude specialized fixed wing configs
The FMUv2 users can default back to generic configs for those.
2020-12-28 21:02:03 +01:00
Lorenz Meier aa28c3bd3c VTOL airframes: Exclude FMUv2
This excludes FMUv2 targets, since VTOL is already disabled on FMUv2.
2020-12-28 21:02:03 +01:00
Lorenz Meier 3d809134f5 Updating SITL gazebo (Mac OS fixes) 2020-12-28 20:41:48 +01:00
Daniel Agar adb98d5702 mavlink: move HIL_ACTUATOR_CONTROLS to separate streams header 2020-12-28 11:09:46 +01:00
Daniel Agar 3b20310e9c mavlink: move POSITION_TARGET_GLOBAL_INT to separate streams header 2020-12-28 11:09:46 +01:00
Daniel Agar 672a1c90aa mavlink: move POSITION_TARGET_LOCAL_NED to separate streams header
- position type_mask
2020-12-28 11:09:46 +01:00
Daniel Agar 6b1d02feb7 mavlink: move RC_CHANNELS to separate streams header 2020-12-28 11:09:46 +01:00
Daniel Agar 48be6962d1 mavlink: move MANUAL_CONTROL to separate streams header 2020-12-28 11:09:46 +01:00
Daniel Agar 629d03b684 mavlink: move TRAJECTORY_REPRESENTATION_WAYPOINTS to separate streams header 2020-12-28 11:09:46 +01:00
Daniel Agar 5762c3b356 mavlink: move NAV_CONTROLLER_OUTPUT to separate streams header 2020-12-28 11:09:46 +01:00
Daniel Agar 9f57df75e8 remove rotation 41 (ROLL_270_YAW_180)
- duplicate of 31 (ROLL_90_PITCH_180)
2020-12-28 11:07:08 +01:00
Daniel Agar a66cb0cbaf mavlink: check TX buffer before processing command ack 2020-12-28 11:05:42 +01:00
bazooka joe 8d5813994f format smart battery serial number as string on mavlink
according to change on mavlink protocol message
formatted as 'dd/mm/yy-123456'
2020-12-28 11:04:54 +01:00
Daniel Agar ceadcd74d0 mavlink: CAMERA_TRIGGER stream check free tx buf before send 2020-12-28 11:03:53 +01:00
Daniel Agar ae706537b8 mavlink: CAMERA_IMAGE_CAPTURED stream check free tx buf before send 2020-12-28 11:03:53 +01:00
Daniel Agar 27b631e827 mavlink: ADSB_VEHICLE stream check free tx buf before send 2020-12-28 11:03:53 +01:00
Daniel Agar 0d72b47571 mavlink: COLLISION stream check free tx buf before send 2020-12-28 11:03:53 +01:00
Daniel Agar dcb897307d mavlink: HEARTBEAT stream check free tx buf before send 2020-12-28 11:03:53 +01:00
Nicolas MARTIN e06d218ff2 commander: disable arm_auth request for prearm status continuous publication 2020-12-27 16:23:05 -05:00
Daniel Agar 02a08c42b7 tests: perf don't bother printing all perf counters 2020-12-27 15:29:45 -05:00
Daniel Agar 12bf035642 uORB: tests limit latency to only orb_test_medium and remove some unnecessary output 2020-12-27 15:29:45 -05:00
Daniel Agar 409ea2ac02 mavlink: parameters manually mark active minimal QGC set on first send 2020-12-27 13:54:03 -05:00
Lorenz Meier 4b0d8efbc1 Commander: move static overload_start to class 2020-12-27 13:44:32 -05:00
Jaeyoung-Lim 4f30037980 Add yosemite world as SITL target for gazebo
This commit adds yosemite world as a SITL target for gazebo
2020-12-27 12:53:25 -05:00
Daniel Agar 092060cde2 posix: improve error out for mlockall() and pthread_create
- add strerror
 - mlockall skipped in lockstep builds (ENABLE_LOCKSTEP_SCHEDULER)
2020-12-27 12:43:32 -05:00
Daniel Agar 48da0055a1 boards: add initial mRo Pixracer Pro (M10064C) support 2020-12-27 12:12:15 -05:00
628 changed files with 18816 additions and 6182 deletions
+1
View File
@@ -53,6 +53,7 @@ pipeline {
"intel_aerofc-v1_default",
"modalai_fc-v1_default",
"mro_ctrl-zero-f7_default",
"mro_pixracerpro_default",
"mro_x21-777_default",
"mro_x21_default",
"nxp_fmuk66-v3_default",
+61 -51
View File
@@ -7,57 +7,57 @@ pipeline {
parallel {
stage("px4_fmu-v2_test") {
stages {
stage("build px4_fmu-v2_test") {
agent {
docker {
image 'px4io/px4-dev-nuttx-focal:2020-09-14'
args '-e CCACHE_BASEDIR=$WORKSPACE -v ${CCACHE_DIR}:${CCACHE_DIR}:rw'
}
}
steps {
sh 'export'
sh 'make distclean'
sh 'ccache -s'
sh 'git fetch --tags'
sh 'make px4_fmu-v2_test'
sh 'make sizes'
sh 'ccache -s'
stash includes: 'build/px4_fmu-v2_test/px4_fmu-v2_test.elf', name: 'px4_fmu-v2_test'
}
post {
always {
sh 'make distclean'
}
}
} // stage build
stage("test") {
agent {
label 'px4_fmu-v2'
}
stages {
stage("flash") {
steps {
sh 'export'
sh 'find /dev/serial'
unstash 'px4_fmu-v2_test'
// flash board and watch bootup
sh './platforms/nuttx/Debug/upload_jlink_gdb.sh build/px4_fmu-v2_test/px4_fmu-v2_test.elf && ./Tools/HIL/monitor_firmware_upload.py --device `find /dev/serial -name *usb-FTDI_*` --baudrate 57600'
}
}
stage("reset") {
steps {
cleanupFTDI();
}
}
}
options {
timeout(time: 90, unit: 'MINUTES')
}
}
}
}
// stage("px4_fmu-v2_test") {
// stages {
// stage("build px4_fmu-v2_test") {
// agent {
// docker {
// image 'px4io/px4-dev-nuttx-focal:2020-09-14'
// args '-e CCACHE_BASEDIR=$WORKSPACE -v ${CCACHE_DIR}:${CCACHE_DIR}:rw'
// }
// }
// steps {
// sh 'export'
// sh 'make distclean'
// sh 'ccache -s'
// sh 'git fetch --tags'
// sh 'make px4_fmu-v2_test'
// sh 'make sizes'
// sh 'ccache -s'
// stash includes: 'build/px4_fmu-v2_test/px4_fmu-v2_test.elf', name: 'px4_fmu-v2_test'
// }
// post {
// always {
// sh 'make distclean'
// }
// }
// } // stage build
// stage("test") {
// agent {
// label 'px4_fmu-v2'
// }
// stages {
// stage("flash") {
// steps {
// sh 'export'
// sh 'find /dev/serial'
// unstash 'px4_fmu-v2_test'
// // flash board and watch bootup
// sh './platforms/nuttx/Debug/upload_jlink_gdb.sh build/px4_fmu-v2_test/px4_fmu-v2_test.elf && ./Tools/HIL/monitor_firmware_upload.py --device `find /dev/serial -name *usb-FTDI_*` --baudrate 57600'
// }
// }
// stage("reset") {
// steps {
// cleanupFTDI();
// }
// }
// }
// options {
// timeout(time: 90, unit: 'MINUTES')
// }
// }
// }
// }
stage("px4_fmu-v3_default") {
stages {
@@ -102,6 +102,7 @@ pipeline {
steps {
// configure
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOSTART 13000"' // generic vtol standard
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param save"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "px4io forceupdate 14662 /etc/extras/px4_io-v2_default.bin" || true' // force px4io update
@@ -175,6 +176,7 @@ pipeline {
steps {
// configure
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOSTART 4001"' // generic multicopter
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param save"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "reboot" || true' // reboot to apply
@@ -247,6 +249,7 @@ pipeline {
steps {
// configure
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOSTART 13000"' // generic vtol standard
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param save"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "px4io forceupdate 14662 /etc/extras/px4_io-v2_default.bin" || true' // force px4io update
@@ -320,6 +323,7 @@ pipeline {
steps {
// configure
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOSTART 13000"' // generic vtol standard
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set IMU_GYRO_RATEMAX 2000"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param save"'
@@ -471,6 +475,7 @@ pipeline {
steps {
// configure
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOSTART 13000"' // generic vtol standard
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param save"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "reboot" || true' // reboot to apply
@@ -620,6 +625,7 @@ pipeline {
steps {
// configure
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "param set SYS_AUTOSTART 4001"' // generic vtol standardulticopter
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "param save"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "reboot" || true' // reboot to apply
@@ -694,6 +700,7 @@ pipeline {
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set DSHOT_CONFIG 600"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set IMU_GYRO_RATEMAX 4000"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOSTART 4001"' // generic quadcopter
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_BL_UPDATE 1"' // update bootloader
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_USE_IO 0"' // for dshot
@@ -770,6 +777,7 @@ pipeline {
steps {
// configure
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set CBRK_BUZZER 782097"' // disable buzzer
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOCONFIG 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param set SYS_AUTOSTART 4001"' // generic multicopter
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "param save"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "reboot" || true' // reboot to apply
@@ -837,6 +845,7 @@ void statusFTDI() {
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "listener estimator_selector_status"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "listener estimator_sensor_bias"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "listener estimator_status"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "listener estimator_status_flags"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "listener logger_status"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "listener sensor_accel"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-FTDI_*` --cmd "listener sensor_accel_fifo"'
@@ -915,6 +924,7 @@ void statusSEGGER() {
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "listener estimator_selector_status"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "listener estimator_sensor_bias"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "listener estimator_status"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "listener estimator_status_flags"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "listener logger_status"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "listener sensor_accel"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-SEGGER_*` --cmd "listener sensor_accel_fifo"'
+1 -1
View File
@@ -23,7 +23,7 @@ jobs:
token: ${{secrets.ACCESS_TOKEN}}
- name: setup
run: ./Tools/setup/macos.sh
run: ./Tools/setup/macos.sh; ./Tools/setup/macos.sh
- name: Prepare ccache timestamp
id: ccache_cache_timestamp
+1
View File
@@ -32,6 +32,7 @@ jobs:
intel_aerofc-v1_default,
modalai_fc-v1_default,
mro_ctrl-zero-f7_default,
mro_pixracerpro_default,
mro_x21-777_default,
mro_x21_default,
nxp_fmuk66-v3_default,
@@ -0,0 +1,59 @@
name: NuttX UAVCAN firmware
on:
push:
branches:
- 'master'
pull_request:
branches:
- '*'
jobs:
build:
runs-on: ubuntu-latest
container: px4io/px4-dev-nuttx-focal:2020-11-18
strategy:
matrix:
config: [
cuav_can-gps-v1_default,
#nxp_ucans32k146_default,
px4_fmu-v4_cannode
]
steps:
- uses: actions/checkout@v1
with:
token: ${{secrets.ACCESS_TOKEN}}
- name: Prepare ccache timestamp
id: ccache_cache_timestamp
shell: cmake -P {0}
run: |
string(TIMESTAMP current_date "%Y-%m-%d-%H;%M;%S" UTC)
message("::set-output name=timestamp::${current_date}")
- name: ccache cache files
uses: actions/cache@v2
with:
path: ~/.ccache
key: ${{matrix.config}}-ccache-${{steps.ccache_cache_timestamp.outputs.timestamp}}
restore-keys: ${{matrix.config}}-ccache-
- name: setup ccache
run: |
mkdir -p ~/.ccache
echo "base_dir = ${GITHUB_WORKSPACE}" > ~/.ccache/ccache.conf
echo "compression = true" >> ~/.ccache/ccache.conf
echo "compression_level = 6" >> ~/.ccache/ccache.conf
echo "max_size = 400M" >> ~/.ccache/ccache.conf
ccache -s
ccache -z
- name: make ${{matrix.config}}
run: make ${{matrix.config}}
- name: ccache post-run
run: ccache -s
- name: Upload px4 package
uses: actions/upload-artifact@v2
with:
name: px4_cannode_${{matrix.config}}
path: build/${{matrix.config}}/*.uavcan.bin
+5
View File
@@ -66,6 +66,11 @@ CONFIG:
buildType: MinSizeRel
settings:
CONFIG: cuav_can-gps-v1_default
cuav_can-gps-v1_canbootloader:
short: cuav_can-gps-v1_canbootloader
buildType: MinSizeRel
settings:
CONFIG: cuav_can-gps-v1_canbootloader
cuav_nora_default:
short: cuav_nora
buildType: MinSizeRel
@@ -16,20 +16,31 @@ then
param set FW_LND_ANG 8
param set FW_THR_LND_MAX 0
param set FW_L1_PERIOD 15
param set FW_P_TC 0.5
param set FW_PR_FF 0.40
param set FW_PR_I 0.05
param set FW_PR_P 0.05
param set FW_R_TC 0.7
param set FW_RR_FF 0.20
param set FW_RR_I 0.02
param set FW_RR_P 0.22
param set FW_L1_PERIOD 12
param set FW_MAN_P_MAX 30
param set FW_PR_I 0.4
param set FW_PR_P 0.9
param set FW_PR_FF 0.2
param set FW_PSP_OFF 2
param set FW_P_LIM_MAX 32
param set FW_P_LIM_MIN -15
param set FW_RR_FF 0.1
param set FW_RR_P 0.3
param set FW_THR_MAX 0.6
param set FW_THR_MIN 0.05
param set FW_THR_CRUISE 0.25
param set FW_T_ALT_TC 2
param set FW_T_CLMB_MAX 8
param set FW_T_HRATE_FF 0.5
param set FW_T_SINK_MAX 2.7
param set FW_T_SINK_MIN 2.2
param set FW_T_TAS_TC 2
param set FW_W_EN 1
param set MIS_LTRMIN_ALT 30
@@ -9,40 +9,46 @@
if [ $AUTOCNF = yes ]
then
param set FW_AIRSPD_MAX 25
param set FW_AIRSPD_MIN 14
param set FW_AIRSPD_TRIM 16
param set FW_L1_PERIOD 12
param set FW_MAN_P_MAX 30
param set FW_PR_FF 0.2
param set FW_PR_I 0.4
param set FW_PR_P 0.9
param set FW_PSP_OFF 2
param set FW_P_LIM_MAX 32
param set FW_P_LIM_MIN -15
param set FW_RR_FF 0.1
param set FW_RR_P 0.01
param set FW_RR_P 0.3
param set FW_THR_CRUISE 0.25
param set FW_THR_MAX 0.6
param set FW_THR_MIN 0.05
param set FW_T_ALT_TC 2
param set FW_T_CLMB_MAX 8
param set FW_T_HRATE_FF 0.5
param set FW_T_SINK_MAX 2.7
param set FW_T_SINK_MIN 2.2
param set FW_T_TAS_TC 2
param set MC_ROLLRATE_P 0.3
param set MC_YAW_P 1.6
param set MIS_LTRMIN_ALT 10
param set MIS_TAKEOFF_ALT 10
param set MIS_YAW_TMT 10
param set MPC_ACC_HOR_MAX 2
param set MPC_ACC_HOR_MAX 2
param set MPC_THR_HOVER 0.58
param set MPC_TKO_SPEED 1
param set MPC_XY_P 0.8
param set MPC_XY_VEL_P_ACC 3
param set MPC_XY_VEL_I_ACC 4
param set MPC_XY_VEL_D_ACC 0.1
param set MPC_Z_VEL_MAX_DN 1.5
param set NAV_ACC_RAD 5
param set NAV_LOITER_RAD 80
param set VT_F_TRANS_DUR 5
param set VT_FWD_THRUST_EN 4
param set VT_F_TRANS_THR 0.75
param set VT_ARSP_TRANS 16
param set VT_MOT_ID 1234
param set VT_FW_MOT_OFFID 1234
param set VT_TYPE 2
param set VT_B_TRANS_DUR 8
param set VT_TYPE 2
fi
@@ -9,23 +9,31 @@
if [ $AUTOCNF = yes ]
then
param set FW_AIRSPD_MAX 25
param set FW_AIRSPD_MIN 14
param set FW_AIRSPD_TRIM 16
param set FW_L1_PERIOD 12
param set FW_MAN_P_MAX 30
param set FW_PR_I 0.2
param set FW_PR_P 0.3
param set FW_PSP_OFF 2
param set FW_P_LIM_MAX 32
param set FW_P_LIM_MIN -15
param set FW_RR_P 0.3
param set FW_THR_CRUISE 0.33
param set FW_THR_MAX 0.6
param set FW_THR_MIN 0.05
param set FW_T_ALT_TC 2
param set FW_T_CLMB_MAX 8
param set FW_T_HRATE_FF 0.5
param set FW_T_SINK_MAX 2.7
param set FW_T_SINK_MIN 2.2
param set FW_T_TAS_TC 2
param set MC_ROLLRATE_P 0.3
param set MIS_YAW_TMT 10
param set MPC_ACC_HOR_MAX 2
param set MPC_ACC_HOR_MAX 2
param set MPC_THR_MIN 0.3
param set MPC_XY_P 0.15
param set MPC_XY_P 0.8
param set MPC_XY_VEL_P_ACC 3
param set MPC_XY_VEL_I_ACC 4
param set MPC_XY_VEL_D_ACC 0.1
param set MPC_XY_VEL_P_ACC 1
param set MPC_Z_VEL_MAX_DN 1.5
param set MPC_Z_VEL_P_ACC 16
param set NAV_ACC_RAD 5
param set NAV_LOITER_RAD 80
@@ -14,9 +14,20 @@ then
param set FW_PR_FF 0.2
param set FW_PR_I 0.4
param set FW_PR_P 0.9
param set FW_PSP_OFF 3
param set FW_PSP_OFF 2
param set FW_P_LIM_MAX 32
param set FW_P_LIM_MIN -15
param set FW_RR_FF 0.1
param set FW_RR_P 0.3
param set FW_THR_CRUISE 0.38
param set FW_THR_MAX 0.6
param set FW_THR_MIN 0.05
param set FW_T_ALT_TC 2
param set FW_T_CLMB_MAX 8
param set FW_T_HRATE_FF 0.5
param set FW_T_SINK_MAX 2.7
param set FW_T_SINK_MIN 2.2
param set FW_T_TAS_TC 2
param set MC_YAW_P 1.6
@@ -28,10 +39,10 @@ then
param set MPC_XY_VEL_I_ACC 4
param set MPC_XY_VEL_D_ACC 0.1
param set NAV_LOITER_RAD 100
param set NAV_ACC_RAD 5
param set NAV_LOITER_RAD 80
param set VT_B_TRANS_DUR 8
param set VT_ELEV_MC_LOCK 0
param set VT_FWD_THRUST_EN 4
param set VT_MOT_ID 1234
param set VT_TILT_TRANS 0.6
@@ -9,12 +9,14 @@
if [ $AUTOCNF = yes ]
then
param set MC_PITCHRATE_P 0.1
param set MC_PITCHRATE_I 0.05
param set MC_PITCH_P 6.0
param set MC_ROLLRATE_P 0.15
param set MC_ROLLRATE_I 0.1
param set MC_ROLL_P 6.0
param set MC_PITCHRATE_P 0.1000
param set MC_PITCHRATE_I 0.0400
param set MC_PITCHRATE_D 0.0010
param set MC_PITCH_P 9.0
param set MC_ROLLRATE_P 0.1000
param set MC_ROLLRATE_I 0.0400
param set MC_ROLLRATE_D 0.0010
param set MC_ROLL_P 9.0
param set MPC_XY_VEL_I_ACC 4
param set MPC_XY_VEL_P_ACC 3
@@ -19,6 +19,7 @@
#
# @maintainer Lorenz Meier <lorenz@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -17,6 +17,7 @@
#
# @maintainer Lorenz Meier <lorenz@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -19,6 +19,7 @@
#
# @maintainer Lorenz Meier <lorenz@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -19,6 +19,7 @@
#
# @maintainer Simon Wilks <simon@uaventure.com>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -7,6 +7,10 @@
#
# @maintainer Roman Bapst <roman@auterion.com>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
. ${R}etc/init.d/rc.vtol_defaults
@@ -16,6 +16,7 @@
#
# @maintainer Simon Wilks <simon@uaventure.com>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -17,6 +17,10 @@
# @output AUX4 Rudder
# @output AUX5 Throttle
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
. ${R}etc/init.d/rc.vtol_defaults
@@ -12,6 +12,10 @@
#
# @maintainer Roman Bapst <roman@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
. ${R}etc/init.d/rc.vtol_defaults
@@ -47,4 +51,4 @@ set MAV_TYPE 19
set MIXER vtol_tailsitter_duo
set PWM_OUT 1234
set PWM_OUT 123456
@@ -7,6 +7,10 @@
#
# @maintainer Roman Bapst <roman@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
. ${R}etc/init.d/rc.vtol_defaults
@@ -25,4 +29,4 @@ set MAV_TYPE 20
set MIXER quad_x_vtol
set PWM_OUT 1234
set PWM_OUT 1234
@@ -17,6 +17,7 @@
# @output AUX4 Rudder
# @output AUX5 Throttle
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -15,6 +15,7 @@
# @output AUX2 Left elevon
# @output AUX3 Motor
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -7,6 +7,7 @@
#
# @maintainer Sander Smeets <sander@droneslab.com>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -7,6 +7,7 @@
#
# @maintainer Sander Smeets <sander@droneslab.com>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -7,6 +7,7 @@
#
# @maintainer Andreas Antener <andreas@uaventure.com>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -16,6 +16,7 @@
# @output MAIN7 Elevon right
# @output MAIN8 Elevon left
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -16,6 +16,10 @@
# @output MAIN7 Pusher motor
# @output MAIN8 Pusher reverse channel
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
. ${R}etc/init.d/rc.vtol_defaults
@@ -50,7 +54,6 @@ then
param set FW_T_SINK_MAX 3
param set FW_T_SINK_MIN 1
param set FW_T_VERT_ACC 6
param set FW_T_HRATE_P 0.1
param set FW_THR_CRUISE 0.70
param set FW_THR_SLEW_MAX 1
param set FW_MAN_P_MAX 30
@@ -49,8 +49,6 @@ then
param set FW_T_HRATE_FF 0
param set FW_T_SINK_MAX 15
param set FW_T_SINK_MIN 3
param set FW_T_THRO_CONST 6
param set FW_T_TIME_CONST 6
param set FW_YR_I 0.1
param set FW_YR_P 0.15
@@ -12,6 +12,7 @@
#
# @maintainer Roman Bapst <roman@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -0,0 +1,49 @@
#!/bin/sh
#
# @name ThunderFly TF-G2
#
# @type Autogyro
# @class Autogyro
#
# @output MAIN2 rotor_head_L
# @output MAIN3 rotor_head_R
# @output MAIN4 rudder
# @output MAIN5 throttle
#
#
# @url https://github.com/ThunderFly-aerospace/TF-G2/
# @maintainer ThunderFly s.r.o., Roman Dvorak <dvorakroman@thunderfly.cz>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
. ${R}etc/init.d/rc.fw_defaults
if [ $AUTOCNF = yes ]
then
param set BAT_CAPACITY 3300
param set BAT_N_CELLS 3
param set PWM_AUX_RATE 50
param set PWM_RATE 50
param set SENS_BOARD_ROT 4
param set FW_AIRSPD_MAX 20
param set FW_AIRSPD_MIN 7
param set FW_AIRSPD_TRIM 13
param set FW_THR_CRUISE 0.8
param set FW_MAN_P_MAX 25
param set FW_MAN_R_MAX 25
param set FW_PR_I 0.02
param set FW_R_LIM 40
param set FW_P_LIM_MAX 25
param set FW_P_LIM_MIN -5
param set FW_P_RMAX_NEG 20
fi
set MIXER TF-G2
set MIXER_AUX pass
@@ -17,6 +17,7 @@
#
# @maintainer Simon Wilks <simon@uaventure.com>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -15,6 +15,7 @@
#
# @maintainer Julian Oes <julian@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -17,6 +17,7 @@
#
# @maintainer Lorenz Meier <lorenz@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -14,6 +14,7 @@
#
# @maintainer Simon Wilks <simon@uaventure.com>
#
# @board px4_fmu-v2 exclude
# @board bitcraze_crazyflie exclude
#
@@ -17,6 +17,7 @@
#
# @maintainer Simon Wilks <simon@uaventure.com>
#
# @board px4_fmu-v2 exclude
# @board bitcraze_crazyflie exclude
#
@@ -7,6 +7,7 @@
#
# @maintainer Lorenz Meier <lorenz@px4.io>
#
# @board px4_fmu-v2 exclude
# @board bitcraze_crazyflie exclude
#
@@ -7,6 +7,7 @@
#
# @maintainer Lorenz Meier <lorenz@px4.io>
#
# @board px4_fmu-v2 exclude
# @board intel_aerofc-v1 exclude
# @board bitcraze_crazyflie exclude
#
@@ -98,7 +98,6 @@ then
param set BAT_V_DIV 10.14
param set BAT_A_PER_V 18.18
#param set CBRK_IO_SAFETY 22027
param set COM_ARM_EKF_AB 0.005
param set COM_DISARM_LAND 2
# Filter settings
@@ -77,7 +77,6 @@ then
param set BAT_SOURCE 0
param set CBRK_IO_SAFETY 22027
#param set COM_ARM_EKF_AB 0.005
#param set COM_DISARM_LAND 3
# Filter settings
@@ -107,7 +107,6 @@ then
param set BAT_V_DIV 10.14
param set BAT_A_PER_V 18.18
#param set CBRK_IO_SAFETY 22027
param set COM_ARM_EKF_AB 0.005
param set COM_DISARM_LAND 2
# Filter settings
@@ -49,7 +49,6 @@ then
# sensor calibration
param set CAL_MAG_SIDES 63
param set SENS_BOARD_ROT 0
param set COM_ARM_EKF_AB 0.0032
# circuit breakers
param set CBRK_IO_SAFETY 22027
@@ -5,8 +5,6 @@
# @type Rover
# @class Rover
#
# @board px4_fmu-v2 exclude
#
# @output MAIN2 steering
# @output MAIN4 throttle
#
@@ -146,7 +146,9 @@ px4_add_romfs_files(
16001_helicopter
# [17000, 17999] Autogyro
17002_TF-AutoG2
17003_TF-G2
24001_dodeca_cox
+1
View File
@@ -62,6 +62,7 @@ mc_att_control start
# Start Multicopter Position Controller.
#
mc_hover_thrust_estimator start
flight_mode_manager start
mc_pos_control start
#
+1
View File
@@ -21,6 +21,7 @@ vtol_att_control start
mc_rate_control start vtol
mc_att_control start vtol
flight_mode_manager start vtol
mc_pos_control start vtol
mc_hover_thrust_estimator start
+49 -56
View File
@@ -183,8 +183,8 @@ else
then
if param compare SYS_AUTOCONFIG 1
then
# Wipe out params except RC*, flight modes, total flight time, accel cal, gyro cal, next flight UUID
param reset_all SYS_AUTOSTART SYS_AUTOCONFIG RC* COM_FLTMODE* LND_FLIGHT_T_* TC_* CAL_ACC* CAL_GYRO* COM_FLIGHT_UUID
# Wipe out params except RC*, flight modes, total flight time, calibration parameters, next flight UUID
param reset_all SYS_AUTO* RC* COM_FLTMODE* LND_FLIGHT* TC_* CAL_ACC* CAL_GYRO* COM_FLIGHT* SYS_PARAM_VER
fi
set AUTOCNF yes
@@ -271,57 +271,6 @@ else
param set SYS_AUTOCONFIG 0
fi
#
# Check if PX4IO present and update firmware if needed.
# Assumption IOFW set to firmware file and IO_PRESENT = no
#
if [ -f $IOFW ]
then
# Check for the mini using build with px4io fw file
# but not a px4IO
if ver hwtypecmp V540 V560
then
param set SYS_USE_IO 0
else
if px4io checkcrc ${IOFW}
then
set IO_PRESENT yes
else
# tune Program PX4IO
tune_control play -t 16 # tune 16 = PROG_PX4IO
if px4io start
then
# Try to safety px4 io so motor outputs don't go crazy.
if ! px4io safety_on
then
# px4io did not respond to the safety command.
px4io stop
fi
fi
if px4io forceupdate 14662 ${IOFW}
then
usleep 10000
tune_control stop
if px4io checkcrc ${IOFW}
then
echo "PX4IO CRC OK after updating"
tune_control play -t 17 # tune 17 = PROG_PX4IO_OK
set IO_PRESENT yes
fi
fi
if [ $IO_PRESENT = no ]
then
echo "PX4IO update failed"
tune_control play -t 18 # tune 18 = PROG_PX4IO_ERR
fi
fi
fi
fi
#
# Set USE_IO flag.
#
@@ -330,10 +279,54 @@ else
set USE_IO yes
fi
if [ $USE_IO = yes -a $IO_PRESENT = no ]
#
# Check if PX4IO present and update firmware if needed.
# Assumption IOFW set to firmware file and IO_PRESENT = no
#
if [ -f $IOFW -a $USE_IO = yes ]
then
echo "PX4IO not found"
tune_control play error
if px4io checkcrc ${IOFW}
then
set IO_PRESENT yes
else
# tune Program PX4IO
tune_control play -t 16 # tune 16 = PROG_PX4IO
if px4io start
then
# Try to safety px4 io so motor outputs don't go crazy.
if ! px4io safety_on
then
# px4io did not respond to the safety command.
px4io stop
fi
fi
if px4io forceupdate 14662 ${IOFW}
then
usleep 10000
tune_control stop
if px4io checkcrc ${IOFW}
then
echo "PX4IO CRC OK after updating"
tune_control play -t 17 # tune 17 = PROG_PX4IO_OK
set IO_PRESENT yes
fi
fi
if [ $IO_PRESENT = no ]
then
echo "PX4IO update failed"
tune_control play -t 18 # tune 18 = PROG_PX4IO_ERR
fi
fi
if [ $USE_IO = yes -a $IO_PRESENT = no ]
then
echo "PX4IO not found"
tune_control play error
fi
fi
#
+39
View File
@@ -0,0 +1,39 @@
TF-G2 autogyro mixer
==================================================
Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
(roll), 1 (pitch) and 3 (thrust).
CH1: empty - fixing cuav nano jittering of 1st output.
Z:
CH2, 3: rotor-head mixer
-------------
Two scalers total (output, roll).
M: 2
O: 10000 10000 0 -10000 10000
S: 0 0 -10000 -10000 0 -10000 10000
S: 0 1 10000 10000 0 -10000 10000
M: 2
O: 10000 10000 0 -10000 10000
S: 0 0 -10000 -10000 0 -10000 10000
S: 0 1 -10000 -10000 0 -10000 10000
CH4: Rudder mixer
------------
Two scalers total (output, yaw).
M: 1
S: 0 2 10000 10000 0 -10000 10000
CH5: Motor speed mixer
-----------------
Two scalers total (output, thrust).
M: 1
S: 0 3 0 20000 -10000 -10000 10000
+2 -3
View File
@@ -12,9 +12,8 @@ if bst start -X
then
fi
if board_adc start
then
fi
board_adc start
system_power start
if sdp3x_airspeed start -X
then
+1 -1
View File
@@ -31,7 +31,7 @@ function spawn_model() {
pushd "$working_dir" &>/dev/null
echo "starting instance $N in $(pwd)"
../bin/px4 -i $N -d "$build_path/etc" -w sitl_${MODEL}_${N} -s etc/init.d-posix/rcS >out.log 2>err.log &
python3 ${src_path}/Tools/sitl_gazebo/scripts/jinja_gen.py ${src_path}/Tools/sitl_gazebo/models/${MODEL}/${MODEL}.sdf.jinja ${src_path}/Tools/sitl_gazebo --mavlink_tcp_port $((4560+${N})) --mavlink_udp_port $((14560+${N})) --output-file /tmp/${MODEL}_${N}.sdf
python3 ${src_path}/Tools/sitl_gazebo/scripts/jinja_gen.py ${src_path}/Tools/sitl_gazebo/models/${MODEL}/${MODEL}.sdf.jinja ${src_path}/Tools/sitl_gazebo --mavlink_tcp_port $((4560+${N})) --mavlink_udp_port $((14560+${N})) --mavlink_id $((1+${N})) --gst_udp_port $((5600+${N})) --video_uri $((5600+${N})) --mavlink_cam_udp_port $((14530+${N})) --output-file /tmp/${MODEL}_${N}.sdf
echo "Spawning ${MODEL}_${N}"
+1 -1
View File
@@ -182,7 +182,7 @@ class FirmwareImage(object):
self._contents.seek(0, os.SEEK_END)
self._length = self._contents.tell()
if self._padding:
fill = self._length % self._padding
fill = self._padding - (self._length % self._padding)
if fill:
self._length += fill
self._padding = fill
+3 -2
View File
@@ -344,8 +344,9 @@ class uploader(object):
try:
self.__getSync(False)
except:
# if it fails we are on a real Serial Port
self.ackWindowedMode = True
# if it fails we are on a real serial port - only leave this enabled on Windows
if _platform.system() == 'Windows':
self.ackWindowedMode = True
self.port.baudrate = self.baudrate_bootloader
+8
View File
@@ -130,6 +130,14 @@ serial_ports = {
"default_baudrate": 0,
},
# WIFI Port (PixRacer)
"WIFI": {
"label": "Wifi Port",
"index": 301,
"default_baudrate": 1, # set default to an unusable value to detect that this serial port has not been configured
},
}
parser = argparse.ArgumentParser(description='Generate Serial params & startup script')
+1 -1
View File
@@ -238,7 +238,7 @@ class Graph(object):
special_cases_pub = [
('replay', r'Replay\.cpp$', None, r'^sub\.orb_meta$'),
('uavcan', r'sensors/.*\.cpp$', r'\bUavcanCDevSensorBridgeBase\([^{]*DEVICE_PATH,([^,)]+)', r'^_orb_topic$'),
('uavcan', r'sensors/.*\.cpp$', None, r'^_orb_topic$'),
]
special_cases_pub = [(a, re.compile(b), re.compile(c) if c is not None else None, re.compile(d))
for a,b,c,d in special_cases_pub]
+1
View File
@@ -45,6 +45,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+2
View File
@@ -45,6 +45,7 @@ px4_add_board(
pwm_out
rc_input
roboclaw
system_power
tap_esc
telemetry # all available telemetry drivers
test_ppm
@@ -59,6 +60,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
@@ -4,6 +4,7 @@
#------------------------------------------------------------------------------
board_adc start
system_power start
# Internal I2C bus
hmc5883 -T -I -R 12 start
@@ -32,6 +32,7 @@ CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F427V=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARCH_STACKDUMP=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
+4 -43
View File
@@ -72,39 +72,24 @@
#define ADC_RC_RSSI_CHANNEL 11
#define ADC_AIRSPEED_VOLTAGE_CHANNEL 15
/* Define Battery 1 Voltage Divider and A per V
*/
/* Define Battery 1 Voltage Divider and A per V */
#define BOARD_BATTERY1_V_DIV (10.177939394f)
#define BOARD_BATTERY1_A_PER_V (15.391030303f)
/* Power supply control and monitoring GPIOs */
// #define GPIO_VDD_5V_PERIPH_EN (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN8)
// #define GPIO_VDD_BRICK_VALID (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN5)
// #define GPIO_VDD_SERVO_VALID (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN7)
// #define GPIO_VDD_3V3_SENSORS_EN (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN3)
// #define GPIO_VDD_5V_HIPOWER_OC (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTE|GPIO_PIN10)
// #define GPIO_VDD_5V_PERIPH_OC (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTE|GPIO_PIN15)
/* Tone alarm output */
#define TONE_ALARM_TIMER 14 /* timer 14 */
#define TONE_ALARM_CHANNEL 1 /* channel 1 */
#define GPIO_TONE_ALARM_IDLE (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN7)
#define GPIO_TONE_ALARM (GPIO_ALT|GPIO_AF9|GPIO_SPEED_2MHz|GPIO_PUSHPULL|GPIO_PORTA|GPIO_PIN7)
/* AUX PWMs
*/
/* AUX PWMs */
#define DIRECT_PWM_OUTPUT_CHANNELS 8
#define DIRECT_INPUT_TIMER_CHANNELS 8
/* USB OTG FS
*
* PA9 OTG_FS_VBUS VBUS sensing
*/
/* USB OTG FS */
#define GPIO_OTGFS_VBUS (GPIO_INPUT|GPIO_FLOAT|GPIO_SPEED_100MHz|GPIO_OPENDRAIN|GPIO_PORTA|GPIO_PIN9)
/* High-resolution timer */
#define HRT_TIMER 8 /* use timer8 for the HRT */
#define HRT_TIMER_CHANNEL 2 /* use capture/compare channel */
@@ -143,46 +128,24 @@
#define SPEKTRUM_RX_AS_UART() px4_arch_configgpio(GPIO_USART1_RX)
#define SPEKTRUM_OUT(_one_true) px4_arch_gpiowrite(GPIO_PPM_IN_AS_OUT, (_one_true))
/* By Providing BOARD_ADC_USB_CONNECTED (using the px4_arch abstraction)
* this board support the ADC system_power interface, and therefore
* provides the true logic GPIO BOARD_ADC_xxxx macros.
*/
#define BOARD_ADC_USB_CONNECTED (px4_arch_gpioread(GPIO_OTGFS_VBUS))
#define BOARD_ADC_BRICK_VALID (1)
#define BOARD_ADC_SERVO_VALID (1)
#define BOARD_ADC_PERIPH_5V_OC (0)
#define BOARD_ADC_HIPOWER_5V_OC (0)
#define BOARD_HAS_PWM DIRECT_PWM_OUTPUT_CHANNELS
/* This board provides a DMA pool and APIs */
#define BOARD_DMA_ALLOC_POOL_SIZE 5120
/* This board provides the board_on_reset interface */
#define BOARD_HAS_ON_RESET 1
__BEGIN_DECLS
/****************************************************************************************************
* Public Types
****************************************************************************************************/
/****************************************************************************************************
* Public data
****************************************************************************************************/
#ifndef __ASSEMBLY__
/****************************************************************************************************
* Public Functions
****************************************************************************************************/
/****************************************************************************************************
* Name: stm32_spiinitialize
*
* Description:
* Called to configure SPI chip select GPIO pins for the PX4FMU board.
* Called to configure SPI chip select GPIO pins for the board.
*
****************************************************************************************************/
@@ -190,10 +153,8 @@ extern void stm32_spiinitialize(void);
extern void stm32_usbinitialize(void);
#define board_peripheral_reset(ms)
#include <px4_platform_common/board_common.h>
#endif /* __ASSEMBLY__ */
+1
View File
@@ -64,6 +64,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+1
View File
@@ -56,6 +56,7 @@ px4_add_board(
attitude_estimator_q
commander
ekf2
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+1
View File
@@ -63,6 +63,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+1
View File
@@ -56,6 +56,7 @@ px4_add_board(
attitude_estimator_q
commander
ekf2
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+1
View File
@@ -59,6 +59,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+3 -1
View File
@@ -8,7 +8,9 @@ param set CBRK_SUPPLY_CHK 894281
if [ $AUTOCNF = yes ]
then
# Multi-EKF
param set EKF2_MULTI_IMU 3
param set SENS_IMU_MODE 0
fi
set LOGGER_BUF 64
@@ -52,6 +52,7 @@ CONFIG_ARMV7M_BASEPRI_WAR=y
CONFIG_ARMV7M_DCACHE=y
CONFIG_ARMV7M_DTCM=y
CONFIG_ARMV7M_ICACHE=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
+2 -30
View File
@@ -49,11 +49,6 @@
#include <stm32_gpio.h>
/* Configuration ************************************************************************************/
#define BOARD_HAS_NBAT_V 1 // Only one Vbat to ADC
#define BOARD_HAS_NBAT_I 0 // No Ibat ADC
/*
* ADC channels
*
@@ -88,18 +83,14 @@
#define ADC_CHANNELS \
((1 << ADC_BATTERY1_VOLTAGE_CHANNEL))
/* Define Battery 1 Voltage Divider and A per V
*/
/* Define Battery 1 Voltage Divider and A per V */
#define BOARD_BATTERY1_V_DIV (10.133333333f)
#define BOARD_BATTERY1_A_PER_V (36.367515152f)
/* HW has to large of R termination on ADC todo:change when HW value is chosen */
#define BOARD_ADC_OPEN_CIRCUIT_V (5.6f)
/* PWM
*/
/* PWM */
#define DIRECT_PWM_OUTPUT_CHANNELS 9
#define DIRECT_INPUT_TIMER_CHANNELS 9
@@ -110,7 +101,6 @@
#define HRT_TIMER_CHANNEL 1 /* use capture/compare channel 3 */
/* RC Serial port */
#define RC_SERIAL_PORT "/dev/ttyS4"
/* Power switch controls ******************************************************/
@@ -118,27 +108,9 @@
#define SDIO_SLOTNO 0 /* Only one slot */
#define SDIO_MINOR 0
/* SD card bringup does not work if performed on the IDLE thread because it
* will cause waiting. Use either:
*
* CONFIG_LIB_BOARDCTL=y, OR
* CONFIG_BOARD_INITIALIZE=y && CONFIG_BOARD_INITTHREAD=y
*/
#if defined(CONFIG_BOARD_INITIALIZE) && !defined(CONFIG_LIB_BOARDCTL) && !defined(CONFIG_BOARD_INITTHREAD)
# warning SDIO initialization cannot be perfomed on the IDLE thread
#endif
/* AV-X_V1 never powers off the Servo rail */
#define BOARD_ADC_SERVO_VALID (1)
#define ADC_BATTERY_VOLTAGE_CHANNEL 0
#define ADC_BATTERY_CURRENT_CHANNEL 1 // TODO: review
#define BOARD_ADC_PERIPH_5V_OC (!px4_arch_gpioread(GPIO_nVDD_5V_PERIPH_OC))
#define BOARD_ADC_HIPOWER_5V_OC (!px4_arch_gpioread(GPIO_nVDD_5V_HIPOWER_OC))
#define BOARD_HAS_PWM DIRECT_PWM_OUTPUT_CHANNELS
/* This board provides a DMA pool and APIs */
+1
View File
@@ -40,6 +40,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+1
View File
@@ -21,6 +21,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
land_detector
landing_target_estimator
load_mon
@@ -31,6 +31,7 @@ CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F405RG=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARCH_STACKDUMP=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
+1 -10
View File
@@ -109,13 +109,6 @@
*/
#define GPIO_OTGFS_VBUS (GPIO_INPUT|GPIO_FLOAT|GPIO_SPEED_100MHz|GPIO_OPENDRAIN|GPIO_PORTA|GPIO_PIN9)
/*
* ADC channels
*
* These are the channel numbers of the ADCs of the microcontroller that can be used by the Px4 Firmware in the adc driver
*/
#define ADC_CHANNELS 0
/* Tone alarm output : These are only applicable when the buzzer deck is attached */
#define TONE_ALARM_TIMER 5 /* timer 5 */
#define TONE_ALARM_CHANNEL 3 /* channel 3 */
@@ -123,9 +116,7 @@
#define GPIO_TONE_ALARM (GPIO_ALT|GPIO_AF2|GPIO_SPEED_2MHz|GPIO_PUSHPULL|GPIO_PORTA|GPIO_PIN2)
#define GPIO_TONE_ALARM_NEG (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN3)
/* PWM
*/
/* PWM */
#define DIRECT_PWM_OUTPUT_CHANNELS 4
/* This board overrides the defaults by providing
+6 -26
View File
@@ -27,45 +27,25 @@ px4_add_board(
ARCHITECTURE cortex-m4
ROMFSROOT cannode
UAVCAN_INTERFACES 1
SERIAL_PORTS
GPS1:/dev/ttyS1
DRIVERS
#adc
barometer/ms5611
bootloaders
gps
magnetometer/rm3100
#safety_button
#tone_alarm
safety_button
tone_alarm
uavcannode
MODULES
#ekf2
#load_mon
#sensors
#temperature_compensation
load_mon
SYSTEMCMDS
#bl_update
#dmesg
#dumpfile
#esc_calib
#hardfault_log
#i2cdetect
#led_control
#mft
#mixer
#motor_ramp
#motor_test
#mtd
#nshterm
i2cdetect
led_control
param
perf
reboot
#reflect
#sd_bench
#shutdown
top
topic_listener
#tune_control
tune_control
ver
work_queue
)
+1 -1
View File
@@ -3,7 +3,7 @@
# board sensors init
#------------------------------------------------------------------------------
#board_adc start
gps start -d /dev/ttyS1 -g 38400 -p ubx
# Internal SPI
ms5611 -s start
@@ -58,8 +58,8 @@
* LSE - not installed
*/
#define STM32_BOARD_USEHSE 1
#define STM32_BOARD_XTAL 8000000
#define STM32_BOARD_USEHSE 1
#define STM32_BOARD_XTAL 16000000
#define STM32_HSE_FREQUENCY STM32_BOARD_XTAL
#define STM32_HSI_FREQUENCY 16000000ul
@@ -128,40 +128,22 @@
/* Alternate function pin selections ************************************************/
/*
* UARTs.
*/
/* UARTs */
#define GPIO_USART1_RX GPIO_USART1_RX_2
#define GPIO_USART1_TX GPIO_USART1_TX_2
#define GPIO_USART2_RX GPIO_USART2_RX_1
#define GPIO_USART2_TX GPIO_USART2_TX_1
/*
* CAN
*
* CAN1 is routed to the onboard transceiver.
*/
/* CAN */
#define GPIO_CAN1_RX GPIO_CAN1_RX_2
#define GPIO_CAN1_TX GPIO_CAN1_TX_2
/*
* I2C
*
* The optional _GPIO configurations allow the I2C driver to manually
* reset the bus to clear stuck slaves. They match the pin configuration,
* but are normally-high GPIOs.
*/
/* I2C */
#define GPIO_I2C3_SCL GPIO_I2C3_SCL_2
#define GPIO_I2C3_SDA GPIO_I2C3_SDA_2
#define GPIO_I2C3_SCL_GPIO (GPIO_OUTPUT|GPIO_OPENDRAIN|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTA|GPIO_PIN8)
#define GPIO_I2C3_SDA_GPIO (GPIO_OUTPUT|GPIO_OPENDRAIN|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN4)
/*
* SPI
*
* There are sensors on SPI1, and SPI2 is connected to the FRAM.
*/
/* SPI */
#define GPIO_SPI1_MISO (GPIO_SPI1_MISO_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_MOSI (GPIO_SPI1_MOSI_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_SCK (GPIO_SPI1_SCK_1|GPIO_SPEED_50MHz)
@@ -28,6 +28,7 @@ CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F412CE=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARCH_STACKDUMP=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
@@ -71,13 +71,15 @@ SECTIONS
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
. = ALIGN(32);
/*
This signature provides the bootloader with a way to delay booting
*/
_bootdelay_signature = ABSOLUTE(.);
FILL(0xffecc2925d7d05c5)
. += 8;
. = 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)
@@ -32,6 +32,7 @@
############################################################################
if("${PX4_BOARD_LABEL}" STREQUAL "canbootloader")
add_library(drivers_board
boot_config.h
boot.c
+4 -3
View File
@@ -48,16 +48,17 @@
#include <stdint.h>
/* BUTTON *************************************************************************** */
#define BUTTON_BOOT0n (GPIO_INPUT|GPIO_FLOAT|GPIO_PORTB|GPIO_PIN3|GPIO_EXTI)
#define IRQBUTTON BUTTON_BOOT0_BIT
#define BUTTON_SAFETY /* PB3 */ (GPIO_INPUT|GPIO_PULLDOWN|GPIO_PORTB|GPIO_PIN3|GPIO_EXTI)
#define GPIO_RGB_S /* PB0 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN0)
/* CAN Silence
*
* Silent mode control \ ESC Mux select
*/
#define GPIO_CAN1_SILENT_S0 /* PB5 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN5)
#define GPIO_CAN_CTRL /* PB5 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_PORTB|GPIO_PIN5|GPIO_OUTPUT_CLEAR)
#define GPIO_LED_SAFETY (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTB|GPIO_PIN1)
#define GPIO_BTN_SAFETY (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTB|GPIO_PIN3)
/* Tone alarm output. */
#define TONE_ALARM_TIMER 2 /* timer 2 */
+19 -19
View File
@@ -65,7 +65,7 @@ __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_CAN_CTRL);
stm32_configgpio(GPIO_CAN1_SILENT_S0);
putreg32(getreg32(STM32_RCC_APB1RSTR) | RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
putreg32(getreg32(STM32_RCC_APB1RSTR) & ~RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
@@ -155,33 +155,33 @@ size_t board_get_hardware_version(uavcan_HardwareVersion_t *hw_version)
#define led(n, code, r , g , b, h) {.red = (r),.green = (g), .blue = (b),.hz = (h)}
typedef begin_packed_struct struct led_t {
uint16_t red : 5;
uint16_t green : 6;
uint16_t blue : 5;
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, 10, 63, 31, 255),
led(2, autobaud_start, 0, 63, 0, 1),
led(3, autobaud_end, 0, 63, 0, 2),
led(4, allocation_start, 0, 0, 31, 2),
led(5, allocation_end, 0, 63, 31, 3),
led(6, fw_update_start, 15, 63, 31, 3),
led(7, fw_update_erase_fail, 15, 63, 15, 3),
led(8, fw_update_invalid_response, 31, 0, 0, 1),
led(9, fw_update_timeout, 31, 0, 0, 2),
led(a, fw_update_invalid_crc, 31, 0, 0, 4),
led(b, jump_to_app, 0, 63, 0, 10),
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 << 3,
i2l[indication].green << 2,
i2l[indication].blue << 3,
rgb_led(i2l[indication].red,
i2l[indication].green,
i2l[indication].blue,
i2l[indication].hz);
}
+2 -6
View File
@@ -101,7 +101,7 @@
#define OPT_RESTART_TIMEOUT_MS 20000
/* Reserved for the Booloader */
#define OPT_BOOTLOADER_SIZE_IN_K (1024*8)
#define OPT_BOOTLOADER_SIZE_IN_K (1024*64)
/* Reserved for the application out of the total
* system flash minus the BOOTLOADER_SIZE_IN_K
@@ -132,9 +132,5 @@
/* Bootloader Option*****************************************************************
*
* GPIO Function MPU Board
* Pin # Name
* -- ----- -------------------------------- ----------------------------
* * PC[09] PC9/TIM3_CH4 40 BOOT0
*/
#define GPIO_GETNODEINFO_JUMPER (BUTTON_BOOT0n&~(GPIO_EXTI))
#define GPIO_GETNODEINFO_JUMPER (BUTTON_SAFETY & ~GPIO_EXTI)
+3
View File
@@ -90,6 +90,9 @@ stm32_boardinitialize(void)
stm32_configgpio(GPIO_CAN1_SILENT_S0);
stm32_configgpio(GPIO_LED_SAFETY);
stm32_configgpio(GPIO_BTN_SAFETY);
// Configure SPI all interfaces GPIO & enable power.
stm32_spiinitialize();
}
+89 -23
View File
@@ -39,17 +39,83 @@
#include <arch/board/board.h>
#include <hardware/stm32_tim.h>
#include <dwt.h>
#include <nvic.h>
#include "led.h"
#define TMR_BASE STM32_TIM3_BASE
#define TMR_FREQUENCY STM32_APB1_TIM3_CLKIN
#define TMR_BASE STM32_TIM1_BASE
#define TMR_FREQUENCY STM32_APB2_TIM1_CLKIN
#define TMR_REG(o) (TMR_BASE+(o))
#define LED_COUNT 8 // Eight LEDs in ring
typedef union {
uint8_t grb[3];
uint32_t l;
} led_data_t;
static uint8_t off[] = {0, 0, 0};
#define REG(_addr) (*(volatile uint32_t *)(_addr))
#define rDEMCR REG(NVIC_DEMCR)
#define rDWT_CTRL REG(DWT_CTRL)
#define rDWT_CNT REG(DWT_CYCCNT)
#define PORT_B REG(STM32_GPIOB_ODR)
#define D0 REG(STM32_GPIOB_ODR) &= ~1;
#define D1 REG(STM32_GPIOB_ODR) |= 1;
#define DWT_DEADLINE(t) rDWT_CNT + (t)
#define DWT_WAIT(v, D) while((rDWT_CNT - (v)) < (D));
#define T0H (STM32_SYSCLK_FREQUENCY/3333333)
#define T1H (STM32_SYSCLK_FREQUENCY/1666666)
#define TW (STM32_SYSCLK_FREQUENCY/800000)
static void setled(uint8_t *p, int count)
{
rDEMCR |= NVIC_DEMCR_TRCENA;
rDWT_CTRL |= DWT_CTRL_CYCCNTENA_MASK;
while (count--) {
uint8_t l = *p++;
uint32_t deadline = DWT_DEADLINE(TW);
for (uint32_t mask = (1 << 7); mask != 0; mask >>= 1) {
DWT_WAIT(deadline, TW);
deadline = rDWT_CNT;
D1;
if (l & mask) {
DWT_WAIT(deadline, T1H);
} else {
DWT_WAIT(deadline, T0H);
}
D0;
}
DWT_WAIT(deadline, TW);
}
}
static led_data_t led_data = {0};
static int timerInterrupt(int irq, void *context, void *arg)
{
putreg16(~getreg16(TMR_REG(STM32_GTIM_SR_OFFSET)), TMR_REG(STM32_GTIM_SR_OFFSET));
static int d2 = 1;
setled((d2++ & 1) ? led_data.grb : off, sizeof(led_data.grb));
return 0;
}
void rgb_led(int r, int g, int b, int freqs)
{
long fosc = TMR_FREQUENCY;
long prescale = 2048;
long prescale = 1536;
long p1s = fosc / prescale;
long p0p5s = p1s / 2;
uint16_t val;
@@ -58,8 +124,15 @@ void rgb_led(int r, int g, int b, int freqs)
if (!once) {
once = 1;
/* Enabel Clock to Block */
modifyreg32(STM32_RCC_APB1ENR, 0, RCC_APB1ENR_TIM3EN);
stm32_configgpio(GPIO_RGB_S);
for (int i = 0; i < LED_COUNT; i++) {
setled(off, sizeof(off));
}
/* Enable Clock to Block */
modifyreg32(STM32_RCC_APB2ENR, 0, RCC_APB2ENR_TIM1EN);
/* Reload */
val = getreg16(TMR_REG(STM32_BTIM_EGR_OFFSET));
@@ -72,28 +145,21 @@ void rgb_led(int r, int g, int b, int freqs)
/* Enable STM32_TIM_SETMODE*/
putreg16(ATIM_CR1_CEN | ATIM_CR1_ARPE, TMR_REG(STM32_BTIM_CR1_OFFSET));
putreg32(p0p5s + 1, TMR_REG(STM32_BTIM_ARR_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));
// TODO: verify
stm32_configgpio(GPIO_TIM3_CH1OUT_1);
stm32_configgpio(GPIO_TIM3_CH2OUT_1);
stm32_configgpio(GPIO_TIM3_CH3OUT_1);
irq_attach(STM32_IRQ_TIM1CC, timerInterrupt, NULL);
up_enable_irq(STM32_IRQ_TIM1CC);
putreg16(GTIM_DIER_CC1IE, TMR_REG(STM32_GTIM_DIER_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));
long p = freqs == 0 ? p1s + 1 : p0p5s / freqs;
putreg32(p + 1, TMR_REG(STM32_BTIM_ARR_OFFSET));
putreg32(p, TMR_REG(STM32_GTIM_CCR1_OFFSET));
led_data.grb[0] = g;
led_data.grb[1] = r;
led_data.grb[2] = b;
setled(led_data.grb, sizeof(led_data.grb));
val = getreg16(TMR_REG(STM32_BTIM_CR1_OFFSET));
+2
View File
@@ -50,6 +50,7 @@ px4_add_board(
rc_input
roboclaw
safety_button
system_power
tap_esc
telemetry # all available telemetry drivers
test_ppm
@@ -64,6 +65,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+6
View File
@@ -31,6 +31,12 @@ then
param set BAT1_A_PER_V 24
param set BAT2_A_PER_V 24
# Multi-EKF
param set EKF2_MULTI_IMU 3
param set SENS_IMU_MODE 0
param set EKF2_MULTI_MAG 3
param set SENS_MAG_MODE 0
# Enable IMU thermal control
param set SENS_EN_THERMAL 1
fi
+1
View File
@@ -3,6 +3,7 @@
# board specific sensors init
#------------------------------------------------------------------------------
board_adc start
system_power start
# SPI1 (internal)
rm3100 -s start
@@ -20,6 +20,7 @@ CONFIG_ARCH_CHIP_STM32H7=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARMV7M_BASEPRI_WAR=y
CONFIG_ARMV7M_ICACHE=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
@@ -35,6 +35,7 @@ CONFIG_ARMV7M_BASEPRI_WAR=y
CONFIG_ARMV7M_DCACHE=y
CONFIG_ARMV7M_DTCM=y
CONFIG_ARMV7M_ICACHE=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
-2
View File
@@ -110,8 +110,6 @@
#define DIRECT_PWM_OUTPUT_CHANNELS 8
/* Power supply control and monitoring GPIOs */
#define BOARD_NUMBER_BRICKS 2
#define GPIO_nPOWER_IN_ADC /* PG1 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN1)
#define GPIO_nPOWER_IN_CAN /* PG2 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN2)
#define GPIO_nPOWER_IN_C /* PG0 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN0)
+2
View File
@@ -53,6 +53,7 @@ px4_add_board(
rc_input
roboclaw
safety_button
system_power
tap_esc
telemetry # all available telemetry drivers
test_ppm
@@ -67,6 +68,7 @@ px4_add_board(
dataman
ekf2
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
+6
View File
@@ -31,6 +31,12 @@ then
param set BAT1_A_PER_V 24
param set BAT2_A_PER_V 24
# Multi-EKF
param set EKF2_MULTI_IMU 3
param set SENS_IMU_MODE 0
param set EKF2_MULTI_MAG 3
param set SENS_MAG_MODE 0
# Enable IMU thermal control
param set SENS_EN_THERMAL 1
fi
+1
View File
@@ -3,6 +3,7 @@
# CUAV X7Pro specific board sensors init
#------------------------------------------------------------------------------
board_adc start
system_power start
# SPI1 (internal)
#adis16470 -s start
@@ -20,6 +20,7 @@ CONFIG_ARCH_CHIP_STM32H7=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARMV7M_BASEPRI_WAR=y
CONFIG_ARMV7M_ICACHE=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
@@ -35,6 +35,7 @@ CONFIG_ARMV7M_BASEPRI_WAR=y
CONFIG_ARMV7M_DCACHE=y
CONFIG_ARMV7M_DTCM=y
CONFIG_ARMV7M_ICACHE=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
+1 -6
View File
@@ -110,8 +110,6 @@
#define DIRECT_PWM_OUTPUT_CHANNELS 8
/* Power supply control and monitoring GPIOs */
#define BOARD_NUMBER_BRICKS 2
#define GPIO_nPOWER_IN_ADC /* PG1 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN1)
#define GPIO_nPOWER_IN_CAN /* PG2 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN2)
#define GPIO_nPOWER_IN_C /* PG0 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN0)
@@ -179,10 +177,7 @@
#define GPIO_LED_SAFETY FMU_LED_AMBER
/* By Providing BOARD_ADC_USB_CONNECTED (using the px4_arch abstraction)
* this board support the ADC system_power interface, and therefore
* provides the true logic GPIO BOARD_ADC_xxxx macros.
*/
#define BOARD_ADC_USB_CONNECTED (px4_arch_gpioread(GPIO_OTGFS_VBUS))
#define BOARD_ADC_USB_VALID (!px4_arch_gpioread(GPIO_nVDD_USB_VALID))
#define BOARD_ADC_BRICK1_VALID (!px4_arch_gpioread(GPIO_nVDD_BRICK1_VALID))
@@ -52,6 +52,7 @@ px4_add_board(
px4io
roboclaw
rpm
system_power
tap_esc
telemetry # all available telemetry drivers
test_ppm
@@ -67,6 +68,7 @@ px4_add_board(
ekf2
esc_battery
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
@@ -52,6 +52,7 @@ px4_add_board(
px4io
roboclaw
rpm
system_power
tap_esc
telemetry # all available telemetry drivers
test_ppm
@@ -67,6 +68,7 @@ px4_add_board(
ekf2
esc_battery
events
flight_mode_manager
fw_att_control
fw_pos_control_l1
land_detector
@@ -31,6 +31,12 @@ then
param set BAT1_A_PER_V 17
param set BAT2_A_PER_V 17
# Multi-EKF
param set EKF2_MULTI_IMU 3
param set SENS_IMU_MODE 0
param set EKF2_MULTI_MAG 3
param set SENS_MAG_MODE 0
# Disable IMU thermal control
param set SENS_EN_THERMAL 0
fi
@@ -3,6 +3,7 @@
# Board specific sensors init
#------------------------------------------------------------------------------
board_adc start
system_power start
# SPI4
ms5611 -s -b 4 start
@@ -20,6 +20,7 @@ CONFIG_ARCH_CHIP_STM32H7=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARMV7M_BASEPRI_WAR=y
CONFIG_ARMV7M_ICACHE=y
CONFIG_ARMV7M_LAZYFPU=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y

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