Compare commits

..

107 Commits

Author SHA1 Message Date
Jaeyoung Lim 0bdd780bdd Set feedforward heightrate setpoint in offboard mode 2023-02-24 08:17:27 +01:00
Jaeyoung Lim 7e49147bcf Fix feedforward acceleration setpoints for fixedwing offboard position
This commit fixes feedforward acceleration setpoints for fixedwing offboard position control.

Previously when acceleration feedforward inputs were sent, negative curvature accelerations were not being computed properly
2022-10-19 09:15:13 +02:00
Daniel Agar b71fc63162 ekf2: fix sideslip timeout (typo) 2022-10-18 18:38:25 -04:00
Daniel Agar 0d2ff6e224 ekf2: test ekf_logger further reduce std::precision to minimize false positives 2022-10-18 14:19:16 -04:00
Daniel Agar 535415a537 ekf2: add OF estimator aid src status 2022-10-18 14:19:16 -04:00
Matthias Grob 75c63aee2a Fix confusion between trajectory_setpoint and vehicle_local_postion_setpoint 2022-10-17 16:18:00 -04:00
Daniel Agar 7c237fca74 boards: px4_sitl use Mavlink development dialect 2022-10-17 16:16:36 -04:00
Daniel Agar 743200df22 mavlink: move mavlink dialect selection to kconfig 2022-10-17 16:16:36 -04:00
Daniel Agar d792a3ff5b simulator_mavlink: use existing development/common mavlink generation if available 2022-10-17 16:16:36 -04:00
Hamish Willee 2a9801f191 Default mavlink dialect should be common.xml 2022-10-17 16:16:36 -04:00
bresch 8b9ac2d7f3 ekf2: remove old mag 3D fusion auto-code 2022-10-17 16:14:56 -04:00
bresch 77a36219c6 ekf2_test: compare 3D mag fusion sympy vs symforce 2022-10-17 16:14:56 -04:00
bresch b92cbe12a0 ekf2: migrate mag 3D fusion to symforce
ekf2: merge mag 3d innov var, Hx and Kx computation to reduce flash

Slightly less code produced, almost no performance change

ekf2_mag3D: do not pre-compute Kalman gains

The vector of Kalaman gains is not too expensive to compute using
matrix-vector multiplication. Pre-generating it using CSE takes a lot of
flash space for little benefit.
2022-10-17 16:14:56 -04:00
Silvan Fuhrer 5ea8c6e507 FlightTaskAuto: remove unused _getTargetVelocityXY()
Inclusive velocity_valid field in position_setpoint message that's then
no longer needed.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-17 16:12:15 -04:00
Silvan Fuhrer 42c613a0c7 position_setpoint.msg: remove unused alt_valid
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-17 16:12:15 -04:00
Silvan Fuhrer 42dd9b5063 position_setpoint.msg: remove unused velocity_frame field
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-17 16:12:15 -04:00
Daniel Agar 0d6766d14d limit vehicle_command subscription updates per cycle
- this is a precaution to eliminate the possibility of getting stuck in
a loop trying to keep up with a high rate publication that could be
coming from a higher priority task
2022-10-17 16:10:51 -04:00
Daniel Agar 677f3e9294 sensors/vehicle_optical_flow: limit gyro updates and generation lost error per cycle
- in the worst case scenario printing the error message can take longer than the next gyro publication, so combined with an infinite loop you could get stuck here
2022-10-17 13:45:04 -04:00
Alex Klimaj 8545164869 sensors/vehicle_optical_flow: only get gyro if optical flow delta angle not available (#20416) 2022-10-17 10:23:36 -04:00
Daniel Agar 116bb6049f ekf2: fusion helper consistency
- yaw fusion use measurementUpdate()
 - fuseVelPosHeight() respect _accel_bias_inhibit (like measurementUpdate())
2022-10-17 10:17:31 -04:00
Silvan Fuhrer 7bc90c7f00 FW rate controller gains: put default for all IMAX gains to 0.4
The previous default for yaw and roll was 0.2, which is very low, and for wheel was
1, which is very high. A value of 0.4 makes sense to me for all axes.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-17 10:27:09 +02:00
Silvan Fuhrer 4bbe8f3c0d FW rate controller gains: open up some limitis for the rate controller gains
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-17 10:27:09 +02:00
Silvan Fuhrer e2d1e79614 FW rate controller gains: reduce max FW_YR_I from 50 to 1
I guess this was a left over from times where the controller had a completely different structure,
a value of 50 is well outside of reasonable range (50x the default).

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-17 10:27:09 +02:00
Silvan Fuhrer ea44c89366 FW rate controller gains: reduce max FF gains to 1
The previous max of 10 for the FF gains seems a bit very high for me, well outside
of reasonable reange.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-17 10:27:09 +02:00
bresch 458e5a6b0e ekf2: update change indicator 2022-10-14 11:42:23 -04:00
bresch 1b4092abbb symforce: temporarily remove custom cmake command
otherwise the generated files are removed with make clean
2022-10-14 11:42:23 -04:00
bresch a8a3107c05 ekf2: remove old covariance prediction code 2022-10-14 11:42:23 -04:00
bresch df084d65e3 ekf2_test: compare covariance prediction sympy vs symforce 2022-10-14 11:42:23 -04:00
bresch a4e511b90e ekf2: migrate covariance prediction to SymForce 2022-10-14 11:42:23 -04:00
chris1seto 079dfdf209 drivers/osd/msp_osd: cleanup and small fixes/additions (#20399)
- Fixed clearing arming word if flightmode unknown
 - Added power and cell voltage elements
 - New OSD layout
 - Fixed home direction/distance are now correct

Co-authored-by: Chris Seto <chris1seto@gmail.com>
2022-10-14 10:54:14 -04:00
Beat Küng 3c290d812d commander: use printRejectMode() also for rtl, takeoff, land & mission commands 2022-10-13 16:05:25 -04:00
Beat Küng d542ffc10c refactor vehicle_status_flags: rename to failsafe_flags 2022-10-13 16:05:25 -04:00
Beat Küng f9c8e760b1 CI: add failsafe web build & deployment to the user guide 2022-10-13 16:05:25 -04:00
chris1seto 0ddba3ea90 Fix Discord badge not a link in README (#20406)
* Add link to image
* Update link to nice permalink

Co-authored-by: Chris Seto <chris1seto@gmail.com>
2022-10-13 11:05:28 -07:00
Daniel Agar 2de990fd4b estimator_aid_source split GNSS pos (3d) -> pos (2d) + hgt
- per estimator air source status only keep a single set of flags and
timestamp that applies to the entire source
2022-10-13 11:28:50 -04:00
David Sidrane 8a9a091ff3 nxp_fmurt1062-v1:Timer configuration for 1 channel per group (timer) 2022-10-13 08:17:51 +02:00
David Sidrane 3be8d52c8e imxrt:io_timers Support 1 channel per group (timer) 2022-10-13 08:17:51 +02:00
David Sidrane 7f7137320a fix imxrt: use 1:1 timer group to channel association 2022-10-13 08:17:51 +02:00
chris1seto 7e9ec325f7 Convert README to Discord (#20400) 2022-10-12 21:41:00 -07:00
bresch bdd043f27f ekf2: fix sideslip fusion sign 2022-10-12 16:14:47 +02:00
bresch 53865118fb ekf2: remove old sideslip fusion code 2022-10-12 09:55:35 -04:00
bresch f7c749c9cd ekf2_test: compare sideslip fusion of Sympy and SymForce 2022-10-12 09:55:35 -04:00
bresch d0f92bfbd5 ekf2_test: create helper functions for auto-generated code diff 2022-10-12 09:55:35 -04:00
bresch 5f54f6fcda ekf2: migrate sideslip fusion to SymForce
- split fusion into update (compute innov and innov_var) and actual fusion to the state vector
- use estimator_aid_source_1d struct to group the data
2022-10-12 09:55:35 -04:00
Beat Küng c09be0f0ac airframes: add r1 again
This was dropped in f454dcef6b
2022-10-12 07:35:35 +02:00
Beat Küng 9b7a8d4568 vehicle_status_flags: add group 'Other' 2022-10-11 22:31:20 -04:00
Beat Küng f7819f5dba commander: reorder update calls
Moves the arming checks before the command handling.
This reduces the chance of race conditions. However it does not prevent
them! The SDK will need to check when offboard is ready to run/arm to fix
this.
Specifically this is for sitl offboard tests, where offboard_control_mode
is updated and immediately after a mode switch into offboard is commanded.
2022-10-11 22:31:20 -04:00
Beat Küng 38d3739b6d refactor commander: rename rc_signal_lost -> manual_control_signal_lost, data_link_lost -> gcs_connection_lost 2022-10-11 22:31:20 -04:00
Beat Küng e2d8ca73a5 commander: add unit tests for failsafe state machine 2022-10-11 22:31:20 -04:00
Beat Küng 3d1da597dd commander: run arming checks on _offboard_control_mode_sub update 2022-10-11 22:31:20 -04:00
Beat Küng 6ee2252b8c events: handle events being generated before a mavlink module started
- do not print dropped events warnings
- make sure current sequence is still sent with reset flag
2022-10-11 22:31:20 -04:00
Beat Küng 3fcdf40a47 events: use PRIx32 to print uint32 2022-10-11 22:31:20 -04:00
Beat Küng acaa50a448 geofence: add and report reason for violation 2022-10-11 22:31:20 -04:00
mcsauder ebc88afe46 Apply Google Style to Commander Private methods, rename geofence message geofence_violation to primary_geofence_breached. 2022-10-11 22:31:20 -04:00
Beat Küng 693af897b3 commander: check if battery was already disconnected on arming
If so, don't report.
Happens e.g. with USB powered pixhawk.
2022-10-11 22:31:20 -04:00
Beat Küng 24142bc014 commander: RcCalibrationChecks: avoid param access on each cycle
reduces cpu usage a bit
2022-10-11 22:31:20 -04:00
Beat Küng c72c580a0b commander: run arming checks @ 10Hz
Required for things like RC loss.
2022-10-11 22:31:20 -04:00
Beat Küng 6fda555cba commander: move ownership of vehicle_status_flags_s to HealthAndArmingChecks 2022-10-11 22:31:20 -04:00
Beat Küng cf2eb69d25 px4events/srcparser: ensure message is a string literal 2022-10-11 22:31:20 -04:00
Beat Küng 500a896a56 commander: print reason for mode rejection & report for GCS switches as well 2022-10-11 22:31:20 -04:00
Beat Küng e4bb219d10 vehicle_status_flags: cleanup message, move non-failsafe flags to vehicle_status 2022-10-11 22:31:20 -04:00
Beat Küng ae6377dfa0 mission_result: remove unused fields 2022-10-11 22:31:20 -04:00
Beat Küng 455b885f86 commander: use new failsafe state machine and add user intention class 2022-10-11 22:31:20 -04:00
Beat Küng a04230faa1 commander: add failsafe state machine with webassembly simulation
to run the simulation:
install sdk: https://emscripten.org/docs/getting_started/downloads.html
make run_failsafe_web_server
open http://0.0.0.0:8000/

Co-authored-by: Konrad <konrad@auterion.com>
2022-10-11 22:31:20 -04:00
Beat Küng 82911e48be fix commander: check estimator type & avoid timestamp wrap-around
Before it was possible that the publication timestamp was never than 'now',
leading to wrap-around.
2022-10-11 22:31:20 -04:00
Beat Küng 27f8298bb9 fix commander: add local position requirement to NAVIGATION_STATE_AUTO_LAND 2022-10-11 22:31:20 -04:00
Beat Küng 57c7b5e843 flight_mode_manager: reduce error verbosity & remove mode switching
While disarmed, commander allows to be in any mode now.
2022-10-11 22:31:20 -04:00
Beat Küng 31dfdea12e commander: remove state_machine_helper tests 2022-10-11 22:31:20 -04:00
Beat Küng e9387cac1d mavlink: move get_px4_custom_mode to px4_custom_mode.h 2022-10-11 22:31:20 -04:00
Silvan Fuhrer 9159f020cb mavlink local_position_ned: always publish on update, not just when xy and v_xy valid
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-11 00:47:32 -04:00
Daniel Agar ce609144b0 simulation/gz_bridge: fix implicit floating-point conversions 2022-10-09 14:11:19 -04:00
Daniel Agar 9010029e0d lib/drivers/device: Device.hpp fully init devid
- constructor use available setters
2022-10-09 13:49:39 -04:00
Daniel Agar f3964513c7 sensors: fix accel/gyro/mag calibration offset units 2022-10-09 13:02:38 -04:00
Daniel Agar ee4821ed0a commander: relax COM_ARM_MAG_ANG default to minimize false positives
- this check is mainly intended for catching blatant setup problems like a magnetometer that's mounted 90 or 180 degrees off
2022-10-09 12:41:06 -04:00
fkaiser 30150f723a Tools/px_uploader.py: use monotonic clock if available (#20352)
Signed-off-by: fkaiser <fabian.kaiser@wingtra.com>
2022-10-06 09:49:05 -04:00
alexklimaj 064f3f86bc Increase mag calibration max_var_allowed 2022-10-06 08:44:36 -04:00
Hamish Willee 022aa13aa1 mpu9250_i2c - also needs docs update 2022-10-05 20:26:25 -04:00
Hamish Willee 6d612b1ba4 MPU9250 driver doc incorrect 2022-10-05 20:26:25 -04:00
Daniel Agar 8cc39096cb load_mon: NuttX cpuload use system times for calculation
- this is to minimize the impact of any load_mon scheduling jitter in the sampled load percentage
2022-10-05 14:21:38 -04:00
benjinne 29b031c862 Tools/setup/ubuntu.sh update comment to include 22.04 2022-10-05 13:41:47 -04:00
Daniel Agar 5f0a539633 gps_blending: fix blending init to best instance
- output GPS publication defaults to best input instance
 - blended states are explicitly cleared and then populated with
weighted blend
2022-10-05 10:26:48 -04:00
Beat Küng f79dad1e63 fix ROMFS: run camera trigger, capture and PPS before pwm_out
As they might need to reserve the pwm pins.
2022-10-05 09:13:35 -04:00
Matthias Grob 46e6e83e14 Commander: allow disarmin not-landed boat like rover
This is a hotfix and a boat should never even detect a takeoff
in normal operation.
2022-10-05 09:07:18 -04:00
Beat Küng dafead6f20 logger: add compressed events metadata file if it exists in the ROMFS
Allows to decode events not (yet) on main.
The file is currently ~15KB.
2022-10-05 07:44:55 +02:00
Beat Küng 02035d94aa metadata: sort json output
ensures the files don't change arbitrarily
2022-10-05 07:44:55 +02:00
modaltb 06a0aedbdb modalai_esc: directly using deadband param value instead of converting it to RPM 2022-10-04 20:14:59 -04:00
Thomas Debrunner 0af87ec745 mavlink: initial OPEN_DRONE_ID_BASIC_ID/OPEN_DRONE_ID_LOCATION support 2022-10-04 14:40:59 -04:00
Matthias Grob b179427b4c Remove opinionated non-default MPC_TKO_SPEED from airframes 2022-10-04 11:36:57 -04:00
pandafeng1999 e4b4df4e5d drivers/distance_sensor/gy_us42: add the specified i2c address 2022-10-04 11:35:45 -04:00
Matthias Grob f96507bb22 vtol_takeoff: fix comment typo 2022-10-04 10:01:04 -04:00
Peter van der Perk c807d6079d FMUK66-V3 Enable DMA on SPI 2022-10-04 09:46:04 -04:00
Peter van der Perk 0cf2ecedb9 FMUK66 Disable Telnet to save RAM 2022-10-04 09:46:04 -04:00
Julian Oes 5c77bbcb4c ms5611: ignore reading 0
This prevents publishing a negative pressure which leads to a NAN
altitude estimate further down the line.
2022-10-04 09:37:53 -04:00
Beat Küng 04b1cbb423 vtol_att_control: standard: also do blending for FW controls
So that the sum of the control is always 1.
2022-10-04 09:54:11 +02:00
Silvan Fuhrer 6db92b4011 ControlAllocation: remove actuator trim value from actuator_sp to calculate allocated control
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-10-04 07:51:25 +02:00
Zachary Lowell 4520186878 qurt: replacing qurt threads with pthread 2022-10-03 18:01:04 -04:00
bresch 4b687beb3b ekf2: remove old airspeed fusion code 2022-10-03 10:59:42 -04:00
bresch 299e6058e3 ekf2_test: test airspeed symforce vs sympy generated code 2022-10-03 10:59:42 -04:00
bresch 29ebef1f74 ekf2: migrate fuse_airspeed to SymForce 2022-10-03 10:59:42 -04:00
Daniel Agar 41cda14126 ekf2: add symforce code generation helper target 2022-10-03 10:59:42 -04:00
Daniel Agar c9441bb48a boards: px4_fmu-v2/v3 allow optional mpu9250 probe to fail without error 2022-10-02 21:40:18 -04:00
Benjamin Perseghetti aa2b47845a new Gazebo simulation handle older gz versions (#20342) 2022-10-02 21:30:30 -04:00
PX4 BuildBot f4d2e176ae Update submodule sitl_gazebo to latest Sun Oct 2 12:38:54 UTC 2022
- sitl_gazebo in PX4/Firmware (2bd1ac005f): https://github.com/PX4/PX4-SITL_gazebo/commit/b968405a617005ba0a793a8b4703913d4c6eff5f
    - sitl_gazebo current upstream: https://github.com/PX4/PX4-SITL_gazebo/commit/e80432759540c91f85a012f47aa6ebb0ee9de7e4
    - Changes: https://github.com/PX4/PX4-SITL_gazebo/compare/b968405a617005ba0a793a8b4703913d4c6eff5f...e80432759540c91f85a012f47aa6ebb0ee9de7e4

    e804327 2022-10-01 Thomas Stauber - set lidar measurements to 0.0 if out of range (#914)
7ed1da6 2022-09-27 Karthik S - Advanced Lift-Drag Plugin (#901)
669d7f5 2022-09-08 Oleg Kalachev - Fix local addr assignment for qgc and sdk sockets
2022-10-02 10:54:31 -04:00
PX4 BuildBot f7a5c91fb3 Update submodule libcanard to latest Sun Oct 2 12:38:56 UTC 2022
- libcanard in PX4/Firmware (8e144eece9e9cd5a23dbeb6723591f214cad631a): https://github.com/opencyphal/libcanard/commit/db87ea32aa092c48ea103963138b6346dd3e9008
    - libcanard current upstream: https://github.com/opencyphal/libcanard/commit/2e3b11f6b8325080c160d38521b169b0bbb6b1c7
    - Changes: https://github.com/opencyphal/libcanard/compare/db87ea32aa092c48ea103963138b6346dd3e9008...2e3b11f6b8325080c160d38521b169b0bbb6b1c7

    2e3b11f 2022-07-15 Pavel Kirienko - Follow-up for #197 -- fix minor issues discovered by Sonar (#198)
106ceaf 2022-07-11 Dmitry Ponomarev - Fix cast-align warnings on ARM
8953fe6 2022-07-06 Dmitry Ponomarev - Add ARM build to github workflow
2022-10-02 10:54:05 -04:00
PX4 BuildBot 644a836d0a Update submodule libevents to latest Sun Oct 2 12:39:02 UTC 2022
- libevents in PX4/Firmware (ddc1e6d6c5c2707be5522d4c4d7434403202cf45): https://github.com/mavlink/libevents/commit/82dabdb914d7bd640c281900e2852d0afc074b68
    - libevents current upstream: https://github.com/mavlink/libevents/commit/a89808bffd1efb0543e66f17a7fa12dfce5e6bf0
    - Changes: https://github.com/mavlink/libevents/compare/82dabdb914d7bd640c281900e2852d0afc074b68...a89808bffd1efb0543e66f17a7fa12dfce5e6bf0

    a89808b 2022-09-26 Beat Küng - combine.py: sort json keys
2022-10-02 10:53:28 -04:00
PX4 BuildBot cf0cd4ebf2 Update submodule mavlink to latest Sun Oct 2 12:39:04 UTC 2022
- mavlink in PX4/Firmware (65bd1fd4c000a7fa0de2a0e8dce1ba9b2a62fa86): https://github.com/mavlink/mavlink/commit/c46af523263ff0dad59afe018fe387c1df030442
    - mavlink current upstream: https://github.com/mavlink/mavlink/commit/dda5a18ddb002a871ba301bb584893ee6378e2f3
    - Changes: https://github.com/mavlink/mavlink/compare/c46af523263ff0dad59afe018fe387c1df030442...dda5a18ddb002a871ba301bb584893ee6378e2f3

    dda5a18d 2022-09-28 WickedShell - Support a return to default speed for DO_CHANGE_SPEED (#1890)
4e04dbbf 2022-09-24 Hamish Willee - MAV_FRAME_BODY_FRD - match to implementations and sanity (#1894)
89a61214 2022-09-23 Hamish Willee - DO_CHANGE_SPEED - clarify lifetime of speed setting (#1892)
11414f88 2022-09-21 Søren Friis - Clarify swarm fields (#1891)
5cdf8b60 2022-09-08 Hamish Willee - HOME_POSITION - clarify local frame means NED (#1886)
551e3b49 2022-09-07 Julian Oes - Fix CI (#1888)
d99ee9b6 2022-09-07 Julian Oes - pymavlink: update submodule to latest master (#1887)
92d2a58d 2022-09-01 Hamish Willee - common.xml:TIMESYNC docs and extensions (#1878)
c424dc65 2022-09-01 Julian Oes - minimal: try to make component ID less confusing (#1876)
153939bd 2022-09-01 Hamish Willee - Fix typo MAV_CMD_DO_SET_MISSION_CURRENT
5043a1e0 2022-09-01 Hamish Willee - MAV_CMD_DO_SET_MISSION_CURRENT - allow mission resetting (#1870)
90aa7bfc 2022-08-31 Chikirev Sirguy - Update common.xml (#1815)
554ccadd 2022-08-31 Hamish Willee - common: OpenDroneID messages no longer WIP (#1882)
06448cf6 2022-08-24 Hamish Willee - MAV_ODID_ARM_STATUS entries update to naming convention (#1883)
ff649224 2022-08-18 Patrick José Pereira - Fix gibberish descriptions ualberta.xml (#1881)
11f4b236 2022-08-18 Hamish Willee - Mission item - document values for autocontinue (#1868)
fb8ac31b 2022-08-18 Julian Oes - development: remove MISSION_CHANGED (#1879)
76b794c2 2022-08-18 Julian Oes - common: extend MISSION_CURRENT (#1869)
1ae3edc4 2022-08-15 Andrew Tridgell - common: added OPEN_DRONE_ID_SYSTEM_UPDATE message (#1880)
aa25f4df 2022-08-11 Andrew Tridgell - common: added OPEN_DRONE_ID_ARM_STATUS (#1873)
2022-10-02 10:53:00 -04:00
Daniel Agar 2bd1ac005f .gitmodules update branches master -> main 2022-10-01 12:22:22 -04:00
290 changed files with 14258 additions and 10270 deletions
+1 -1
View File
@@ -937,7 +937,7 @@ void printTopics() {
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener vehicle_odometry" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener vehicle_rates_setpoint" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener vehicle_status" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener vehicle_status_flags" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener failsafe_flags" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener vtol_vehicle_status" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener yaw_estimator_status" || true'
}
-1
View File
@@ -23,7 +23,6 @@ jobs:
"shellcheck_all",
"NO_NINJA_BUILD=1 px4_fmu-v5_default",
"NO_NINJA_BUILD=1 px4_sitl_default",
"NO_NINJA_BUILD=1 px4_sitl_gps_base",
"BUILD_MICRORTPS_AGENT=1 px4_sitl_rtps",
"airframe_metadata",
"module_documentation",
+44
View File
@@ -0,0 +1,44 @@
name: Failsafe Simulator Build
on:
push:
branches:
- 'main'
pull_request:
branches:
- '*'
jobs:
build:
runs-on: ubuntu-latest
defaults:
run:
shell: bash
strategy:
fail-fast: false
matrix:
check: [
"failsafe_web",
]
container:
image: px4io/px4-dev-nuttx-focal:2021-09-08
options: --privileged --ulimit core=-1 --security-opt seccomp=unconfined
steps:
- uses: actions/checkout@v1
with:
token: ${{ secrets.ACCESS_TOKEN }}
- name: check environment
run: |
export
ulimit -a
- name: install emscripten
run: |
git clone https://github.com/emscripten-core/emsdk.git _emscripten_sdk
cd _emscripten_sdk
./emsdk install latest
./emsdk activate latest
- name: ${{matrix.check}}
run: |
. ./_emscripten_sdk/emsdk_env.sh
make ${{matrix.check}}
+4 -3
View File
@@ -9,15 +9,15 @@
[submodule "Tools/simulation/jmavsim/jMAVSim"]
path = Tools/simulation/jmavsim/jMAVSim
url = https://github.com/PX4/jMAVSim.git
branch = master
branch = main
[submodule "Tools/simulation/gazebo/sitl_gazebo"]
path = Tools/simulation/gazebo/sitl_gazebo
url = https://github.com/PX4/PX4-SITL_gazebo.git
branch = master
branch = main
[submodule "src/drivers/gps/devices"]
path = src/drivers/gps/devices
url = https://github.com/PX4/PX4-GPSDrivers.git
branch = master
branch = main
[submodule "src/modules/micrortps_bridge/micro-CDR"]
path = src/modules/micrortps_bridge/micro-CDR
url = https://github.com/PX4/Micro-CDR.git
@@ -53,6 +53,7 @@
[submodule "src/lib/events/libevents"]
path = src/lib/events/libevents
url = https://github.com/mavlink/libevents.git
branch = main
[submodule "src/lib/crypto/libtomcrypt"]
path = src/lib/crypto/libtomcrypt
url = https://github.com/PX4/libtomcrypt.git
-5
View File
@@ -6,11 +6,6 @@ CONFIG:
buildType: RelWithDebInfo
settings:
CONFIG: px4_sitl_default
px4_sitl_gps_base:
short: px4_sitl_gps_base
buildType: RelWithDebInfo
settings:
CONFIG: px4_sitl_gps_base
px4_sitl_rtps:
short: px4_sitl_rtps
buildType: RelWithDebInfo
Vendored
+31
View File
@@ -162,6 +162,35 @@ pipeline {
}
}
stage('failsafe docs') {
agent {
docker { image 'px4io/px4-dev-base-focal:2021-08-18' }
}
steps {
sh '''#!/bin/bash -l
echo $0;
git clone https://github.com/emscripten-core/emsdk.git _emscripten_sdk;
cd _emscripten_sdk;
./emsdk install latest;
./emsdk activate latest;
. ./_emscripten_sdk/emsdk_env.sh;
make failsafe_web;
cd build/px4_sitl_default_failsafe_web;
mkdir -p failsafe_sim;
cp index.* parameters.json failsafe_sim;
'''
dir('build/px4_sitl_default_failsafe_web') {
archiveArtifacts(artifacts: 'failsafe_sim/*')
stash includes: 'failsafe_sim/*', name: 'failsafe_sim'
}
}
post {
always {
sh 'make distclean; git clean -ff -x -d .'
}
}
}
stage('uORB graphs') {
agent {
docker {
@@ -203,6 +232,7 @@ pipeline {
unstash 'metadata_parameters'
unstash 'metadata_module_documentation'
unstash 'msg_documentation'
unstash 'failsafe_sim'
unstash 'uorb_graph'
withCredentials([usernamePassword(credentialsId: 'px4buildbot_github_personal_token', passwordVariable: 'GIT_PASS', usernameVariable: 'GIT_USER')]) {
sh('git clone https://${GIT_USER}:${GIT_PASS}@github.com/PX4/PX4-user_guide.git')
@@ -211,6 +241,7 @@ pipeline {
sh('cp -R modules/*.md PX4-user_guide/en/modules/')
sh('cp -R graph_*.json PX4-user_guide/.vuepress/public/en/middleware/')
sh('cp -R msg_docs/*.md PX4-user_guide/en/msg_docs/')
sh('cp -R failsafe_sim/* PX4-user_guide/.vuepress/public/en/config/failsafe')
sh('cd PX4-user_guide; git status; git add .; git commit -a -m "Update PX4 Firmware metadata `date`" || true')
sh('cd PX4-user_guide; git push origin main || true')
sh('rm -rf PX4-user_guide')
+10
View File
@@ -575,3 +575,13 @@ update_px4_ros_com:
update_px4_msgs:
@Tools/update_px4_ros2_bridge.sh --ws_dir ${ROS2_WS_DIR} --px4_msgs
.PHONY: failsafe_web run_failsafe_web_server
failsafe_web:
@if ! command -v emcc; then echo -e "Install emscripten first: https://emscripten.org/docs/getting_started/downloads.html\nAnd source the env: source <path>/emsdk_env.sh"; exit 1; fi
@$(MAKE) --no-print-directory px4_sitl_default failsafe_test parameters_xml \
PX4_CMAKE_BUILD_TYPE=Release BUILD_DIR_SUFFIX=_failsafe_web \
CMAKE_ARGS="-DCMAKE_CXX_COMPILER=em++ -DCMAKE_C_COMPILER=emcc"
run_failsafe_web_server: failsafe_web
@cd build/px4_sitl_default_failsafe_web && \
python3 -m http.server
+1 -1
View File
@@ -4,7 +4,7 @@
[![Nuttx Targets](https://github.com/PX4/PX4-Autopilot/workflows/Nuttx%20Targets/badge.svg)](https://github.com/PX4/PX4-Autopilot/actions?query=workflow%3A%22Nuttx+Targets%22?branch=master) [![SITL Tests](https://github.com/PX4/PX4-Autopilot/workflows/SITL%20Tests/badge.svg?branch=master)](https://github.com/PX4/PX4-Autopilot/actions?query=workflow%3A%22SITL+Tests%22)
[![Slack](/.github/slack.svg)](https://join.slack.com/t/px4/shared_invite/zt-si4xo5qs-R4baYFmMjlrT4rQK5yUnaA)
[![Discord Shield](https://discordapp.com/api/guilds/1022170275984457759/widget.png?style=shield)](https://discord.gg/dronecode)
This repository holds the [PX4](http://px4.io) flight control solution for drones, with the main applications located in the [src/modules](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules) directory. It also contains the PX4 Drone Middleware Platform, which provides drivers and middleware to run drones.
@@ -41,6 +41,20 @@ elif [ "$PX4_SIMULATOR" = "gz" ]; then
fi
gz_world=$( ign topic -l | grep -m 1 -e "/world/.*/clock" | sed 's/\/world\///g; s/\/clock//g' )
gz_version_major=$( ign gazebo --versions | sed 's/\..*//g' )
gz_version_minor=$( ign gazebo --versions | sed 's/'"${gz_version_major}"\.'//; s/\..*//g' )
gz_version_point=$( ign gazebo --versions | sed 's/'"${gz_version_major}"\.'//; s/'"${gz_version_minor}"\.'//')
if [ "$gz_version_major" -gt "6" ] || { [ "$gz_version_major" -eq "6" ] && [ "$gz_version_minor" -gt "12" ]; } || { [ "$gz_version_major" -eq "6" ] && [ "$gz_version_minor" -eq "12" ] && [ "$gz_version_point" -gt "0" ]; }; then
echo "INFO [init] using latest version of MultiCopterMotor plugin."
else
echo "WARN [init] using older version of MultiCopterMotor plugin, please update to latest gazebo > 6.12.0."
if [ "$PX4_SIM_MODEL" = "x500" ]; then
PX4_SIM_MODEL="x500-Legacy"
echo "WARN [init] setting PX4_SIM_MODEL -> $PX4_SIM_MODEL from x500 till gazebo > 6.12.0"
fi
fi
if [ -z $gz_world ]; then
@@ -38,7 +38,6 @@ param set-default MIS_YAW_TMT 10
param set-default MPC_ACC_HOR_MAX 2
param set-default MPC_ACC_HOR_MAX 2
param set-default MPC_THR_MIN 0.1
param set-default MPC_TKO_SPEED 1
param set-default MPC_XY_P 0.8
param set-default MPC_XY_VEL_D_ACC 0.1
param set-default MPC_XY_VEL_I_ACC 4
@@ -65,7 +65,6 @@ param set-default COM_SPOOLUP_TIME 1.5
param set-default MPC_THR_HOVER 0.45
param set-default MPC_TILTMAX_AIR 25
param set-default MPC_TKO_RAMP_T 1.8
param set-default MPC_TKO_SPEED 1
param set-default MPC_VEL_MANUAL 3
param set-default MPC_XY_CRUISE 3
param set-default MPC_XY_VEL_MAX 3.5
@@ -63,7 +63,6 @@ param set-default MPC_ACC_UP_MAX 4
param set-default MPC_MAN_Y_MAX 120
param set-default MPC_TILTMAX_AIR 45
param set-default MPC_THR_HOVER 0.3
param set-default MPC_TKO_SPEED 1
param set-default MPC_VEL_MANUAL 5
param set-default MPC_XY_CRUISE 5
param set-default MPC_XY_VEL_MAX 5
@@ -64,7 +64,6 @@ param set-default MPC_MANTHR_MIN 0
param set-default MPC_MAN_Y_MAX 120
param set-default MPC_TILTMAX_AIR 45
param set-default MPC_THR_HOVER 0.3
param set-default MPC_TKO_SPEED 1
param set-default MPC_VEL_MANUAL 5
param set-default MPC_XY_CRUISE 5
param set-default MPC_XY_VEL_MAX 5
@@ -53,7 +53,6 @@ param set-default MPC_XY_VEL_P_ACC 2.6
param set-default MPC_XY_VEL_I_ACC 1.2
param set-default MPC_XY_VEL_D_ACC 0.2
param set-default MPC_TKO_RAMP_T 1
param set-default MPC_TKO_SPEED 1.1
param set-default MPC_VEL_MANUAL 3
param set-default BAT1_SOURCE 0
@@ -62,7 +62,6 @@ param set-default MPC_XY_VEL_P_ACC 2.6
param set-default MPC_XY_VEL_I_ACC 1.2
param set-default MPC_XY_VEL_D_ACC 0.2
param set-default MPC_TKO_RAMP_T 1
param set-default MPC_TKO_SPEED 1.1
param set-default MPC_VEL_MANUAL 3
param set-default BAT1_SOURCE 0
@@ -0,0 +1,75 @@
#!/bin/sh
#
# @name Aion Robotics R1 UGV
#
# @url https://www.aionrobotics.com/r1
#
# @type Rover
# @class Rover
#
# @board px4_fmu-v2 exclude
# @board bitcraze_crazyflie exclude
#
. ${R}etc/init.d/rc.rover_defaults
param set-default BAT1_N_CELLS 4
param set-default EKF2_GBIAS_INIT 0.01
param set-default EKF2_ANGERR_INIT 0.01
param set-default EKF2_MAG_TYPE 1
param set-default FW_AIRSPD_MIN 0
param set-default FW_AIRSPD_TRIM 1
param set-default FW_AIRSPD_MAX 3
param set-default GND_SP_CTRL_MODE 1
param set-default GND_L1_DIST 5
param set-default GND_L1_PERIOD 3
param set-default GND_THR_CRUISE 0.7
param set-default GND_THR_MAX 0.5
# Because this is differential drive, it can make a turn with radius 0.
# This corresponds to a turn angle of pi radians.
# If a special case is made for differential-drive, this will need to change.
param set-default GND_MAX_ANG 3.142
param set-default GND_WHEEL_BASE 0.3
# TODO: Set to -1.0, to allow reversing. This will require many changes in the codebase
# to support negative throttle.
param set-default GND_THR_MIN 0
param set-default GND_SPEED_P 0.25
param set-default GND_SPEED_I 3
param set-default GND_SPEED_D 0.001
param set-default GND_SPEED_IMAX 0.125
param set-default GND_SPEED_THR_SC 1
param set-default MIS_LTRMIN_ALT 0.01
param set-default MIS_TAKEOFF_ALT 0.01
param set-default NAV_ACC_RAD 0.5
# Enable Airspeed check circuit breaker because Rovers will have no airspeed sensor
param set-default CBRK_AIRSPD_CHK 162128
# Differential drive acts like ackermann steering with a maximum turn angle of 180 degrees, or pi radians
param set-default GND_MAX_ANG 3.1415
param set-default RBCLW_BAUD 8
param set-default RBCLW_COUNTS_REV 1200
param set-default RBCLW_ADDRESS 128
# 104 corresponds to Telem 4
param set-default RBCLW_SER_CFG 104
# Start this driver after setting parameters, because the driver uses some of those parameters.
# roboclaw start /dev/ttyS3
# Set geometry & output configration
param set-default CA_AIRFRAME 6
param set-default CA_R_REV 3
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
param set-default PWM_MAIN_DIS1 1500
param set-default PWM_MAIN_DIS2 1500
param set-default PWM_MAIN_TIM0 50
param set-default PWM_MAIN_TIM1 50
@@ -118,6 +118,7 @@ px4_add_romfs_files(
50000_generic_ground_vehicle
50004_nxpcup_car_dfrobot_gpx
50003_aion_robotics_r1_rover
# [60000, 61000] (Unmanned) Underwater Robots
60000_uuv_generic
+21 -21
View File
@@ -324,6 +324,27 @@ else
rc_update start
manual_control start
# Start camera trigger, capture and PPS before pwm_out as they might access
# pwm pins
if param greater -s TRIG_MODE 0
then
camera_trigger start
camera_feedback start
fi
# PPS capture driver
if param greater -s PPS_CAP_ENABLE 0
then
pps_capture start
fi
# Camera capture driver
if param greater -s CAM_CAP_FBACK 0
then
if camera_capture start
then
camera_capture on
fi
fi
#
# Sensors System (start before Commander so Preflight checks are properly run).
# Commander needs to be this early for in-air-restarts.
@@ -390,12 +411,6 @@ else
mag_bias_estimator start
fi
if param greater -s TRIG_MODE 0
then
camera_trigger start
camera_feedback start
fi
#
# Optional board mavlink streams: rc.board_mavlink
#
@@ -416,21 +431,6 @@ else
# Must be started after the serial config is read
rc_input start $RC_INPUT_ARGS
# PPS capture driver (before pwm_out)
if param greater -s PPS_CAP_ENABLE 0
then
pps_capture start
fi
# Camera capture driver (before pwm_out)
if param greater -s CAM_CAP_FBACK 0
then
if camera_capture start
then
camera_capture on
fi
fi
#
# Play the startup tune (if not disabled or there is an error)
#
@@ -489,7 +489,7 @@ actuators = {
with open(output_file, 'w') as outfile:
indent = 2 if verbose else None
json.dump(actuators, outfile, indent=indent)
json.dump(actuators, outfile, indent=indent, sort_keys=True)
if compress:
save_compressed(output_file)
@@ -32,16 +32,16 @@ def extract_timer(line):
# Try format: initIOTimer(Timer::Timer5, DMA{DMA::Index1, DMA::Stream0, DMA::Channel6}),
search = re.search('Timer::([0-9a-zA-Z_]+)[,\)]', line, re.IGNORECASE)
if search:
return search.group(1)
return search.group(1), 'generic'
# nxp rt1062 format: initIOPWM(PWM::FlexPWM2),
search = re.search('PWM::Flex([0-9a-zA-Z_]+)[,\)]', line, re.IGNORECASE)
if search:
return search.group(1)
return search.group(1), 'imxrt'
return None
return None, 'unknown'
def extract_timer_from_channel(line):
def extract_timer_from_channel(line, num_channels_already_found):
# Try format: initIOTimerChannel(io_timers, {Timer::Timer5, Timer::Channel1}, {GPIO::PortA, GPIO::Pin0}),
search = re.search('Timer::([0-9a-zA-Z_]+), ', line, re.IGNORECASE)
if search:
@@ -50,7 +50,8 @@ def extract_timer_from_channel(line):
# nxp rt1062 format: initIOTimerChannel(io_timers, {PWM::PWM2_PWM_A, PWM::Submodule0}, IOMUX::Pad::GPIO_B0_06),
search = re.search('PWM::(PWM[0-9]+)[_,\)]', line, re.IGNORECASE)
if search:
return search.group(1)
# imxrt uses a 1:1 timer group to channel association
return str(num_channels_already_found)
return None
@@ -72,7 +73,14 @@ def get_timer_groups(timer_config_file, verbose=False):
line = line.strip()
if len(line) == 0 or line.startswith('//'):
continue
timer = extract_timer(line)
timer, timer_type = extract_timer(line)
if timer_type == 'imxrt':
if verbose: print('imxrt timer found')
max_num_channels = 16 # Just add a fixed number of timers
timers = [str(i) for i in range(max_num_channels)]
dshot_support = {str(i): False for i in range(max_num_channels)}
break
if timer:
if verbose: print('found timer def: {:}'.format(timer))
@@ -101,7 +109,7 @@ def get_timer_groups(timer_config_file, verbose=False):
continue
if verbose: print('--'+line+'--')
timer = extract_timer_from_channel(line)
timer = extract_timer_from_channel(line, len(channel_timers))
if timer:
if verbose: print('Found timer: {:} in channel line {:}'.format(timer, line))
+7 -3
View File
@@ -211,6 +211,11 @@ class SourceParser(object):
ignore_event = False
def parse_message(s):
assert s[0] == '"', "Argument must be a string literal: {:}".format(s)
# unescape \x, to treat the string the same as the C++ compiler
return s[1:-1].encode("utf-8").decode('unicode_escape')
# extract function arguments
args_split = self._parse_arguments(args)
if call == "events::send" or call == "send":
@@ -228,8 +233,7 @@ class SourceParser(object):
else:
raise Exception("Could not extract event ID from {:}".format(args_split[0]))
event.name = event_name
# unescape \x, to treat the string the same as the C++ compiler
event.message = args_split[2][1:-1].encode("utf-8").decode('unicode_escape')
event.message = parse_message(args_split[2])
elif call in ['reporter.healthFailure', 'reporter.armingCheckFailure']:
assert len(args_split) == num_args + 5, \
"Unexpected Number of arguments for: {:}, {:}".format(args_split, num_args)
@@ -239,7 +243,7 @@ class SourceParser(object):
else:
raise Exception("Could not extract event ID from {:}".format(args_split[2]))
event.name = event_name
event.message = args_split[4][1:-1]
event.message = parse_message(args_split[4])
if 'health' in call:
event.group = "health"
else:
+20 -8
View File
@@ -77,11 +77,23 @@ except ImportError as e:
print("")
sys.exit(1)
# Define time to use time.time() by default
def _time():
return time.time()
# Detect python version
if sys.version_info[0] < 3:
runningPython3 = False
else:
runningPython3 = True
if sys.version_info[1] >=3:
# redefine to use monotonic time when available
def _time():
try:
return time.monotonic()
except Exception:
return time.time()
class FirmwareNotSuitableException(Exception):
def __init__(self, message):
@@ -230,7 +242,7 @@ class uploader(object):
def open(self):
# upload timeout
timeout = time.time() + 0.2
timeout = _time() + 0.2
# attempt to open the port while it exists and until timeout occurs
while self.port is not None:
@@ -240,7 +252,7 @@ class uploader(object):
except AttributeError:
portopen = self.port.isOpen()
if not portopen and time.time() < timeout:
if not portopen and _time() < timeout:
try:
self.port.open()
except OSError:
@@ -415,16 +427,16 @@ class uploader(object):
uploader.EOC)
# erase is very slow, give it 30s
deadline = time.time() + 30.0
while time.time() < deadline:
deadline = _time() + 30.0
while _time() < deadline:
usualEraseDuration = 15.0
estimatedTimeRemaining = deadline-time.time()
estimatedTimeRemaining = deadline-_time()
if estimatedTimeRemaining >= usualEraseDuration:
self.__drawProgressBar(label, 30.0-estimatedTimeRemaining, usualEraseDuration)
else:
self.__drawProgressBar(label, 10.0, 10.0)
sys.stdout.write(" (timeout: %d seconds) " % int(deadline-time.time()))
sys.stdout.write(" (timeout: %d seconds) " % int(deadline-_time()))
sys.stdout.flush()
if self.__trySync():
@@ -572,7 +584,7 @@ class uploader(object):
# upload the firmware
def upload(self, fw, force=False, boot_delay=None):
# Make sure we are doing the right thing
start = time.time()
start = _time()
if self.board_type != fw.property('board_id'):
msg = "Firmware not suitable for this board (Firmware board_type=%u board_id=%u)" % (
self.board_type, fw.property('board_id'))
@@ -668,7 +680,7 @@ class uploader(object):
print("\nRebooting.", end='')
self.__reboot()
self.port.close()
print(" Elapsed Time %3.3f\n" % (time.time() - start))
print(" Elapsed Time %3.3f\n" % (_time() - start))
def __next_baud_flightstack(self):
if self.baudrate_flightstack_idx + 1 >= len(self.baudrate_flightstack):
+1 -1
View File
@@ -2,7 +2,7 @@
set -e
## Bash script to setup PX4 development environment on Ubuntu LTS (20.04, 18.04, 16.04).
## Bash script to setup PX4 development environment on Ubuntu LTS (22.04, 20.04, 18.04).
## Can also be used in docker.
##
## Installs:
@@ -0,0 +1,11 @@
<?xml version="1.0"?>
<model>
<name>x500-Legacy</name>
<version>1.0</version>
<sdf version="1.9">model.sdf</sdf>
<author>
<name>Benjamin Perseghetti</name>
<email>bperseghetti@rudislabs.com</email>
</author>
<description>Model of the NXP HoverGames Drone development kit (KIT-HGDRONEK66). The PX4 software compatible kit provides mechanical, RC remote and other components needed to evaluate the RDDRONE-FMUK66 reference design. The FMU includes 100Base-T1 Automotive Ethernet, dual CAN transceivers, as well as SE050 secure element, and works with add on boards NavQPlus, MR-T1ETH8, MR-T1ADAPT, and CAN-nodes such as UCANS32K1SIC. Kit may be used with, and contains the components needed for the HoverGames.com coding challenges.</description>
</model>
@@ -0,0 +1,76 @@
<?xml version="1.0" encoding="UTF-8"?>
<sdf version='1.9'>
<model name='x500-Legacy'>
<include merge='true'>
<uri>model://x500-NoPlugin</uri>
</include>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<robotNamespace>/x500-Legacy_0</robotNamespace>
<jointName>rotor_0_joint</jointName>
<linkName>rotor_0</linkName>
<turningDirection>ccw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>0</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<robotNamespace>/x500-Legacy_0</robotNamespace>
<jointName>rotor_1_joint</jointName>
<linkName>rotor_1</linkName>
<turningDirection>ccw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>1</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<robotNamespace>/x500-Legacy_0</robotNamespace>
<jointName>rotor_2_joint</jointName>
<linkName>rotor_2</linkName>
<turningDirection>cw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>2</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<robotNamespace>/x500-Legacy_0</robotNamespace>
<jointName>rotor_3_joint</jointName>
<linkName>rotor_3</linkName>
<turningDirection>cw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>3</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
</model>
</sdf>
Binary file not shown.

After

Width:  |  Height:  |  Size: 32 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 51 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 28 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 27 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 23 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 1.5 MiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 25 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 26 KiB

Binary file not shown.
Binary file not shown.
File diff suppressed because one or more lines are too long
File diff suppressed because one or more lines are too long
Binary file not shown.

After

Width:  |  Height:  |  Size: 1.5 MiB

File diff suppressed because one or more lines are too long
@@ -0,0 +1,11 @@
<?xml version="1.0"?>
<model>
<name>x500-NoPlugin</name>
<version>1.0</version>
<sdf version="1.9">model.sdf</sdf>
<author>
<name>Benjamin Perseghetti</name>
<email>bperseghetti@rudislabs.com</email>
</author>
<description>Model of the NXP HoverGames Drone development kit (KIT-HGDRONEK66). The PX4 software compatible kit provides mechanical, RC remote and other components needed to evaluate the RDDRONE-FMUK66 reference design. The FMU includes 100Base-T1 Automotive Ethernet, dual CAN transceivers, as well as SE050 secure element, and works with add on boards NavQPlus, MR-T1ETH8, MR-T1ADAPT, and CAN-nodes such as UCANS32K1SIC. Kit may be used with, and contains the components needed for the HoverGames.com coding challenges.</description>
</model>
@@ -0,0 +1,516 @@
<?xml version="1.0" encoding="UTF-8"?>
<sdf version='1.9'>
<model name='x500-NoPlugin'>
<pose>0 0 .24 0 0 0</pose>
<self_collide>false</self_collide>
<static>false</static>
<link name="base_link">
<inertial>
<mass>2.0</mass>
<inertia>
<ixx>0.02166666666666667</ixx>
<ixy>0</ixy>
<ixz>0</ixz>
<iyy>0.02166666666666667</iyy>
<iyz>0</iyz>
<izz>0.04000000000000001</izz>
</inertia>
</inertial>
<gravity>true</gravity>
<velocity_decay/>
<visual name="base_link_visual">
<pose>0 0 .025 0 0 3.141592654</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/NXP-HGD-CF.dae</uri>
</mesh>
</geometry>
</visual>
<visual name="5010_motor_base_0">
<pose>0.174 0.174 .032 0 0 -.45</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Base.dae</uri>
</mesh>
</geometry>
</visual>
<visual name="5010_motor_base_1">
<pose>-0.174 0.174 .032 0 0 -.45</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Base.dae</uri>
</mesh>
</geometry>
</visual>
<visual name="5010_motor_base_2">
<pose>0.174 -0.174 .032 0 0 -.45</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Base.dae</uri>
</mesh>
</geometry>
</visual>
<visual name="5010_motor_base_3">
<pose>-0.174 -0.174 .032 0 0 -.45</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Base.dae</uri>
</mesh>
</geometry>
</visual>
<visual name="NXP_FMUK66_FRONT">
<pose>0.047 .001 .043 1 0 1.57</pose>
<cast_shadows>false</cast_shadows>
<geometry>
<plane>
<normal>0 0 1</normal>
<size>.013 .007</size>
</plane>
</geometry>
<material>
<diffuse>1.0 1.0 1.0</diffuse>
<specular>1.0 1.0 1.0</specular>
<pbr>
<metal>
<albedo_map>model://x500-NoPlugin/materials/textures/nxp.png</albedo_map>
</metal>
</pbr>
</material>
</visual>
<visual name="NXP_FMUK66_TOP">
<pose>-0.023 0 .0515 0 0 -1.57</pose>
<cast_shadows>false</cast_shadows>
<geometry>
<plane>
<normal>0 0 1</normal>
<size>.013 .007</size>
</plane>
</geometry>
<material>
<diffuse>1.0 1.0 1.0</diffuse>
<specular>1.0 1.0 1.0</specular>
<pbr>
<metal>
<albedo_map>model://x500-NoPlugin/materials/textures/nxp.png</albedo_map>
</metal>
</pbr>
</material>
</visual>
<visual name="RDDRONE_FMUK66_TOP">
<pose>-.03 0 .0515 0 0 -1.57</pose>
<cast_shadows>false</cast_shadows>
<geometry>
<plane>
<normal>0 0 1</normal>
<size>.032 .0034</size>
</plane>
</geometry>
<material>
<diffuse>1.0 1.0 1.0</diffuse>
<specular>1.0 1.0 1.0</specular>
<pbr>
<metal>
<albedo_map>model://x500-NoPlugin/materials/textures/rd.png</albedo_map>
</metal>
</pbr>
</material>
</visual>
<collision name="base_link_collision_0">
<pose>0 0 .007 0 0 0</pose>
<geometry>
<box>
<size>0.35355339059327373 0.35355339059327373 0.05</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
<collision name="base_link_collision_1">
<pose>0 -0.098 -.123 -0.35 0 0</pose>
<geometry>
<box>
<size>0.015 0.015 0.21</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
<collision name="base_link_collision_2">
<pose>0 0.098 -.123 0.35 0 0</pose>
<geometry>
<box>
<size>0.015 0.015 0.21</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
<collision name="base_link_collision_3">
<pose>0 -0.132 -.2195 0 0 0</pose>
<geometry>
<box>
<size>0.25 0.015 0.015</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
<collision name="base_link_collision_4">
<pose>0 0.132 -.2195 0 0 0</pose>
<geometry>
<box>
<size>0.25 0.015 0.015</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
<sensor name="imu_sensor" type="imu">
<always_on>1</always_on>
<update_rate>250</update_rate>
</sensor>
</link>
<link name="rotor_0">
<gravity>true</gravity>
<self_collide>false</self_collide>
<velocity_decay/>
<pose>0.174 -0.174 0.06 0 0 0</pose>
<inertial>
<mass>0.016076923076923075</mass>
<inertia>
<ixx>3.8464910483993325e-07</ixx>
<iyy>2.6115851691700804e-05</iyy>
<izz>2.649858234714004e-05</izz>
</inertia>
</inertial>
<visual name="rotor_0_visual">
<pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
<geometry>
<mesh>
<scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
<uri>model://x500-NoPlugin/meshes/1345_prop_ccw.stl</uri>
</mesh>
</geometry>
<material>
<script>
<name>Gazebo/DarkGrey</name>
<uri>file://media/materials/scripts/gazebo.material</uri>
</script>
</material>
</visual>
<visual name="rotor_0_visual_motor_bell">
<pose>0 0 -.032 0 0 0</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Bell.dae</uri>
</mesh>
</geometry>
</visual>
<collision name="rotor_0_collision">
<pose>0 0 0 0 0 0 </pose>
<geometry>
<box>
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
</link>
<joint name="rotor_0_joint" type="revolute">
<parent>base_link</parent>
<child>rotor_0</child>
<axis>
<xyz>0 0 1</xyz>
<limit>
<lower>-1e+16</lower>
<upper>1e+16</upper>
</limit>
<dynamics>
<spring_reference>0</spring_reference>
<spring_stiffness>0</spring_stiffness>
</dynamics>
<use_parent_model_frame>1</use_parent_model_frame>
</axis>
</joint>
<link name="rotor_1">
<gravity>true</gravity>
<self_collide>false</self_collide>
<velocity_decay/>
<pose>-0.174 0.174 0.06 0 0 0</pose>
<inertial>
<mass>0.016076923076923075</mass>
<inertia>
<ixx>3.8464910483993325e-07</ixx>
<iyy>2.6115851691700804e-05</iyy>
<izz>2.649858234714004e-05</izz>
</inertia>
</inertial>
<visual name="rotor_1_visual">
<pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
<geometry>
<mesh>
<scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
<uri>model://x500-NoPlugin/meshes/1345_prop_ccw.stl</uri>
</mesh>
</geometry>
<material>
<script>
<name>Gazebo/DarkGrey</name>
<uri>file://media/materials/scripts/gazebo.material</uri>
</script>
</material>
</visual>
<visual name="rotor_1_visual_motor_top">
<pose>0 0 -.032 0 0 0</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Bell.dae</uri>
</mesh>
</geometry>
</visual>
<collision name="rotor_1_collision">
<pose>0 0 0 0 0 0 </pose>
<geometry>
<box>
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
</link>
<joint name="rotor_1_joint" type="revolute">
<parent>base_link</parent>
<child>rotor_1</child>
<axis>
<xyz>0 0 1</xyz>
<limit>
<lower>-1e+16</lower>
<upper>1e+16</upper>
</limit>
<dynamics>
<spring_reference>0</spring_reference>
<spring_stiffness>0</spring_stiffness>
</dynamics>
<use_parent_model_frame>1</use_parent_model_frame>
</axis>
</joint>
<link name="rotor_2">
<gravity>true</gravity>
<self_collide>false</self_collide>
<velocity_decay/>
<pose>0.174 0.174 0.06 0 0 0</pose>
<inertial>
<mass>0.016076923076923075</mass>
<inertia>
<ixx>3.8464910483993325e-07</ixx>
<iyy>2.6115851691700804e-05</iyy>
<izz>2.649858234714004e-05</izz>
</inertia>
</inertial>
<visual name="rotor_2_visual">
<pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
<geometry>
<mesh>
<scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
<uri>model://x500-NoPlugin/meshes/1345_prop_cw.stl</uri>
</mesh>
</geometry>
<material>
<script>
<name>Gazebo/DarkGrey</name>
<uri>file://media/materials/scripts/gazebo.material</uri>
</script>
</material>
</visual>
<visual name="rotor_2_visual_motor_top">
<pose>0 0 -.032 0 0 0</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Bell.dae</uri>
</mesh>
</geometry>
</visual>
<collision name="rotor_2_collision">
<pose>0 0 0 0 0 0 </pose>
<geometry>
<box>
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
</link>
<joint name="rotor_2_joint" type="revolute">
<parent>base_link</parent>
<child>rotor_2</child>
<axis>
<xyz>0 0 1</xyz>
<limit>
<lower>-1e+16</lower>
<upper>1e+16</upper>
</limit>
<dynamics>
<spring_reference>0</spring_reference>
<spring_stiffness>0</spring_stiffness>
</dynamics>
<use_parent_model_frame>1</use_parent_model_frame>
</axis>
</joint>
<link name="rotor_3">
<gravity>true</gravity>
<self_collide>false</self_collide>
<velocity_decay/>
<pose>-0.174 -0.174 0.06 0 0 0</pose>
<inertial>
<mass>0.016076923076923075</mass>
<inertia>
<ixx>3.8464910483993325e-07</ixx>
<iyy>2.6115851691700804e-05</iyy>
<izz>2.649858234714004e-05</izz>
</inertia>
</inertial>
<visual name="rotor_3_visual">
<pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
<geometry>
<mesh>
<scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
<uri>model://x500-NoPlugin/meshes/1345_prop_cw.stl</uri>
</mesh>
</geometry>
<material>
<script>
<name>Gazebo/DarkGrey</name>
<uri>file://media/materials/scripts/gazebo.material</uri>
</script>
</material>
</visual>
<visual name="rotor_3_visual_motor_top">
<pose>0 0 -.032 0 0 0</pose>
<geometry>
<mesh>
<scale>1 1 1</scale>
<uri>model://x500-NoPlugin/meshes/5010Bell.dae</uri>
</mesh>
</geometry>
</visual>
<collision name="rotor_3_collision">
<pose>0 0 0 0 0 0 </pose>
<geometry>
<box>
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
</box>
</geometry>
<surface>
<contact>
<ode>
<min_depth>0.001</min_depth>
<max_vel>0</max_vel>
</ode>
</contact>
<friction>
<ode/>
</friction>
</surface>
</collision>
</link>
<joint name="rotor_3_joint" type="revolute">
<parent>base_link</parent>
<child>rotor_3</child>
<axis>
<xyz>0 0 1</xyz>
<limit>
<lower>-1e+16</lower>
<upper>1e+16</upper>
</limit>
<dynamics>
<spring_reference>0</spring_reference>
<spring_stiffness>0</spring_stiffness>
</dynamics>
<use_parent_model_frame>1</use_parent_model_frame>
</axis>
</joint>
</model>
</sdf>
Binary file not shown.

After

Width:  |  Height:  |  Size: 32 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 51 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 28 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 27 KiB

Binary file not shown.

After

Width:  |  Height:  |  Size: 23 KiB

+65 -1
View File
@@ -2,7 +2,71 @@
<sdf version='1.9'>
<model name='x500'>
<include merge='true'>
<uri>https://fuel.gazebosim.org/1.0/RudisLaboratories/models/x500-Base</uri>
<uri>model://x500-NoPlugin</uri>
</include>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<jointName>rotor_0_joint</jointName>
<linkName>rotor_0</linkName>
<turningDirection>ccw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>0</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<jointName>rotor_1_joint</jointName>
<linkName>rotor_1</linkName>
<turningDirection>ccw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>1</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<jointName>rotor_2_joint</jointName>
<linkName>rotor_2</linkName>
<turningDirection>cw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>2</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
<plugin filename="ignition-gazebo-multicopter-motor-model-system" name="ignition::gazebo::systems::MulticopterMotorModel">
<jointName>rotor_3_joint</jointName>
<linkName>rotor_3</linkName>
<turningDirection>cw</turningDirection>
<timeConstantUp>0.0125</timeConstantUp>
<timeConstantDown>0.025</timeConstantDown>
<maxRotVelocity>1000.0</maxRotVelocity>
<motorConstant>8.54858e-06</motorConstant>
<momentConstant>0.016</momentConstant>
<commandSubTopic>command/motor_speed</commandSubTopic>
<motorNumber>3</motorNumber>
<rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
<rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
<motorType>velocity</motorType>
</plugin>
</model>
</sdf>
@@ -127,7 +127,6 @@ CONFIG_MTD_RAMTRON=y
CONFIG_NETDEV_PHY_IOCTL=y
CONFIG_NETINIT_THREAD=y
CONFIG_NETINIT_THREAD_PRIORITY=49
CONFIG_NETUTILS_TELNETD=y
CONFIG_NET_ARP_IPIN=y
CONFIG_NET_ARP_SEND=y
CONFIG_NET_BROADCAST=y
@@ -157,7 +156,6 @@ CONFIG_NSH_DISABLE_UNAME=y
CONFIG_NSH_DISABLE_WGET=y
CONFIG_NSH_DISABLE_XD=y
CONFIG_NSH_FILEIOSIZE=512
CONFIG_NSH_IOBUFFER_SIZE=256
CONFIG_NSH_LINELEN=128
CONFIG_NSH_MAXARGUMENTS=15
CONFIG_NSH_NESTDEPTH=8
@@ -165,8 +163,6 @@ CONFIG_NSH_READLINE=y
CONFIG_NSH_ROMFSETC=y
CONFIG_NSH_ROMFSSECTSIZE=128
CONFIG_NSH_STRERROR=y
CONFIG_NSH_TELNETD_CLIENTSTACKSIZE=1280
CONFIG_NSH_TELNETD_DAEMONSTACKSIZE=1024
CONFIG_NSH_VARS=y
CONFIG_PIPES=y
CONFIG_PREALLOC_TIMERS=50
@@ -204,10 +200,6 @@ CONFIG_SYSTEM_CUTERM_DEFAULT_BAUD=57600
CONFIG_SYSTEM_NSH=y
CONFIG_SYSTEM_PING=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_TELNET_IOTHREAD_STACKSIZE=512
CONFIG_TELNET_MAXLCLIENTS=1
CONFIG_TELNET_RXBUFFER_SIZE=128
CONFIG_TELNET_TXBUFFER_SIZE=128
CONFIG_UART0_IFLOWCONTROL=y
CONFIG_UART0_OFLOWCONTROL=y
CONFIG_UART1_RXBUFSIZE=600
@@ -95,7 +95,9 @@ CONFIG_KINETIS_SDHC=y
CONFIG_KINETIS_SERIALBRK_BSDCOMPAT=y
CONFIG_KINETIS_SPI0=y
CONFIG_KINETIS_SPI1=y
CONFIG_KINETIS_SPI1_DMA=y
CONFIG_KINETIS_SPI2=y
CONFIG_KINETIS_SPI_DMA=y
CONFIG_KINETIS_UART0=y
CONFIG_KINETIS_UART0_RXDMA=y
CONFIG_KINETIS_UART1=y
@@ -125,7 +127,6 @@ CONFIG_MTD_RAMTRON=y
CONFIG_NETDEV_PHY_IOCTL=y
CONFIG_NETINIT_THREAD=y
CONFIG_NETINIT_THREAD_PRIORITY=49
CONFIG_NETUTILS_TELNETD=y
CONFIG_NET_ARP_IPIN=y
CONFIG_NET_ARP_SEND=y
CONFIG_NET_BROADCAST=y
@@ -155,7 +156,6 @@ CONFIG_NSH_DISABLE_UNAME=y
CONFIG_NSH_DISABLE_WGET=y
CONFIG_NSH_DISABLE_XD=y
CONFIG_NSH_FILEIOSIZE=512
CONFIG_NSH_IOBUFFER_SIZE=256
CONFIG_NSH_LINELEN=128
CONFIG_NSH_MAXARGUMENTS=15
CONFIG_NSH_NESTDEPTH=8
@@ -163,8 +163,6 @@ CONFIG_NSH_READLINE=y
CONFIG_NSH_ROMFSETC=y
CONFIG_NSH_ROMFSSECTSIZE=128
CONFIG_NSH_STRERROR=y
CONFIG_NSH_TELNETD_CLIENTSTACKSIZE=1280
CONFIG_NSH_TELNETD_DAEMONSTACKSIZE=1024
CONFIG_NSH_VARS=y
CONFIG_PIPES=y
CONFIG_PREALLOC_TIMERS=50
@@ -202,10 +200,6 @@ CONFIG_SYSTEM_CUTERM_DEFAULT_BAUD=57600
CONFIG_SYSTEM_NSH=y
CONFIG_SYSTEM_PING=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_TELNET_IOTHREAD_STACKSIZE=512
CONFIG_TELNET_MAXLCLIENTS=1
CONFIG_TELNET_RXBUFFER_SIZE=128
CONFIG_TELNET_TXBUFFER_SIZE=128
CONFIG_UART1_RXBUFSIZE=600
CONFIG_UART1_TXBUFSIZE=1100
CONFIG_UART4_BAUD=57600
@@ -236,6 +236,7 @@
*/
#define DIRECT_PWM_OUTPUT_CHANNELS 8
#define BOARD_NUM_IO_TIMERS 8
// Input Capture not supported on MVP
+8 -3
View File
@@ -76,9 +76,14 @@
#define rENBL REG(IMXRT_TMR_ENBL_OFFSET)
constexpr io_timers_t io_timers[MAX_IO_TIMERS] = {
initIOPWM(PWM::FlexPWM2),
initIOPWM(PWM::FlexPWM3),
initIOPWM(PWM::FlexPWM4),
initIOPWM(PWM::FlexPWM2, PWM::Submodule0),
initIOPWM(PWM::FlexPWM2, PWM::Submodule1),
initIOPWM(PWM::FlexPWM2, PWM::Submodule2),
initIOPWM(PWM::FlexPWM2, PWM::Submodule3),
initIOPWM(PWM::FlexPWM3, PWM::Submodule2),
initIOPWM(PWM::FlexPWM3, PWM::Submodule0),
initIOPWM(PWM::FlexPWM4, PWM::Submodule2),
initIOPWM(PWM::FlexPWM4, PWM::Submodule0),
};
constexpr timer_io_channels_t timer_io_channels[MAX_TIMER_IO_CHANNELS] = {
+1 -1
View File
@@ -100,7 +100,7 @@ else
# V3 build hwtypecmp supports V2|V2M|V30
if ! ver hwtypecmp V2M
then
mpu9250 -s -b 1 -R 14 start
mpu9250 -s -b 1 -R 14 -q start
# else: On the PixhawkMini the mpu9250 has been disabled due to HW errata
fi
+1 -1
View File
@@ -100,7 +100,7 @@ else
# V3 build hwtypecmp supports V2|V2M|V30
if ! ver hwtypecmp V2M
then
mpu9250 -s -b 1 -R 14 start
mpu9250 -s -b 1 -R 14 -q start
# else: On the PixhawkMini the mpu9250 has been disabled due to HW errata
fi
+1
View File
@@ -29,6 +29,7 @@ CONFIG_MODULES_LOGGER=y
CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
CONFIG_MODULES_MANUAL_CONTROL=y
CONFIG_MODULES_MAVLINK=y
CONFIG_MAVLINK_DIALECT="development"
CONFIG_MODULES_MC_ATT_CONTROL=y
CONFIG_MODULES_MC_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=y
-27
View File
@@ -1,27 +0,0 @@
CONFIG_PLATFORM_POSIX=y
CONFIG_BOARD_TESTING=y
CONFIG_BOARD_ETHERNET=y
CONFIG_DRIVERS_GPS=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_GPS_BASE_STATION=y
CONFIG_MODULES_LOAD_MON=y
CONFIG_MODULES_LOGGER=y
CONFIG_MODULES_MAVLINK=y
CONFIG_MODULES_REPLAY=y
CONFIG_COMMON_SIMULATION=y
CONFIG_SYSTEMCMDS_DYN=y
CONFIG_SYSTEMCMDS_FAILURE=y
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_SD_BENCH=y
CONFIG_SYSTEMCMDS_SHUTDOWN=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
CONFIG_EXAMPLES_HELLO=y
CONFIG_EXAMPLES_PX4_MAVLINK_DEBUG=y
CONFIG_EXAMPLES_PX4_SIMPLE_APP=y
CONFIG_EXAMPLES_WORK_ITEM=y
+1 -2
View File
@@ -59,7 +59,6 @@ set(msg_files
cellular_status.msg
collision_constraints.msg
collision_report.msg
commander_state.msg
control_allocator_status.msg
cpuload.msg
differential_pressure.msg
@@ -81,6 +80,7 @@ set(msg_files
estimator_status_flags.msg
event.msg
failure_detector_status.msg
failsafe_flags.msg
follow_target.msg
follow_target_estimator.msg
follow_target_status.msg
@@ -202,7 +202,6 @@ set(msg_files
vehicle_rates_setpoint.msg
vehicle_roi.msg
vehicle_status.msg
vehicle_status_flags.msg
vehicle_thrust_setpoint.msg
vehicle_torque_setpoint.msg
vehicle_trajectory_bezier.msg
+1 -1
View File
@@ -16,4 +16,4 @@ uint8 SOURCE_RC_SWITCH = 1
uint8 SOURCE_RC_BUTTON = 2
uint8 SOURCE_RC_MODE_SLOT = 3
uint8 mode # for ACTION_SWITCH_MODE what mode is requested according to commander_state.MAIN_STATE_
uint8 mode # for ACTION_SWITCH_MODE what mode is requested according to vehicle_status_s::NAVIGATION_STATE_*
-24
View File
@@ -1,24 +0,0 @@
# Main state, i.e. what user wants. Controlled by RC or from ground station via telemetry link.
uint64 timestamp # time since system start (microseconds)
uint8 MAIN_STATE_MANUAL = 0
uint8 MAIN_STATE_ALTCTL = 1
uint8 MAIN_STATE_POSCTL = 2
uint8 MAIN_STATE_AUTO_MISSION = 3
uint8 MAIN_STATE_AUTO_LOITER = 4
uint8 MAIN_STATE_AUTO_RTL = 5
uint8 MAIN_STATE_ACRO = 6
uint8 MAIN_STATE_OFFBOARD = 7
uint8 MAIN_STATE_STAB = 8
# LEGACY RATTITUDE = 9
uint8 MAIN_STATE_AUTO_TAKEOFF = 10
uint8 MAIN_STATE_AUTO_LAND = 11
uint8 MAIN_STATE_AUTO_FOLLOW_TARGET = 12
uint8 MAIN_STATE_AUTO_PRECLAND = 13
uint8 MAIN_STATE_ORBIT = 14
uint8 MAIN_STATE_AUTO_VTOL_TAKEOFF = 15
uint8 MAIN_STATE_MAX = 16
uint8 main_state
uint16 main_state_changes
+2 -1
View File
@@ -19,6 +19,7 @@ bool innovation_rejected # true if the observation has been rejected
bool fused # true if the sample was successfully fused
# TOPICS estimator_aid_source_1d
# TOPICS estimator_aid_src_baro_hgt estimator_aid_src_rng_hgt estimator_aid_src_airspeed
# TOPICS estimator_aid_src_baro_hgt estimator_aid_src_ev_hgt estimator_aid_src_gnss_hgt estimator_aid_src_rng_hgt
# TOPICS estimator_aid_src_airspeed estimator_aid_src_sideslip
# TOPICS estimator_aid_src_fake_hgt
# TOPICS estimator_aid_src_mag_heading estimator_aid_src_gnss_yaw estimator_aid_src_ev_yaw
+6 -5
View File
@@ -5,7 +5,7 @@ uint8 estimator_instance
uint32 device_id
uint64[2] time_last_fuse
uint64 time_last_fuse
float32[2] observation
float32[2] observation_variance
@@ -14,9 +14,10 @@ float32[2] innovation
float32[2] innovation_variance
float32[2] test_ratio
bool[2] fusion_enabled # true when measurements are being fused
bool[2] innovation_rejected # true if the observation has been rejected
bool[2] fused # true if the sample was successfully fused
bool fusion_enabled # true when measurements are being fused
bool innovation_rejected # true if the observation has been rejected
bool fused # true if the sample was successfully fused
# TOPICS estimator_aid_source_2d
# TOPICS estimator_aid_src_fake_pos
# TOPICS estimator_aid_src_ev_pos estimator_aid_src_fake_pos estimator_aid_src_gnss_pos
# TOPICS estimator_aid_src_aux_vel estimator_aid_src_optical_flow
+7 -6
View File
@@ -5,7 +5,7 @@ uint8 estimator_instance
uint32 device_id
uint64[3] time_last_fuse
uint64 time_last_fuse
float32[3] observation
float32[3] observation_variance
@@ -14,10 +14,11 @@ float32[3] innovation
float32[3] innovation_variance
float32[3] test_ratio
bool[3] fusion_enabled # true when measurements are being fused
bool[3] innovation_rejected # true if the observation has been rejected
bool[3] fused # true if the sample was successfully fused
bool fusion_enabled # true when measurements are being fused
bool innovation_rejected # true if the observation has been rejected
bool fused # true if the sample was successfully fused
# TOPICS estimator_aid_source_3d
# TOPICS estimator_aid_src_gnss_pos estimator_aid_src_gnss_vel
# TOPICS estimator_aid_src_mag estimator_aid_src_aux_vel
# TOPICS estimator_aid_src_ev_vel
# TOPICS estimator_aid_src_gnss_vel
# TOPICS estimator_aid_src_mag
+1 -1
View File
@@ -1,7 +1,7 @@
uint64 timestamp # time since system start (microseconds)
uint64 timestamp_sample # the timestamp of the raw data (microseconds)
uint32 baro_device_id # unique device ID for the sensor that does not change between power cycles
uint32 device_id # unique device ID for the sensor that does not change between power cycles
float32 bias # estimated barometric altitude bias (m)
float32 bias_var # estimated barometric altitude bias variance (m^2)
+57
View File
@@ -0,0 +1,57 @@
# Input flags for the failsafe state machine set by the arming & health checks.
#
# Flags must be named such that false == no failure (e.g. _invalid, _unhealthy, _lost)
# The flag comments are used as label for the failsafe state machine simulation
uint64 timestamp # time since system start (microseconds)
# Per-mode requirements
uint32 mode_req_angular_velocity
uint32 mode_req_attitude
uint32 mode_req_local_alt
uint32 mode_req_local_position
uint32 mode_req_local_position_relaxed
uint32 mode_req_global_position
uint32 mode_req_mission
uint32 mode_req_offboard_signal
uint32 mode_req_home_position
uint32 mode_req_prevent_arming # if set, cannot arm while in this mode
uint32 mode_req_other # other requirements, not covered above (for external modes)
# Mode requirements
bool angular_velocity_invalid # Angular velocity invalid
bool attitude_invalid # Attitude invalid
bool local_altitude_invalid # Local altitude invalid
bool local_position_invalid # Local position estimate invalid
bool local_position_invalid_relaxed # Local position with reduced accuracy requirements invalid (e.g. flying with optical flow)
bool local_velocity_invalid # Local velocity estimate invalid
bool global_position_invalid # Global position estimate invalid
bool gps_position_invalid # GPS position invalid
bool auto_mission_missing # No mission available
bool offboard_control_signal_lost # Offboard signal lost
bool home_position_invalid # No home position available
# Control links
bool manual_control_signal_lost # Manual control (RC) signal lost
bool gcs_connection_lost # GCS connection lost
# Battery
uint8 battery_warning # Battery warning level
bool battery_low_remaining_time # Low battery based on remaining flight time
bool battery_unhealthy # Battery unhealthy
# Other
bool primary_geofence_breached # Primary Geofence breached
bool mission_failure # Mission failure
bool vtol_transition_failure # VTOL transition failed (quadchute)
bool wind_limit_exceeded # Wind limit exceeded
bool flight_time_limit_exceeded # Maximum flight time exceeded
# Failure detector
bool fd_critical_failure # Critical failure (attitude/altitude limit exceeded, or external ATS)
bool fd_esc_arming_failure # ESC failed to arm
bool fd_imbalanced_prop # Imbalanced propeller detected
bool fd_motor_failure # Motor failure
+12 -10
View File
@@ -1,12 +1,14 @@
uint64 timestamp # time since system start (microseconds)
uint8 GF_ACTION_NONE = 0 # no action on geofence violation
uint8 GF_ACTION_WARN = 1 # critical mavlink message
uint8 GF_ACTION_LOITER = 2 # switch to AUTO|LOITER
uint8 GF_ACTION_RTL = 3 # switch to AUTO|RTL
uint8 GF_ACTION_TERMINATE = 4 # flight termination
uint8 GF_ACTION_LAND = 5 # switch to AUTO|LAND
uint64 timestamp # time since system start (microseconds)
uint8 GF_ACTION_NONE = 0 # no action on geofence violation
uint8 GF_ACTION_WARN = 1 # critical mavlink message
uint8 GF_ACTION_LOITER = 2 # switch to AUTO|LOITER
uint8 GF_ACTION_RTL = 3 # switch to AUTO|RTL
uint8 GF_ACTION_TERMINATE = 4 # flight termination
uint8 GF_ACTION_LAND = 5 # switch to AUTO|LAND
bool geofence_violated # true if the geofence is violated
uint8 geofence_action # action to take when geofence is violated
uint8 geofence_violation_reason # one of geofence_violation_reason_t::*
bool home_required # true if the geofence requires a valid home position
bool primary_geofence_breached # true if the primary geofence is breached
uint8 primary_geofence_action # action to take when the primary geofence is breached
bool home_required # true if the geofence requires a valid home position
-3
View File
@@ -14,9 +14,6 @@ bool warning # true if mission is valid, but has potentially problematic items
bool finished # true if mission has been completed
bool failure # true if the mission cannot continue or be completed for some reason
bool stay_in_failsafe # true if the commander should not switch out of the failsafe mode
bool flight_termination # true if the navigator demands a flight termination from the commander app
bool item_do_jump_changed # true if the number of do jumps remaining has changed
uint16 item_changed_index # indicate which item has changed
uint16 item_do_jump_remaining # set to the number of do jumps remaining for that item
-6
View File
@@ -9,18 +9,12 @@ uint8 SETPOINT_TYPE_TAKEOFF=3 # takeoff setpoint
uint8 SETPOINT_TYPE_LAND=4 # land setpoint, altitude must be ignored, descend until landing
uint8 SETPOINT_TYPE_IDLE=5 # do nothing, switch off motors or keep at idle speed (MC)
uint8 VELOCITY_FRAME_LOCAL_NED = 1 # MAV_FRAME_LOCAL_NED
uint8 VELOCITY_FRAME_BODY_NED = 8 # MAV_FRAME_BODY_NED
bool valid # true if setpoint is valid
uint8 type # setpoint type to adjust behavior of position controller
float32 vx # local velocity setpoint in m/s in NED
float32 vy # local velocity setpoint in m/s in NED
float32 vz # local velocity setpoint in m/s in NED
bool velocity_valid # true if local velocity setpoint valid
uint8 velocity_frame # to set velocity setpoints in NED or body
bool alt_valid # do not set for 3D position control. Set to true if you want z-position control while doing vx,vy velocity control.
float64 lat # latitude, in deg
float64 lon # longitude, in deg
+2
View File
@@ -45,6 +45,7 @@ bool heartbeat_type_gimbal # MAV_TYPE_GIMBAL
bool heartbeat_type_adsb # MAV_TYPE_ADSB
bool heartbeat_type_camera # MAV_TYPE_CAMERA
bool heartbeat_type_parachute # MAV_TYPE_PARACHUTE
bool heartbeat_type_open_drone_id # MAV_TYPE_ODID
# Heartbeats per component
bool heartbeat_component_telemetry_radio # MAV_COMP_ID_TELEMETRY_RADIO
@@ -58,4 +59,5 @@ bool heartbeat_component_uart_bridge # MAV_COMP_ID_UART_BRIDGE
# Misc component health
bool avoidance_system_healthy
bool open_drone_id_system_healthy
bool parachute_system_healthy
+13 -10
View File
@@ -33,8 +33,9 @@ uint8 ARM_DISARM_REASON_UNIT_TEST = 13
uint64 nav_state_timestamp # time when current nav_state activated
# Navigation state "what should vehicle do"
uint8 nav_state
uint8 nav_state_user_intention # Mode that the user selected (might be different from nav_state in a failsafe situation)
uint8 nav_state # Currently active mode
uint8 NAVIGATION_STATE_MANUAL = 0 # Manual mode
uint8 NAVIGATION_STATE_ALTCTL = 1 # Altitude control mode
uint8 NAVIGATION_STATE_POSCTL = 2 # Position control mode
@@ -83,12 +84,11 @@ uint8 VEHICLE_TYPE_ROVER = 3
uint8 VEHICLE_TYPE_AIRSHIP = 4
bool failsafe # true if system is in failsafe state (e.g.:RTL, Hover, Terminate, ...)
uint64 failsafe_timestamp # time when failsafe was activated
bool failsafe_and_user_took_over # true if system is in failsafe state but the user took over control
# Link loss
bool rc_signal_lost # true if RC reception lost
bool data_link_lost # datalink to GCS lost
uint8 data_link_lost_counter # counts unique data link lost events
bool gcs_connection_lost # datalink to GCS lost
uint8 gcs_connection_lost_counter # counts unique GCS connection lost events
bool high_latency_data_link_lost # Set to true if the high latency data link (eg. RockBlock Iridium 9603 telemetry module) is lost
# VTOL flags
@@ -97,9 +97,6 @@ bool is_vtol_tailsitter # True if the system performs a 90° pitch down rotatio
bool in_transition_mode # True if VTOL is doing a transition
bool in_transition_to_fw # True if VTOL is doing a transition from MC to FW
bool mission_failure # Set to true if mission could not continue/finish
bool geofence_violated
# MAVLink identification
uint8 system_type # system type, contains mavlink MAV_TYPE
uint8 system_id # system id, contains MAVLink's system ID field
@@ -107,15 +104,21 @@ uint8 component_id # subsystem / component id, contains MAVLink's component ID f
bool safety_button_available # Set to true if a safety button is connected
bool safety_off # Set to true if safety is off
bool auto_mission_available
bool power_input_valid # set if input power is valid
bool usb_connected # set to true (never cleared) once telemetry received from usb link
bool open_drone_id_system_present
bool open_drone_id_system_healthy
bool parachute_system_present
bool parachute_system_healthy
bool avoidance_system_required # Set to true if avoidance system is enabled via COM_OBS_AVOID parameter
bool avoidance_system_valid # Status of the obstacle avoidance system
bool rc_calibration_in_progress
bool calibration_enabled
bool pre_flight_checks_pass # true if all checks necessary to arm pass
-43
View File
@@ -1,43 +0,0 @@
# TODO: rename to failsafe_flags (will be input to failsafe state machine)
#
uint64 timestamp # time since system start (microseconds)
# Per-mode requirements
uint32 mode_req_angular_velocity
uint32 mode_req_attitude
uint32 mode_req_local_position
uint32 mode_req_local_position_relaxed
uint32 mode_req_global_position
uint32 mode_req_local_alt
uint32 mode_req_mission
uint32 mode_req_offboard_signal
uint32 mode_req_home_position
uint32 mode_req_prevent_arming # if set, cannot arm while in this mode
uint32 mode_req_other # other requirements, not covered above (for external modes)
bool calibration_enabled
bool pre_flight_checks_pass # true if all checks necessary to arm pass
bool auto_mission_available
bool angular_velocity_valid
bool attitude_valid
bool local_altitude_valid
bool local_position_valid # set to true by the commander app if the quality of the local position estimate is good enough to use for navigation
bool local_position_valid_relaxed # Local position with reduced accuracy requirements (e.g. flying with optical flow)
bool local_velocity_valid # set to true by the commander app if the quality of the local horizontal velocity data is good enough to use for navigation
bool global_position_valid # set to true by the commander app if the quality of the global position estimate is good enough to use for navigation
bool gps_position_valid
bool home_position_valid # indicates a valid home position (a valid home position is not always a valid launch)
bool offboard_control_signal_lost
bool rc_signal_found_once
bool rc_calibration_in_progress
bool vtol_transition_failure # Set to true if vtol transition failed
bool battery_low_remaining_time
bool battery_unhealthy
uint8 battery_warning
@@ -39,7 +39,7 @@
// It does not print arguments.
#if 0
#include <px4_platform_common/log.h>
#define CONSOLE_PRINT_EVENT(log_level, id, str) PX4_INFO_RAW("Event 0x%08x: %s\n", id, str)
#define CONSOLE_PRINT_EVENT(log_level, id, str) PX4_INFO_RAW("Event 0x%08" PRIx32 ": %s\n", id, str)
#else
#define CONSOLE_PRINT_EVENT(log_level, id, str)
#endif
@@ -45,7 +45,11 @@
#pragma once
__BEGIN_DECLS
/* configuration limits */
#define MAX_IO_TIMERS 4
#ifdef BOARD_NUM_IO_TIMERS
#define MAX_IO_TIMERS BOARD_NUM_IO_TIMERS
#else
#define MAX_IO_TIMERS 4
#endif
#define MAX_TIMER_IO_CHANNELS 16
#define MAX_LED_TIMERS 2
@@ -78,6 +82,7 @@ typedef uint16_t io_timer_channel_allocation_t; /* big enough to hold MAX_TIMER_
*/
typedef struct io_timers_t {
uint32_t base; /* Base address of the timer */
uint32_t submodle; /* Which Submodule */
uint32_t clock_register; /* SIM_SCGCn */
uint32_t clock_bit; /* SIM_SCGCn bit pos */
uint32_t vectorno; /* IRQ number */
@@ -56,7 +56,6 @@ static inline constexpr timer_io_channels_t initIOTimerChannel(const io_timers_t
PWM::FlexPWMConfig pwm_config, IOMUX::Pad pad)
{
timer_io_channels_t ret{};
PWM::FlexPWM pwm{};
// FlexPWM Muxing Options
@@ -591,7 +590,7 @@ static inline constexpr timer_io_channels_t initIOTimerChannel(const io_timers_t
const uint32_t timer_base = getFlexPWMBaseRegister(pwm);
for (int i = 0; i < MAX_IO_TIMERS; ++i) {
if (io_timers_conf[i].base == timer_base) {
if (io_timers_conf[i].base == timer_base && io_timers_conf[i].submodle == ret.sub_module) {
ret.timer_index = i;
break;
}
@@ -602,11 +601,11 @@ static inline constexpr timer_io_channels_t initIOTimerChannel(const io_timers_t
return ret;
}
static inline constexpr io_timers_t initIOPWM(PWM::FlexPWM pwm)
static inline constexpr io_timers_t initIOPWM(PWM::FlexPWM pwm, PWM::FlexPWMSubmodule sub)
{
io_timers_t ret{};
ret.base = getFlexPWMBaseRegister(pwm);
ret.submodle = sub;
return ret;
}
@@ -431,46 +431,69 @@ static inline void io_timer_set_PWM_mode(unsigned channel)
void io_timer_trigger(unsigned channel_mask)
{
// Any Channels in oneshot?
int oneshots = io_timer_get_mode_channels(IOTimerChanMode_OneShot) & channel_mask;
struct {
uint32_t base;
uint16_t triggers;
} action_cache[MAX_IO_TIMERS] = {0};
int actions = 0;
/* Pre-calculate the list of channels to Trigger */
int mask;
// Yes do triggering
if (oneshots) {
struct {
uint32_t base;
uint16_t triggers;
} action_cache[MAX_IO_TIMERS] = {0};
for (int timer = 0; timer < MAX_IO_TIMERS; timer++) {
action_cache[actions].base = io_timers[timer].base;
int actions = 0;
if (action_cache[actions].base) {
uint32_t first_channel_index = io_timers_channel_mapping.element[timer].first_channel_index;
uint32_t last_channel_index = first_channel_index + io_timers_channel_mapping.element[timer].channel_count;
// Get the Timer modules addresses
for (int timer = 0; timer < MAX_IO_TIMERS && io_timers[timer].base != 0; timer++) {
if (action_cache[actions].base == 0) {
action_cache[actions].base = io_timers[timer].base;
} else if (action_cache[actions].base != io_timers[timer].base) {
actions++;
action_cache[actions].base = io_timers[timer].base;
}
}
/* Pre-calculate the list of channels to Trigger for each Timer module */
int mask;
uint32_t channel = 0;
for (actions = 0; actions < MAX_IO_TIMERS; actions++) {
if (action_cache[actions].base == 0) {
// All have been processed
break;
}
// Group the bits from channels on the same timer
for (; channel < MAX_TIMER_IO_CHANNELS && timer_io_channels[channel].val_offset; channel++) {
if (io_timers[timer_io_channels[channel].timer_index].base != action_cache[actions].base) {
break;
}
for (uint32_t channel = first_channel_index; channel < last_channel_index; channel++) {
mask = get_channel_mask(channel);
if (oneshots & mask) {
action_cache[actions].triggers |= timer_io_channels[channel].sub_module_bits;
}
}
actions++;
}
/* Now do them all with the shortest delay in between */
irqstate_t flags = px4_enter_critical_section();
for (actions = 0; action_cache[actions].base != 0 && actions < MAX_IO_TIMERS; actions++) {
_REG16(action_cache[actions].base, IMXRT_FLEXPWM_MCTRL_OFFSET) |= (action_cache[actions].triggers >> MCTRL_LDOK_SHIFT)
<< MCTRL_CLDOK_SHIFT ;
_REG16(action_cache[actions].base, IMXRT_FLEXPWM_MCTRL_OFFSET) |= action_cache[actions].triggers;
}
px4_leave_critical_section(flags);
}
/* Now do them all with the shortest delay in between */
irqstate_t flags = px4_enter_critical_section();
for (actions = 0; action_cache[actions].base != 0 && actions < MAX_IO_TIMERS; actions++) {
_REG16(action_cache[actions].base, IMXRT_FLEXPWM_MCTRL_OFFSET) |= (action_cache[actions].triggers >> MCTRL_LDOK_SHIFT)
<< MCTRL_CLDOK_SHIFT ;
_REG16(action_cache[actions].base, IMXRT_FLEXPWM_MCTRL_OFFSET) |= action_cache[actions].triggers;
}
px4_leave_critical_section(flags);
}
int io_timer_init_timer(unsigned timer, io_timer_channel_mode_t mode)
@@ -685,44 +708,71 @@ int io_timer_set_enable(bool state, io_timer_channel_mode_t mode, io_timer_chann
}
struct {
uint32_t sm_ens;
uint32_t base;
uint32_t io_index;
uint32_t gpios[MAX_TIMER_IO_CHANNELS];
} action_cache[MAX_IO_TIMERS];
if (masks) {
struct {
uint32_t sm_ens;
uint32_t base;
uint32_t io_index;
uint32_t gpios[MAX_TIMER_IO_CHANNELS];
} action_cache[MAX_IO_TIMERS];
memset(action_cache, 0, sizeof(action_cache));
unsigned int actions = 0;
memset(action_cache, 0, sizeof(action_cache));
for (int chan_index = 0; masks != 0 && chan_index < MAX_TIMER_IO_CHANNELS; chan_index++) {
if (masks & (1 << chan_index)) {
masks &= ~(1 << chan_index);
for (int timer = 0; timer < MAX_IO_TIMERS && io_timers[timer].base != 0; timer++) {
if (action_cache[actions].base == 0) {
action_cache[actions].base = io_timers[timer].base;
if (io_timer_validate_channel_index(chan_index) == 0) {
uint32_t timer_index = channels_timer(chan_index);
action_cache[timer_index].base = io_timers[timer_index].base;
action_cache[timer_index].sm_ens |= MCTRL_RUN(1 << timer_io_channels[chan_index].sub_module) |
timer_io_channels[chan_index].sub_module_bits;
action_cache[timer_index].gpios[action_cache[timer_index].io_index++] = timer_io_channels[chan_index].gpio_out;
} else if (action_cache[actions].base != io_timers[timer].base) {
actions++;
action_cache[actions].base = io_timers[timer].base;
}
}
}
irqstate_t flags = px4_enter_critical_section();
int chan_index = 0;
for (actions = 0; actions < MAX_IO_TIMERS; actions++) {
if (action_cache[actions].base == 0) {
// All have been processed
break;
}
for (; masks != 0 && chan_index < MAX_TIMER_IO_CHANNELS && timer_io_channels[chan_index].val_offset; chan_index++) {
if (masks & (1 << chan_index)) {
if (io_timers[timer_io_channels[chan_index].timer_index].base != action_cache[actions].base) {
break;
}
masks &= ~(1 << chan_index);
action_cache[actions].sm_ens |= MCTRL_RUN(1 << timer_io_channels[chan_index].sub_module) |
timer_io_channels[chan_index].sub_module_bits;
action_cache[actions].gpios[action_cache[actions].io_index++] = timer_io_channels[chan_index].gpio_out;
}
}
}
irqstate_t flags = px4_enter_critical_section();
for (actions = 0; actions < arraySize(action_cache); actions++) {
if (action_cache[actions].base == 0) {
break;
}
for (unsigned actions = 0; actions < arraySize(action_cache); actions++) {
if (action_cache[actions].base != 0) {
for (unsigned int index = 0; index < action_cache[actions].io_index; index++) {
if (action_cache[actions].gpios[index]) {
px4_arch_configgpio(action_cache[actions].gpios[index]);
}
_REG16(action_cache[actions].base, IMXRT_FLEXPWM_MCTRL_OFFSET) = action_cache[actions].sm_ens;
}
_REG16(action_cache[actions].base, IMXRT_FLEXPWM_MCTRL_OFFSET) = action_cache[actions].sm_ens;
}
px4_leave_critical_section(flags);
}
px4_leave_critical_section(flags);
return 0;
}
-1
View File
@@ -47,7 +47,6 @@ endforeach()
# standalone tests
set(cmd_tests
commander_tests
controllib_test
lightware_laser_test
rc_tests
+1 -2
View File
@@ -35,7 +35,7 @@ set(HEXAGON_SDK_INCLUDES
${HEXAGON_SDK_ROOT}/incs
${HEXAGON_SDK_ROOT}/incs/stddef
${HEXAGON_SDK_ROOT}/rtos/qurt/computev66/include/qurt
# ${HEXAGON_SDK_ROOT}/rtos/qurt/computev66/include/posix
${HEXAGON_SDK_ROOT}/rtos/qurt/computev66/include/posix
${HEXAGON_SDK_ROOT}/tools/HEXAGON_Tools/8.4.05/Tools/target/hexagon/include
)
@@ -100,7 +100,6 @@ set(ARCHCPUFLAGS
add_definitions(
-D __QURT
-D _PROVIDE_POSIX_TIME_DECLS
-D _TIMER_T
-D _HAS_C9X
-D restrict=__restrict__
-D noreturn_function=
@@ -966,8 +966,8 @@ void ModalaiEsc::mix_turtle_mode(uint16_t outputs[MAX_ACTUATORS])
float)_parameters.turtle_motor_percent / 100.f);
// Add a little bit to the motorOutputMin so props aren't spinning when sticks are centered
float dead_band_rpm = ((float)_parameters.turtle_motor_deadband / 100.0f) * _rpm_fullscale;
motor_output = (motor_output < _rpm_turtle_min + dead_band_rpm) ? 0.0f : (motor_output - dead_band_rpm);
motor_output = (motor_output < _rpm_turtle_min + _parameters.turtle_motor_deadband) ? 0.0f :
(motor_output - _parameters.turtle_motor_deadband);
// using the output map here for clarity as PX4 motors are 1-4
switch (_output_map[i].number) {
+12
View File
@@ -253,6 +253,18 @@ MS5611::collect()
return ret;
}
// According to the sensor docs:
// If the conversion is not executed before the ADC read command, or the
// ADC read command is repeated, it will give 0 as the output result.
//
// We have seen 0 during the init phase on I2C, therefore, we add this
// protection in.
if (raw == 0) {
perf_count(_comms_errors);
perf_end(_sample_perf);
return ret;
}
/* handle a measurement */
if (_measure_phase == 0) {
@@ -54,6 +54,7 @@ extern "C" __EXPORT int gy_us42_main(int argc, char *argv[])
BusCLIArguments cli{true, false};
cli.rotation = (Rotation)distance_sensor_s::ROTATION_DOWNWARD_FACING;
cli.default_i2c_frequency = 100000;
cli.i2c_address = GY_US42_BASEADDR;
while ((ch = cli.getOpt(argc, argv, "R:")) != EOF) {
switch (ch) {
@@ -38,7 +38,7 @@
void MPU9250_I2C::print_usage()
{
PRINT_MODULE_USAGE_NAME("mpu9520_i2c", "driver");
PRINT_MODULE_USAGE_NAME("mpu9250_i2c", "driver");
PRINT_MODULE_USAGE_SUBCATEGORY("imu");
PRINT_MODULE_USAGE_COMMAND("start");
PRINT_MODULE_USAGE_PARAMS_I2C_SPI_DRIVER(true, false);
@@ -38,7 +38,7 @@
void MPU9250::print_usage()
{
PRINT_MODULE_USAGE_NAME("mpu9520", "driver");
PRINT_MODULE_USAGE_NAME("mpu9250", "driver");
PRINT_MODULE_USAGE_SUBCATEGORY("imu");
PRINT_MODULE_USAGE_COMMAND("start");
PRINT_MODULE_USAGE_PARAMS_I2C_SPI_DRIVER(false, true);
+2 -2
View File
@@ -37,9 +37,9 @@ parameters:
16: (unused) PITCH_ANGLE
17: (unused) ROLL_ANGLE
18: (unused) CROSSHAIRS
19: (unused) AVG_CELL_VOLTAGE
19: AVG_CELL_VOLTAGE
20: (unused) HORIZON_SIDEBARS
21: (unused) POWER
21: POWER
default: 16383
# OSD Log Level
+32 -10
View File
@@ -71,25 +71,44 @@
// Currently working elements positions (hardcoded)
/* center col
Speed Power Alt
Rssi cell_voltage mah
craft name
*/
// Left
const uint16_t osd_gps_lat_pos = 2048;
const uint16_t osd_gps_lon_pos = 2080;
const uint16_t osd_gps_sats_pos = 2112;
const uint16_t osd_rssi_value_pos = 2176;
// Center
const uint16_t osd_home_dir_pos = 2093;
const uint16_t osd_craft_name_pos = 2543;
// Top
const uint16_t osd_disarmed_pos = 2125;
const uint16_t osd_home_dir_pos = 2093;
const uint16_t osd_home_dist_pos = 2095;
// Bottom row 1
const uint16_t osd_gps_speed_pos = 2413;
const uint16_t osd_power_pos = 2415;
const uint16_t osd_altitude_pos = 2416;
// Bottom Row 2
const uint16_t osd_rssi_value_pos = 2445;
const uint16_t osd_avg_cell_voltage_pos = 2446;
const uint16_t osd_mah_drawn_pos = 2449;
// Bottom Row 3
const uint16_t osd_craft_name_pos = 2480;
// Right
const uint16_t osd_main_batt_voltage_pos = 2073;
const uint16_t osd_current_draw_pos = 2103;
const uint16_t osd_mah_drawn_pos = 2138;
const uint16_t osd_altitude_pos = 2233;
const uint16_t osd_numerical_vario_pos = 2267;
const uint16_t osd_gps_speed_pos = 2299;
const uint16_t osd_home_dist_pos = 2331;
const uint16_t osd_numerical_vario_pos = LOCATION_HIDDEN;
MspOsd::MspOsd(const char *device) :
ModuleParams(nullptr),
@@ -147,15 +166,18 @@ void MspOsd::SendConfig()
msp_osd_config.osd_numerical_vario_pos = enabled(SymbolIndex::NUMERICAL_VARIO) ? osd_numerical_vario_pos :
LOCATION_HIDDEN;
msp_osd_config.osd_power_pos = enabled(SymbolIndex::POWER) ? osd_power_pos : LOCATION_HIDDEN;
msp_osd_config.osd_avg_cell_voltage_pos = enabled(SymbolIndex::AVG_CELL_VOLTAGE) ? osd_avg_cell_voltage_pos :
LOCATION_HIDDEN;
// possibly available, but not currently used
msp_osd_config.osd_flymode_pos = LOCATION_HIDDEN;
msp_osd_config.osd_esc_tmp_pos = LOCATION_HIDDEN;
msp_osd_config.osd_pitch_angle_pos = LOCATION_HIDDEN;
msp_osd_config.osd_roll_angle_pos = LOCATION_HIDDEN;
msp_osd_config.osd_crosshairs_pos = LOCATION_HIDDEN;
msp_osd_config.osd_avg_cell_voltage_pos = LOCATION_HIDDEN;
msp_osd_config.osd_horizon_sidebars_pos = LOCATION_HIDDEN;
msp_osd_config.osd_power_pos = LOCATION_HIDDEN;
// Not implemented or not available
msp_osd_config.osd_artificial_horizon_pos = LOCATION_HIDDEN;
+35 -12
View File
@@ -261,7 +261,7 @@ msp_status_BF_t construct_STATUS(const vehicle_status_s &vehicle_status)
break;
default:
status_BF.flight_mode_flags = 0;
status_BF.flight_mode_flags |= 0;
break;
}
}
@@ -277,10 +277,9 @@ msp_analog_t construct_ANALOG(const battery_status_s &battery_status, const inpu
msp_analog_t analog {0};
analog.vbat = battery_status.voltage_v * 10; // bottom right... v * 10
analog.rssi = (uint16_t)((input_rc.rssi * 1023.0f) / 100.0f);
analog.rssi = (uint16_t)((input_rc.link_quality * 1023.0f) / 100.0f);
analog.amperage = battery_status.current_a * 100; // main amperage
analog.mAhDrawn = battery_status.discharged_mah; // unused
return analog;
}
@@ -290,8 +289,8 @@ msp_battery_state_t construct_BATTERY_STATE(const battery_status_s &battery_stat
msp_battery_state_t battery_state = {0};
// MSP_BATTERY_STATE
battery_state.amperage = battery_status.current_a; // not used?
battery_state.batteryVoltage = (uint16_t)(battery_status.voltage_v * 400.0f); // OK
battery_state.amperage = battery_status.current_a * 100.0f; // Used for power element
battery_state.batteryVoltage = (uint16_t)((battery_status.voltage_v / battery_status.cell_count) * 400.0f); // OK
battery_state.mAhDrawn = battery_status.discharged_mah ; // OK
battery_state.batteryCellCount = battery_status.cell_count;
battery_state.batteryCapacity = battery_status.capacity; // not used?
@@ -318,14 +317,24 @@ msp_raw_gps_t construct_RAW_GPS(const sensor_gps_s &vehicle_gps_position,
raw_gps.lat = vehicle_gps_position.lat;
raw_gps.lon = vehicle_gps_position.lon;
raw_gps.alt = vehicle_gps_position.alt / 10;
//raw_gps.groundCourse = vehicle_gps_position_struct
float course = math::degrees(vehicle_gps_position.cog_rad);
if (course < 0) {
course += 360.0f;
}
raw_gps.groundCourse = course * 100.0f; // centidegrees
} else {
raw_gps.lat = 0;
raw_gps.lon = 0;
raw_gps.alt = 0;
raw_gps.groundCourse = 0; // centidegrees
}
raw_gps.groundCourse = 0; // centidegrees
if (vehicle_gps_position.fix_type == 0
|| vehicle_gps_position.fix_type == 1) {
raw_gps.fixType = MSP_GPS_NO_FIX;
@@ -367,20 +376,24 @@ msp_comp_gps_t construct_COMP_GPS(const home_position_s &home_position,
if (home_position.valid_hpos
&& home_position.valid_lpos
&& estimator_status.solution_status_flags & (1 << 4)) {
float bearing_to_home = get_bearing_to_next_waypoint(vehicle_global_position.lat,
vehicle_global_position.lon,
home_position.lat, home_position.lon);
float bearing_to_home = math::degrees(get_bearing_to_next_waypoint(vehicle_global_position.lat,
vehicle_global_position.lon,
home_position.lat, home_position.lon));
if (bearing_to_home < 0) {
bearing_to_home += 360.0f;
}
float distance_to_home = get_distance_to_next_waypoint(vehicle_global_position.lat,
vehicle_global_position.lon,
home_position.lat, home_position.lon);
comp_gps.distanceToHome = (int16_t)distance_to_home; // meters
comp_gps.directionToHome = bearing_to_home; // degrees
comp_gps.directionToHome = bearing_to_home;
} else {
comp_gps.distanceToHome = 0; // meters
comp_gps.directionToHome = 0; // degrees
comp_gps.directionToHome = 0;
}
comp_gps.heartbeat = heartbeat;
@@ -396,7 +409,17 @@ msp_attitude_t construct_ATTITUDE(const vehicle_attitude_s &vehicle_attitude)
matrix::Eulerf euler_attitude(matrix::Quatf(vehicle_attitude.q));
attitude.pitch = math::degrees(euler_attitude.theta()) * 10;
attitude.roll = math::degrees(euler_attitude.phi()) * 10;
attitude.yaw = math::degrees(euler_attitude.psi()) * 10;
//attitude.yaw = math::degrees(euler_attitude.psi()) * 10;
float yaw_fixed = math::degrees(euler_attitude.psi());
if (yaw_fixed < 0) {
yaw_fixed += 360.0f;
}
attitude.yaw = yaw_fixed;
//attitude.yaw = 360;
return attitude;
}
@@ -90,6 +90,7 @@ add_custom_command(OUTPUT ${component_general_json} ${component_general_json}.xz
--version-file ${PX4_BINARY_DIR}/src/lib/version/build_git_version.h
COMMAND ${PYTHON_EXECUTABLE} ${CMAKE_CURRENT_SOURCE_DIR}/generate_crc.py
${component_general_json}
${PX4_BINARY_DIR}/events/all_events.json.xz
--output ${component_information_header}
DEPENDS
generate_component_general.py
@@ -74,7 +74,7 @@ for metadata_type_tuple in args.type:
component_general['metadataTypes'] = metadata_types
with open(filename, 'w') as outfile:
json.dump(component_general, outfile)
json.dump(component_general, outfile, sort_keys=True)
if compress:
save_compressed(filename)
@@ -2,6 +2,7 @@
import argparse
import os
import hashlib
parser = argparse.ArgumentParser(description="""Generate the COMPONENT_INFORMATION checksums (CRC32) header file""")
parser.add_argument('--output', metavar='checksums.h', help='output file')
@@ -30,6 +31,16 @@ def crc_update(buf, crc_table, crc):
crc_table = create_table()
def sha256sum(filename):
h = hashlib.sha256()
b = bytearray(128*1024)
mv = memoryview(b)
with open(filename, 'rb', buffering=0) as f:
for n in iter(lambda : f.readinto(mv), 0):
h.update(mv[:n])
return h.hexdigest()
with open(filename, 'w') as outfile:
outfile.write("#pragma once\n")
outfile.write("#include <stdint.h>\n")
@@ -38,10 +49,12 @@ with open(filename, 'w') as outfile:
file_crc = 0
for line in open(filename, "rb"):
file_crc = crc_update(line, crc_table, file_crc)
file_sha256 = sha256sum(filename)
basename = os.path.basename(filename)
identifier = basename.split('.')[0]
outfile.write("static constexpr uint32_t {:}_crc = {:};\n".format(identifier, file_crc))
outfile.write("static constexpr const char *{:}_sha256 = \"{:}\";\n".format(identifier, file_sha256))
outfile.write("}\n")
+4 -4
View File
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2012-2017 PX4 Development Team. All rights reserved.
* Copyright (c) 2012-2022 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -169,7 +169,7 @@ public:
union DeviceId {
struct DeviceStructure devid_s;
uint32_t devid;
uint32_t devid{0};
};
uint32_t get_device_id() const { return _device_id.devid; }
@@ -268,8 +268,8 @@ protected:
Device(uint8_t devtype, const char *name, DeviceBusType bus_type, uint8_t bus, uint8_t address) : _name(name)
{
set_device_type(devtype);
_device_id.devid_s.bus_type = bus_type;
_device_id.devid_s.bus = bus;
set_device_bus_type(bus_type);
set_device_bus(bus);
set_device_address(address);
}
+82 -18
View File
@@ -276,41 +276,83 @@
}
}
},
"failsafe_reason_t": {
"failsafe_cause_t": {
"type": "uint8_t",
"description": "Reason for entering failsafe",
"description": "Cause for entering failsafe",
"entries": {
"0": {
"name": "no_rc",
"description": "No manual control stick input"
"name": "generic",
"description": ""
},
"1": {
"name": "no_offboard",
"description": "No offboard control inputs"
"name": "manual_control_loss",
"description": "manual control loss"
},
"2": {
"name": "no_rc_and_no_offboard",
"description": "No manual control stick and no offboard control inputs"
"name": "gcs_connection_loss",
"description": "GCS connection loss"
},
"3": {
"name": "no_local_position",
"description": "No local position estimate"
"name": "low_battery_level",
"description": "low battery level"
},
"4": {
"name": "no_global_position",
"description": "No global position estimate"
"name": "critical_battery_level",
"description": "critical battery level"
},
"5": {
"name": "no_datalink",
"description": "No datalink"
"name": "emergency_battery_level",
"description": "emergency battery level"
}
}
},
"failsafe_action_t": {
"type": "uint8_t",
"description": "failsafe action",
"entries": {
"0": {
"name": "none",
"description": ""
},
"1": {
"name": "warn",
"description": "warning"
},
"2": {
"name": "fallback_posctrl",
"description": "fallback to position control"
},
"3": {
"name": "fallback_altctrl",
"description": "fallback to altitude control"
},
"4": {
"name": "fallback_stabilized",
"description": "fallback to stabilized"
},
"5": {
"name": "hold",
"description": "hold"
},
"6": {
"name": "no_rc_and_no_datalink",
"description": "No RC and no datalink"
"name": "rtl",
"description": "RTL"
},
"7": {
"name": "no_gps",
"description": "No valid GPS"
"name": "land",
"description": "land"
},
"8": {
"name": "descend",
"description": "descend"
},
"9": {
"name": "disarm",
"description": "disarm"
},
"10": {
"name": "terminate",
"description": "terminate"
}
}
},
@@ -373,6 +415,10 @@
"13": {
"name": "rc_button",
"description": "RC (button)"
},
"14": {
"name": "failsafe",
"description": "failsafe"
}
}
},
@@ -577,6 +623,24 @@
"description": "Reduce throttle!"
}
}
},
"geofence_violation_reason_t": {
"type": "uint8_t",
"description": "Reason for geofence violation",
"entries": {
"0": {
"name": "dist_to_home_exceeded",
"description": "maximum distance to home exceeded"
},
"1": {
"name": "max_altitude_exceeded",
"description": "maximum altitude exceeded"
},
"2": {
"name": "fence_violation",
"description": "approaching or outside geofence"
}
}
}
},
"navigation_mode_groups": {
+1
View File
@@ -147,6 +147,7 @@ add_custom_command(OUTPUT px4_parameters.hpp
px_generate_params.py
templates/px4_parameters.hpp.jinja
)
add_custom_target(parameters_header DEPENDS px4_parameters.hpp)
set(SRCS)
+1 -1
View File
@@ -114,7 +114,7 @@ class JsonOutput():
#Json string output.
self.output = json.dumps(all_json,indent=2)
self.output = json.dumps(all_json, indent=2, sort_keys=True)
def Save(self, filename):
-1
View File
@@ -4,7 +4,6 @@ Param source code generation script.
"""
from __future__ import print_function
import xml.etree.ElementTree as ET
import codecs
import argparse
import sys
-2
View File
@@ -50,9 +50,7 @@ import argparse
from px4params import srcscanner, srcparser, injectxmlparams, xmlout, markdownout, jsonout
import lzma #to create .xz file
import re
import json
import codecs
def save_compressed(filename):
#create lzma compressed version
@@ -39,9 +39,12 @@
#include <uORB/topics/actuator_armed.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/vehicle_status_flags.h>
#include "../../state_machine_helper.h" // TODO: get independent of transition_result_t
typedef enum {
TRANSITION_DENIED = -1,
TRANSITION_NOT_CHANGED = 0,
TRANSITION_CHANGED
} transition_result_t;
using arm_disarm_reason_t = events::px4::enums::arm_disarm_reason_t;
@@ -242,7 +242,6 @@ TEST(ArmStateMachineTest, ArmingStateTransitionTest)
};
struct vehicle_status_s status {};
struct vehicle_status_flags_s status_flags {};
struct actuator_armed_s armed {};
size_t cArmingTransitionTests = sizeof(rgArmingTransitionTests) / sizeof(rgArmingTransitionTests[0]);
@@ -254,7 +253,7 @@ TEST(ArmStateMachineTest, ArmingStateTransitionTest)
arm_state_machine.forceArmState(test->current_state.arming_state);
status.hil_state = test->hil_state;
HealthAndArmingChecks health_and_arming_checks(nullptr, status_flags, status);
HealthAndArmingChecks health_and_arming_checks(nullptr, status);
// Attempt transition
transition_result_t result = arm_state_machine.arming_state_transition(
+3 -5
View File
@@ -33,6 +33,7 @@
add_subdirectory(failure_detector)
add_subdirectory(HealthAndArmingChecks)
add_subdirectory(failsafe)
add_subdirectory(Arming)
add_subdirectory(ModeUtil)
@@ -51,12 +52,12 @@ px4_add_module(
factory_calibration_storage.cpp
gyro_calibration.cpp
HomePosition.cpp
UserModeIntention.cpp
level_calibration.cpp
lm_fit.cpp
mag_calibration.cpp
rc_calibration.cpp
Safety.cpp
state_machine_helper.cpp
worker_thread.cpp
DEPENDS
circuit_breaker
@@ -69,10 +70,7 @@ px4_add_module(
sensor_calibration
world_magnetic_model
mode_util
failsafe
)
if(PX4_TESTING)
add_subdirectory(commander_tests)
endif()
px4_add_unit_gtest(SRC mag_calibration_test.cpp LINKLIBS modules__commander)
File diff suppressed because it is too large Load Diff
+103 -168
View File
@@ -36,11 +36,12 @@
/* Helper classes */
#include "Arming/ArmStateMachine/ArmStateMachine.hpp"
#include "failure_detector/FailureDetector.hpp"
#include "failsafe/failsafe.h"
#include "Safety.hpp"
#include "state_machine_helper.h"
#include "worker_thread.hpp"
#include "HealthAndArmingChecks/HealthAndArmingChecks.hpp"
#include "HomePosition.hpp"
#include "UserModeIntention.hpp"
#include <lib/controllib/blocks.hpp>
#include <lib/hysteresis/hysteresis.h>
@@ -57,7 +58,6 @@
#include <uORB/topics/vehicle_command_ack.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/vehicle_status_flags.h>
// subscriptions
#include <uORB/Subscription.hpp>
@@ -68,7 +68,6 @@
#include <uORB/topics/battery_status.h>
#include <uORB/topics/cpuload.h>
#include <uORB/topics/distance_sensor.h>
#include <uORB/topics/geofence_result.h>
#include <uORB/topics/iridiumsbd_status.h>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/mission_result.h>
@@ -84,7 +83,6 @@
#include <uORB/topics/vehicle_land_detected.h>
#include <uORB/topics/vehicle_local_position.h>
#include <uORB/topics/vtol_vehicle_status.h>
#include <uORB/topics/wind.h>
using math::constrain;
using systemlib::Hysteresis;
@@ -117,12 +115,11 @@ public:
void enable_hil();
void get_circuit_breaker_params();
private:
void answer_command(const vehicle_command_s &cmd, uint8_t result);
transition_result_t arm(arm_disarm_reason_t calling_reason, bool run_preflight_checks = true);
transition_result_t disarm(arm_disarm_reason_t calling_reason, bool forced = false);
void battery_status_check();
@@ -132,9 +129,11 @@ private:
/**
* Checks the status of all available data links and handles switching between different system telemetry states.
*/
void data_link_check();
void dataLinkCheck();
void manual_control_check();
void manualControlCheck();
void offboardControlCheck();
/**
* @brief Handle incoming vehicle command relavant to Commander
@@ -146,110 +145,43 @@ private:
*/
bool handle_command(const vehicle_command_s &cmd);
unsigned handle_command_actuator_test(const vehicle_command_s &cmd);
unsigned handleCommandActuatorTest(const vehicle_command_s &cmd);
void executeActionRequest(const action_request_s &action_request);
void offboard_control_update();
void printRejectMode(uint8_t nav_state);
void print_reject_mode(uint8_t main_state);
void updateControlMode();
void update_control_mode();
bool shutdown_if_allowed();
bool shutdownIfAllowed();
void send_parachute_command();
void checkWindSpeedThresholds();
void checkForMissionUpdate();
void handlePowerButtonState();
void systemPowerUpdate();
void landDetectorUpdate();
void safetyButtonUpdate();
void vtolStatusUpdate();
void updateTunes();
void checkWorkerThread();
bool getPrearmState() const;
void handleAutoDisarm();
bool handleModeIntentionAndFailsafe();
void updateParameters();
void check_and_inform_ready_for_takeoff();
DEFINE_PARAMETERS(
(ParamInt<px4::params::NAV_DLL_ACT>) _param_nav_dll_act,
(ParamInt<px4::params::COM_DL_LOSS_T>) _param_com_dl_loss_t,
(ParamInt<px4::params::COM_RC_OVERRIDE>) _param_com_rc_override,
(ParamInt<px4::params::COM_HLDL_LOSS_T>) _param_com_hldl_loss_t,
(ParamInt<px4::params::COM_HLDL_REG_T>) _param_com_hldl_reg_t,
(ParamFloat<px4::params::COM_RC_LOSS_T>) _param_com_rc_loss_t,
(ParamInt<px4::params::NAV_RCL_ACT>) _param_nav_rcl_act,
(ParamFloat<px4::params::COM_RCL_ACT_T>) _param_com_rcl_act_t,
(ParamInt<px4::params::COM_RCL_EXCEPT>) _param_com_rcl_except,
(ParamBool<px4::params::COM_HOME_EN>) _param_com_home_en,
(ParamBool<px4::params::COM_HOME_IN_AIR>) _param_com_home_in_air,
(ParamInt<px4::params::COM_POSCTL_NAVL>) _param_com_posctl_navl, /* failsafe response to loss of navigation accuracy */
(ParamInt<px4::params::COM_LOW_BAT_ACT>) _param_com_low_bat_act,
(ParamFloat<px4::params::COM_BAT_ACT_T>) _param_com_bat_act_t,
(ParamInt<px4::params::COM_IMB_PROP_ACT>) _param_com_imb_prop_act,
(ParamFloat<px4::params::COM_DISARM_LAND>) _param_com_disarm_land,
(ParamFloat<px4::params::COM_DISARM_PRFLT>) _param_com_disarm_preflight,
(ParamBool<px4::params::COM_OBS_AVOID>) _param_com_obs_avoid,
(ParamInt<px4::params::COM_FLT_PROFILE>) _param_com_flt_profile,
(ParamFloat<px4::params::COM_OBC_LOSS_T>) _param_com_obc_loss_t,
(ParamFloat<px4::params::COM_WIND_WARN>) _param_com_wind_warn,
// Quadchute
(ParamInt<px4::params::COM_QC_ACT>) _param_com_qc_act,
// Offboard
(ParamFloat<px4::params::COM_OF_LOSS_T>) _param_com_of_loss_t,
(ParamInt<px4::params::COM_OBL_ACT>) _param_com_obl_act,
(ParamInt<px4::params::COM_OBL_RC_ACT>) _param_com_obl_rc_act,
(ParamInt<px4::params::COM_PREARM_MODE>) _param_com_prearm_mode,
(ParamBool<px4::params::COM_FORCE_SAFETY>) _param_com_force_safety,
(ParamBool<px4::params::COM_MOT_TEST_EN>) _param_com_mot_test_en,
(ParamFloat<px4::params::COM_KILL_DISARM>) _param_com_kill_disarm,
(ParamFloat<px4::params::COM_LKDOWN_TKO>) _param_com_lkdown_tko,
// Engine failure
(ParamInt<px4::params::COM_ACT_FAIL_ACT>) _param_com_actuator_failure_act,
(ParamInt<px4::params::COM_FLIGHT_UUID>) _param_flight_uuid,
(ParamInt<px4::params::COM_TAKEOFF_ACT>) _param_takeoff_finished_action,
// Circuit breakers
(ParamInt<px4::params::CBRK_SUPPLY_CHK>) _param_cbrk_supply_chk,
(ParamInt<px4::params::CBRK_USB_CHK>) _param_cbrk_usb_chk,
(ParamInt<px4::params::CBRK_AIRSPD_CHK>) _param_cbrk_airspd_chk,
(ParamInt<px4::params::CBRK_FLIGHTTERM>) _param_cbrk_flightterm,
(ParamInt<px4::params::CBRK_VTOLARMING>) _param_cbrk_vtolarming,
(ParamInt<px4::params::COM_FLT_TIME_MAX>) _param_com_flt_time_max,
(ParamFloat<px4::params::COM_WIND_MAX>) _param_com_wind_max,
(ParamFloat<px4::params::COM_SPOOLUP_TIME>) _param_com_spoolup_time
)
// optional parameters
param_t _param_mav_comp_id{PARAM_INVALID};
param_t _param_mav_sys_id{PARAM_INVALID};
param_t _param_mav_type{PARAM_INVALID};
param_t _param_rc_map_fltmode{PARAM_INVALID};
void checkAndInformReadyForTakeoff();
enum class PrearmedMode {
DISABLED = 0,
@@ -262,110 +194,91 @@ private:
OFFBOARD_MODE_BIT = (1 << 1),
};
enum class ActuatorFailureActions {
DISABLED = 0,
AUTO_LOITER = 1,
AUTO_LAND = 2,
AUTO_RTL = 3,
TERMINATE = 4,
};
/* Decouple update interval and hysteresis counters, all depends on intervals */
static constexpr uint64_t COMMANDER_MONITORING_INTERVAL{10_ms};
static constexpr uint64_t INAIR_RESTART_HOLDOFF_INTERVAL{500_ms};
ArmStateMachine _arm_state_machine{};
vehicle_status_s _vehicle_status{};
bool _geofence_loiter_on{false};
bool _geofence_rtl_on{false};
bool _geofence_land_on{false};
bool _geofence_warning_action_on{false};
bool _geofence_violated_prev{false};
ArmStateMachine _arm_state_machine{};
Failsafe _failsafe_instance{this};
FailsafeBase &_failsafe{_failsafe_instance};
FailureDetector _failure_detector{this};
HealthAndArmingChecks _health_and_arming_checks{this, _vehicle_status};
Safety _safety{};
UserModeIntention _user_mode_intention{this, _vehicle_status, _health_and_arming_checks};
WorkerThread _worker_thread{};
bool _circuit_breaker_flight_termination_disabled{false};
bool _rtl_time_actions_done{false};
FailureDetector _failure_detector;
bool _flight_termination_triggered{false};
bool _lockdown_triggered{false};
bool _imbalanced_propeller_check_triggered{false};
const failsafe_flags_s &_failsafe_flags{_health_and_arming_checks.failsafeFlags()};
HomePosition _home_position{_failsafe_flags};
hrt_abstime _datalink_last_heartbeat_gcs{0};
hrt_abstime _datalink_last_heartbeat_avoidance_system{0};
hrt_abstime _datalink_last_heartbeat_onboard_controller{0};
hrt_abstime _datalink_last_heartbeat_parachute_system{0};
bool _onboard_controller_lost{false};
bool _avoidance_system_lost{false};
bool _parachute_system_lost{true};
Hysteresis _auto_disarm_landed{false};
Hysteresis _auto_disarm_killed{false};
hrt_abstime _high_latency_datalink_heartbeat{0};
hrt_abstime _high_latency_datalink_lost{0};
hrt_abstime _datalink_last_heartbeat_open_drone_id_system{0};
hrt_abstime _datalink_last_heartbeat_avoidance_system{0};
hrt_abstime _datalink_last_heartbeat_gcs{0};
hrt_abstime _datalink_last_heartbeat_onboard_controller{0};
hrt_abstime _datalink_last_heartbeat_parachute_system{0};
uint8_t _battery_warning{battery_status_s::BATTERY_WARNING_NONE};
hrt_abstime _battery_failsafe_timestamp{0};
Hysteresis _auto_disarm_landed{false};
Hysteresis _auto_disarm_killed{false};
Hysteresis _offboard_available{false};
hrt_abstime _last_print_mode_reject_time{0}; ///< To remember when last notification was sent
hrt_abstime _last_print_mode_reject_time{0}; ///< To remember when last notification was sent
bool _mode_switch_mapped{false};
hrt_abstime _high_latency_datalink_heartbeat{0};
hrt_abstime _high_latency_datalink_lost{0};
bool _last_overload{false};
hrt_abstime _last_valid_manual_control_setpoint{0};
bool _is_throttle_above_center{false};
bool _is_throttle_low{false};
hrt_abstime _boot_timestamp{0};
hrt_abstime _last_disarmed_timestamp{0};
hrt_abstime _overload_start{0}; ///< time when CPU overload started
hrt_abstime _boot_timestamp{0};
hrt_abstime _last_disarmed_timestamp{0};
hrt_abstime _overload_start{0}; ///< time when CPU overload started
hrt_abstime _led_armed_state_toggle{0};
hrt_abstime _led_overload_toggle{0};
hrt_abstime _last_termination_message_sent{0};
hrt_abstime _last_health_and_arming_check{0};
bool _status_changed{true};
bool _arm_tune_played{false};
bool _was_armed{false};
bool _failsafe_old{false}; ///< check which state machines for changes, clear "changed" flag
bool _have_taken_off_since_arming{false};
uint8_t _battery_warning{battery_status_s::BATTERY_WARNING_NONE};
bool _failsafe_user_override_request{false}; ///< override request due to stick movements
bool _flight_termination_triggered{false};
bool _lockdown_triggered{false};
bool _open_drone_id_system_lost{true};
bool _avoidance_system_lost{false};
bool _onboard_controller_lost{false};
bool _parachute_system_lost{true};
bool _last_overload{false};
bool _mode_switch_mapped{false};
bool _is_throttle_above_center{false};
bool _is_throttle_low{false};
bool _arm_tune_played{false};
bool _was_armed{false};
bool _have_taken_off_since_arming{false};
bool _status_changed{true};
geofence_result_s _geofence_result{};
vehicle_land_detected_s _vehicle_land_detected{};
vtol_vehicle_status_s _vtol_vehicle_status{};
hrt_abstime _last_wind_warning{0};
// commander publications
actuator_armed_s _actuator_armed{};
commander_state_s _commander_state{};
vehicle_control_mode_s _vehicle_control_mode{};
vehicle_status_s _vehicle_status{};
vehicle_status_flags_s _vehicle_status_flags{};
Safety _safety;
WorkerThread _worker_thread;
vtol_vehicle_status_s _vtol_vehicle_status{};
// Subscriptions
uORB::Subscription _action_request_sub {ORB_ID(action_request)};
uORB::Subscription _action_request_sub{ORB_ID(action_request)};
uORB::Subscription _cpuload_sub{ORB_ID(cpuload)};
uORB::Subscription _geofence_result_sub{ORB_ID(geofence_result)};
uORB::Subscription _iridiumsbd_status_sub{ORB_ID(iridiumsbd_status)};
uORB::Subscription _vehicle_land_detected_sub{ORB_ID(vehicle_land_detected)};
uORB::Subscription _manual_control_setpoint_sub{ORB_ID(manual_control_setpoint)};
uORB::Subscription _system_power_sub{ORB_ID(system_power)};
uORB::Subscription _vehicle_command_sub{ORB_ID(vehicle_command)};
uORB::Subscription _vehicle_land_detected_sub{ORB_ID(vehicle_land_detected)};
uORB::Subscription _vtol_vehicle_status_sub{ORB_ID(vtol_vehicle_status)};
uORB::Subscription _wind_sub{ORB_ID(wind)};
uORB::SubscriptionInterval _parameter_update_sub{ORB_ID(parameter_update), 1_s};
uORB::SubscriptionMultiArray<telemetry_status_s> _telemetry_status_subs{ORB_ID::telemetry_status};
uORB::SubscriptionMultiArray<telemetry_status_s> _telemetry_status_subs{ORB_ID::telemetry_status};
#if defined(BOARD_HAS_POWER_CONTROL)
uORB::Subscription _power_button_state_sub {ORB_ID(power_button_state)};
@@ -376,19 +289,41 @@ private:
// Publications
uORB::Publication<actuator_armed_s> _actuator_armed_pub{ORB_ID(actuator_armed)};
uORB::Publication<commander_state_s> _commander_state_pub{ORB_ID(commander_state)};
uORB::Publication<failure_detector_status_s> _failure_detector_status_pub{ORB_ID(failure_detector_status)};
uORB::Publication<actuator_test_s> _actuator_test_pub{ORB_ID(actuator_test)};
uORB::Publication<vehicle_control_mode_s> _vehicle_control_mode_pub{ORB_ID(vehicle_control_mode)};
uORB::Publication<vehicle_status_flags_s> _vehicle_status_flags_pub{ORB_ID(vehicle_status_flags)};
uORB::Publication<vehicle_status_s> _vehicle_status_pub{ORB_ID(vehicle_status)};
uORB::Publication<failure_detector_status_s> _failure_detector_status_pub{ORB_ID(failure_detector_status)};
uORB::Publication<vehicle_command_ack_s> _vehicle_command_ack_pub{ORB_ID(vehicle_command_ack)};
uORB::Publication<vehicle_control_mode_s> _vehicle_control_mode_pub{ORB_ID(vehicle_control_mode)};
uORB::Publication<vehicle_status_s> _vehicle_status_pub{ORB_ID(vehicle_status)};
orb_advert_t _mavlink_log_pub{nullptr};
perf_counter_t _loop_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": cycle")};
perf_counter_t _preflight_check_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": preflight check")};
HealthAndArmingChecks _health_and_arming_checks;
HomePosition _home_position{_vehicle_status_flags};
// optional parameters
param_t _param_mav_comp_id{PARAM_INVALID};
param_t _param_mav_sys_id{PARAM_INVALID};
param_t _param_mav_type{PARAM_INVALID};
param_t _param_rc_map_fltmode{PARAM_INVALID};
DEFINE_PARAMETERS(
(ParamFloat<px4::params::COM_DISARM_LAND>) _param_com_disarm_land,
(ParamFloat<px4::params::COM_DISARM_PRFLT>) _param_com_disarm_preflight,
(ParamInt<px4::params::COM_DL_LOSS_T>) _param_com_dl_loss_t,
(ParamInt<px4::params::COM_HLDL_LOSS_T>) _param_com_hldl_loss_t,
(ParamInt<px4::params::COM_HLDL_REG_T>) _param_com_hldl_reg_t,
(ParamBool<px4::params::COM_HOME_EN>) _param_com_home_en,
(ParamBool<px4::params::COM_HOME_IN_AIR>) _param_com_home_in_air,
(ParamInt<px4::params::COM_FLT_PROFILE>) _param_com_flt_profile,
(ParamBool<px4::params::COM_FORCE_SAFETY>) _param_com_force_safety,
(ParamFloat<px4::params::COM_KILL_DISARM>) _param_com_kill_disarm,
(ParamBool<px4::params::COM_MOT_TEST_EN>) _param_com_mot_test_en,
(ParamBool<px4::params::COM_OBS_AVOID>) _param_com_obs_avoid,
(ParamFloat<px4::params::COM_OBC_LOSS_T>) _param_com_obc_loss_t,
(ParamInt<px4::params::COM_PREARM_MODE>) _param_com_prearm_mode,
(ParamInt<px4::params::COM_RC_OVERRIDE>) _param_com_rc_override,
(ParamInt<px4::params::COM_FLIGHT_UUID>) _param_flight_uuid,
(ParamInt<px4::params::COM_TAKEOFF_ACT>) _param_takeoff_finished_action
)
};

Some files were not shown because too many files have changed in this diff Show More