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194 Commits

Author SHA1 Message Date
Daniel Agar 97922f3e7e WIP: ODOMETRY quality metric 2022-06-29 10:16:41 -04:00
Daniel Agar 58faa6a8b1 WIP 2022-06-28 21:23:00 -04:00
Martina Rivizzigno 55563eba49 MPC_SPOOLUP_TIME -> COM_SPOOLUP_TIME 2022-06-24 19:44:43 +02:00
Matthias Grob c8fb7a6990 fw/uuv control: remove duplicated comments, restyle initializers 2022-06-24 10:05:16 -05:00
Matthias Grob 78225f7b1f examples/fixedwing_control: use initializers instead of memset 2022-06-24 10:05:16 -05:00
Matthias Grob cfd4e64b02 uuv_pos_control: remove practically unused manual control subscription 2022-06-24 10:05:16 -05:00
Matthias Grob 3a239ff649 examples: remove empty fake_gyro 2022-06-24 10:05:16 -05:00
CUAVhonglang cfa8b451c7 cuav-nora: changed brick to compatible with cuav noraplus 2022-06-24 10:03:43 -05:00
CR ffb0097052 removed unused code - _constrainOneSide and _constrainAbs 2022-06-22 23:21:16 +02:00
Matthias Grob 479c85047f WeatherVane: Allow weathervane on multirotors not just VTOLs 2022-06-22 14:19:28 +02:00
Matthias Grob 54145cedc7 FlightTask: Weather vane cleanup
Remove the entire external yaw handler, dynamic memory allocation,
pointer passing logic. Directly instanciate the weather vane instance
in the flight tasks that support it.
2022-06-22 14:19:28 +02:00
Daniel Agar ab4e10dc26 paa3905: update scaling from datasheet 2022-06-21 16:59:14 -04:00
Daniel Agar 07e28fda7a paw3902: update scaling from datasheet 2022-06-21 16:59:14 -04:00
Daniel Agar dc8ed97809 ekf2: optical flow control limits constrain speed using HAGL max 2022-06-21 12:52:25 -04:00
Daniel Agar 15747239c1 mc_pos_control: always respect position estimate vxy_max if set
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2022-06-21 12:52:25 -04:00
Daniel Agar 5d2dfadb0e boards: px4_fmu-v5_uavcanv0periph disable modules to save flash 2022-06-20 21:31:27 -04:00
Daniel Agar e5f081d9ac drivers/optical_flow/paa3905: cleanup/overhaul
- remove internal accumulation and publish every valid raw sample synchronized with sensor
 - store timestamp_sample from motion interrupt
 - improve timing requirements from datasheet (minimum delays after register read/write)
2022-06-20 20:56:56 -04:00
Daniel Agar 1fbe3c4ab3 drivers/optical_flow/paw3902: cleanup/overhaul
- remove internal accumulation and publish every valid raw sample synchronized with sensor
 - store timestamp_sample from motion interrupt
 - improve timing requirements from datasheet (minimum delays after register read/write)
2022-06-20 20:56:56 -04:00
Daniel Agar d5839e2dd5 optical flow sensor pipeline overhaul
- all sources of optical flow publish sensor_optical_flow
 - sensor_optical_flow is aggregated by the sensors module, aligned with integrated gyro, and published as vehicle_optical_flow

Co-authored-by: alexklimaj <alex@arkelectron.com>
2022-06-20 20:56:56 -04:00
Chuck 32544452f0 drivers: Sagetech MXS transponder support
Co-authored-by: Megan McCormick <megan.mccormick@sagetech.com>
Co-authored-by: Chuck Faber <chuck.faber@sagetech.com>
2022-06-20 18:16:07 -04:00
Claudio Micheli 9d486b1ccd esc_battery: account for online ESCs when averaging voltage
Signed-off-by: Claudio Micheli <claudio@auterion.com>
2022-06-20 18:14:13 -04:00
Daniel Agar 450fcca8b8 drivers/differential_pressure/Kconfig: remove ets and ms4515 from common sensors to save flash 2022-06-20 13:04:19 -04:00
Daniel Agar 8d2e8ef422 boards: px4_fmu-v5_test disable gyro_fft module to save flash 2022-06-20 13:04:19 -04:00
Bruce Meagher 714234ca90 posix: add mavlink shell for posix targets (#19800) 2022-06-20 11:51:47 +02:00
alexklimaj 4cc3e78558 Add mag bias estimator to CAN GPS units with IMUs
- run `sensors` hub to process sensor_mag and publish vehicle_magnetometer
 - update uavcannode to use vehicle_magnetometer
2022-06-19 15:46:36 -04:00
Daniel Agar 73f45fee6e boards: px4_fmu-v5_test disable fake_gps module to save flash 2022-06-19 14:25:06 -04:00
Daniel Agar 902b789292 boards: px4_fmu-v5_protected disable gyro_fft module to save flash 2022-06-19 14:25:01 -04:00
Daniel Agar b81a5b3efa ekf2: request mag yaw reset after calibration or sensor change 2022-06-17 21:04:05 -04:00
Daniel Agar c7cec4252c sensors: add CONFIG_SENSORS_VEHICLE_AIRSPEED for airspeed/differential pressure
- disable CONFIG_SENSORS_VEHICLE_AIRSPEED on boards only used for multicopter
2022-06-17 19:31:45 -04:00
Daniel Agar 10deb7019e enable gyro_calibration for CAN nodes
- allow saving initial gyro cal if very close to 0
2022-06-17 19:31:45 -04:00
Daniel Agar db4e09d529 Tools/kconfig: delete old migration helpers
- people are updating this without really understanding the purpose,
and it's generally no longer useful
2022-06-17 19:31:45 -04:00
Daniel Agar c46fa01195 sensors: add kconfig mechanism to optionally exclude sensor types 2022-06-17 19:31:45 -04:00
Alex Klimaj 60450e63c0 uavcannode: Fix dronecan baro units 2022-06-17 14:22:15 -04:00
Beat Küng b9475d6ebe mavlink_shell: set target system and component id
These got added in https://github.com/mavlink/mavlink/pull/1725 and need
to be set for correct routing.
2022-06-17 09:29:43 -04:00
Daniel Agar dea404a9a3 boards: disable modules to save flash
- px4_fmu-v5x_rtps disable common barometers to save flash
 - px4_fmu-v6x_default disable telemetry drivers to save flash
2022-06-16 16:14:57 -04:00
Junwoo Hwang 8bae4e5c0e FollowMe : Replace First order target position filter with Second order position and velocity filter
Follow me : tidied second order filter implementation

Added velocity filtered info to uORB follow target status message, and rebase to potaito/new-follow-me-task

FollowMe : Rebasing and missing definition fixes on target position second order filter

Follow Me : Remove Alpha filter delay compensation code, since second order filter is used for pose filtering now

Followme : Remove unused target pose estimation update function

Follow Target : Added Target orientation estimation logic

Follow Target : Replaced offset vector based setpoint to rate controlled orbital angle control

Follow Target : Bug fixes and first working version of rate based control logic, still buggy

Follow Target : Added target orientation, follow angle, orbit angle value into follow_target_status uORB message for debugging

Follow Target : Fix orbit angle step calculation typo bug

Follow Target : Few more fixes

Follow Target : Few fixes and follow angle value logging bug fix

Follow Target : Added lowpass alpha filter for yaw setpoint filtering

Follow Target : Remove unused filter delay compensation param

Follow Target : Add Yaw setpoint filter initialization logic and bufix for when unwrap had an input of NAN angle value

Follow Target : Add Yaw setpoint filtering enabler parameter

Follow Target : Change Target Velocity Deadzone to 1.0 m/s, to accomodate walking speed of 1.5 m/s

Follow Target : Add Orbit Tangential Velocity calculation for velocity setpoint and logging uORB topics

Follow target : Fix indentation in yaw setpoint filtering logic

Follow Target : Fix Follow Target Estimator timeout logic bug that was making the 2nd order pose filter reset to raw value every loop

Follow Target : Remove debug printf statement for target pose filter reset check

Follow Target : Add pose filter natural frequency parameter for filter testing

Follow Target : Make target following side param selectable and add target pose filter natural frequency param description

Follow Target : Add Terrain following altitude mode and make 2D altitude mode keep altitude relative to the home position, instead of raw local position origin

Follow Target : Log follow target estimator & status at full rate for filter characteristics test

Follow Target : Implementing RC control user input for Follow Target control

Follow Target : edit to conform to updated unwrap_pi function

Follow Target : Make follow angle, distance and height RC command input configurable

Follow Target : Make Follow Target not interruptable by moving joystick in Commander

Follow Target : reconfigure yaw, pitch and roll for better user experience in RC adjusting configurations, and add angular rate limit taking target distance into account

Follow Target : Change RC channels used for adjustments and re-order header file for clarity

Follow Target : Fix Parameters custom parent macro, since using DEFINE_PARAMETERS alone misses the parameter updates of the parent class, FlightTask

Follow Target : Fix Orbit Tangential speed actually being angular rate bug, which was causing a phenomenon of drnoe getting 'dragged' towards the target velocity direction

Follow Target : Final tidying and refactoring for master merge - step 1

Add more comments on header file

Follow Target : tidy, remove unnecessary debug uORB elements from follow_target_status message

Follow Target : Turn off Yaw filtering by default

Follow Target : Tidy maximum orbital velocity calculation

Follow Target : add yaw setpoint filter time constant parameter for testing and fix NAV_FT_HT title

Follow Target : Add RC adjustment window logic to prevent drone not catching up the change of follow target parameters

Follow Target : fixes

Follow Target: PR tidy few edits remove, and update comments

Follow Target : apply comments and reviews

Follow Target : Edit according to review comments part 2

Follow Target : Split RC adjustment code and other refactors

- Splitted the RC adjustment into follow angle, height and distance
- Added Parameter change detection to reset the follow properties
- Added comments and removed yaw setpoint filter enabler logic

Follow Target : Modify orbit angle error bufferzone bug that was causing excessive velocity setpoints when setpoint catched up with raw orbit setpoint

Follow Target : Remove buffer zone velocity ramp down logic and add acceleration and rate limited Trajectory generation library for orbit angle and velocity setpoint

Follow Target : Remove internally tracked data from local scope function's parameters to simplify code

Follow Target : Fix to track unwrapped orbit angle, with no wrapping

Follow Target : Apply user adjustment deadzone to reduce sensitivity

Follow Target : Apply suggestions from PR review round 2 by @potaito

Revert submodule update changes, fall back to potaito/new-followme-task

Follow Target : [Debug] Expose max vel and acceleration settings as parameters, instead of using Multicopter Position Controller
's settings

Follow Target : Use matrix::isEqualF() function to compare floats

Follow Target : Add Acceleration feedback enabler parameter and Velocity ramp in initial commit for overshoot phenomenon improvement

Follow Target : Implement Velocity feed forward limit and debug logging values

Follow Target : Apply Velocity Ramp-in for Acceleration as well & Apply it to total velocity setpoint and not just orbit tangential velocity component

Follow Target : Don't set Acceleration setpoint if not commanded

Follow Target : Use Jerk limited orbit angle control. Add orbit angle tracking related uORB values"

Follow Target : Add Orbit Angle Setpoint Rate Tracking filter, to take into consideration for calculating velocity setpoint for trajectory generator for orbit angle

Revert "Follow Target : Add Orbit Angle Setpoint Rate Tracking filter, to take into consideration for calculating velocity setpoint for trajectory generator for orbit angle"

This reverts commit a3f48ac7652adb70baf3a2fed3ea34d77cbd6a70.

Follow Target : Take Unfiltered target velocity into acount for target course calculation to fix overshoot orbit angle 180 deg flip problem

Follow Target : Remove Yaw Filter since it doesn't make a big difference in yaw jitterness

Follow Target : Remove velocity ramp in control & remove debug values from follow_target_status.msg

Follow Target : Tidy Follow Target Status message logging code

Follow Target : Remove jerk and acceleration settings from Follow Target orbit trajectory generation

Follow Target : Change PublicationMulti into Publication, since topics published are single instances

Follow Target : Edit comments to reflect changes in the final revision of Follow Target

Follow Target : Apply incorrectly merged conflicts during rebase & update Sticks function usage for getThrottled()

Follow Target : Apply final review comments before merge into Alessandro's PR

Apply further changes from the PR review, like units

Use RC Sticks' Expo() function for user adjustments to decrease sensitivity around the center (0 value)

Update Function styles to lowerCamelCase

And make functions const & return the params, rather than modifying them
internally via pointer / reference

Specify kFollowPerspective enum as uint8_t, so that it can't be set to negative value when converted from the parameter 'FLW_TGT_FP'

Fix bug in updateParams() to reset internally tracked params if they actually changed.

Remove unnecessary comments

Fix format of the Follow Target code

Fix Follow Perspective Param metadata

follow-me: use new trajectory_setpoint msg

Convert FollowPerspective enum into a Follow Angle float value

1. Increases flexibility in user's side, to set any arbitrary follow
angle [deg]
2. Removes the need to have a dedicated Enum, which can be a hassle to
make it match MAVSDK's side
3. A step in the direction of adding a proper Follow Mode (Perspective)
mode support, where we can support kite mode (drone behaves as if it is
hovering & getting dragged by the target with a leash) or a constant
orbit angle mode (Drone always on the East / North / etc. side, for
cinematic shots)

Continue fixing Follow Target MAVSDK code to match MAVSDK changes

- Support Follow Angle configuration instead of Follow Direction
- Change follow position tolerance logic to use the follow angle
*Still work in progress!

Update Follow Me MAVSDK Test Code to match MAVSDK v2 spec

- Add RC Adjustment Test case
- Change follow direction logic to follow angle based logic completely
- Cleanup on variable names and comment on code

follow-me: disable SITL test

Need to update MAVSDK with the following PR:
https://github.com/mavlink/MAVSDK/pull/1770

SITL is failing now because the follow-me
perspectives are no longer defined the
same way in MAVSDK and in the flight task.

update copyright year

follow-me: mark uORB topics optional

Apply review comments

more copyright years

follow-me sitl test: simpler "state machine"

flight_mode_manager: exclude AutoFollowTarget and Orbit on flash contrained boards

Remove unnecessary follow_target_status message properties

- As it eats up FLASH and consumes uLog bandwidth
2022-06-16 16:14:57 -04:00
Alessandro Simovic de1fa11e96 New follow-me flight task
rename follow_me_status to follow_target_status

enable follow_target_estimator on skynode

implement the responsiveness parameter:
The responsiveness parameter should behave similarly to the previous
follow-me implementation in navigator. The difference here is that
there are now two separate gains for position and velocity fusion.
The previous implemenation in navigator had no velocity fusion.

Allow follow-me to be flown without RC

SITL tests for follow-me flight task

This includes:
- Testing the setting for the follow-me angle
- Testing that streaming position only or position
  and velocity measurements both work
- Testing that RC override works

Most of these tests are done with a simulated model
of a point object that moves on a straight line. So
nothing too spectacular. But it makes the test checks
much easier.

Since the estimator for the target actually checks new
measurements and compares them to old ones, I also added
random gausian noise to the measurements with a fixed seed
for deterministic randomness. So repeated runs produce
exactly the same results over and over.

Half of the angles are still missing in MAVSDK. Need to create
an upstream PR to add center left/right and rear left/right options.
These and the corresponding SITL tests need to be implemented
later.

sitl: Increase position tolerance during follow-me

Astro seems to barely exceed the current tolerance (4.3 !< 4.0)
causing CI to fail. The point of the CI test is not to check
the accuracy of the flight behaviour, but only the fact that the
drone is doing the expected thing. So the exact value of this
tolerance is not really important.

follow-me: gimbal control in follow-me

follow-me: create sub-routines in flight task class

follow-me: use ground-dist for emergency ascent

dist_bottom is only defined when a ground facing distance sensor exist.
It's therefore better to use dist_ground instead, which has the distance
to the home altitude if no distance sensor is available.

As a consequence it will only be possible to use follow-me in a valley
when the drone has a distance sensor.

follow-me: point gimbal to the ground in 2D mode

follow-me: another fuzzy msg handling for the estimator

follow-me: bugfix in acceleration saturation limit

follow-me: parameter for filter delay compensation

mantis: dont use flow for terrain estimation

follow-me: default responsiveness 0.5 -> 0.1

0.5 is way too jerky in real and simulated tests.

flight_task: clarify comments for bottom distance

follow-me: minor comment improvement

follow-me: [debug] log emergency_ascent

follow-me: [debug] log gimbal pitch

follow-me: [debug] status values for follow-me estimator

follow-me: setting for gimbal tracking mode

follow-me: release gimbal control at destruction

mavsdk: cosmetics 💄
2022-06-16 16:14:57 -04:00
Chris Seto 285556e463 Re-set param limits for fw tuning values to align with fw tuning guide 2022-06-16 14:22:51 -04:00
Daniel Agar c1c2858341 Update submodule GPSDrivers to latest Thu Jun 16 12:38:52 UTC 2022
- GPSDrivers in PX4/Firmware (1069570a2a90fdc7f0e081b6c2c4b418446d65d7): https://github.com/PX4/PX4-GPSDrivers/commit/016c37cd1f18c716427e2465d8daa6aa1054b0f1
    - GPSDrivers current upstream: https://github.com/PX4/PX4-GPSDrivers/commit/8c09c5426d23ea4db4e462c1f4e3a1de33d253cc
    - Changes: https://github.com/PX4/PX4-GPSDrivers/compare/016c37cd1f18c716427e2465d8daa6aa1054b0f1...8c09c5426d23ea4db4e462c1f4e3a1de33d253cc

    8c09c54 2022-06-15 Daniel Agar - sbf trivial whitespace fix

Co-authored-by: PX4 BuildBot <bot@px4.io>
2022-06-16 12:21:06 -04:00
Matthias Grob 92b6862485 Commander: replace arm requirements 2022-06-16 10:25:32 -04:00
Matthias Grob 3b3d8b9942 Commander: execute pre arm check with preflight checks 2022-06-16 10:25:32 -04:00
Matthias Grob aa575d6af0 Commander: move first preflight check run to constructor 2022-06-16 10:25:32 -04:00
Matthias Grob 0f41a5e385 ArmStateMachine: simplify how preflight checks are called 2022-06-16 10:25:32 -04:00
Igor Mišić 5dc3fecac0 boards/bitcraze: add PWM_SERVO_STOP define 2022-06-16 08:09:00 +02:00
Igor Mišić 7c1da8d608 driver/px4io: set default failsafe values 2022-06-16 08:09:00 +02:00
Igor Mišić 04c2d0fe97 drivers/pwm_out: set default failsafe values 2022-06-16 08:09:00 +02:00
Daniel Agar 1980b5c5e8 ekf2: setEkfGlobalOrigin() reset baro and hgt sensor offsets if necessary
- handle uninitalized _gps_alt_ref
 - add basic lat/lon/alt sanity checks
2022-06-16 00:59:54 -04:00
achim fc3d88bb67 boards/diatone/mamba-f405-mk2: symmetric buffers for wifi telemetry (#19808)
Symmetric buffers allow a much more reliable QGC Wifi telemetry connection especially when (virtual) joysticks are used.  (this board does not provide RX DMA on UART 4 as its timer does DSHOT).
2022-06-15 14:30:28 -04:00
Matthias Grob c59809b14a Commander: remove system_sensors_initialized
and system_hotplug_timeout. They're not in use for over 2 years.
Instead control LED with preflight checks.
2022-06-15 14:02:00 -04:00
Igor Mišić 0922f003f5 uavcan: don't print an error if there is no UAVCAN device on the CAN bus 2022-06-15 03:29:13 -04:00
bresch 680191cc75 WindEstimator: make wind process noise tuning same as EKF2 2022-06-14 18:44:30 +10:00
bresch b6f1a7aed9 migrate wind process noise parameters 2022-06-14 18:39:10 +10:00
bresch 0d256b8ff6 ekf2 wind: use noise spectral density for process noise tuning
The noise spectral density, NSD, (square root of power spectral density) is a
continuous-time parameter that makes the tuning independent from the EKF
prediction rate.
NSD corresponds to the rate at which the state uncertainty increases
when no measurements are fused into the filter.
Given that the current prediction rate of EKF2 is 100Hz, the
same tuning is obtained by dividing the std_dev legacy parameter by 10:
nsd = sqrt(std_dev^2 / 100Hz)
2022-06-14 18:39:10 +10:00
bresch e105869986 wind_estimator: use noise spectral density for process noise tuning
The noise spectral density, NSD, (square root of power spectral density) is a
continuous-time parameter that makes the tuning independent from the EKF
prediction rate.
NSD corresponds to the rate at which the state uncertainty increases
when no measurements are fused into the filter.
Given that the current prediction rate of the wind estimator is 1Hz, the
same tuning is obtained with the same values as before.
2022-06-14 18:39:10 +10:00
Junwoo Hwang 377338109c uLog message definition comment improvements
- Added more comments
- Converted to DOxygen comment format for the comments on struct members
2022-06-13 10:31:07 +02:00
Junwoo Hwang 1ddd1573be Improve uLog message struct definitions
1. Rename *_header_s structs to *_s, since the _header postfix is not
helpful
2. Rename the "key" string variables in the message structs to
"key_value_str" as the string actually contains not just the key but the
key and value pair information
3. Add comments on other uLog messages to clarify use (need more
improvement / can be even more simplified)
2022-06-13 10:31:07 +02:00
achim e6f90bcb81 disable uart´s dma
Still no way to get GPS and auto flash of the IO without disabling their uart´s dma
2022-06-11 13:39:01 -04:00
fury1895 283aad01fd Airspeed params: change default for ASPD_SCALE_APPLY to 2 2022-06-10 14:02:41 +02:00
David Sidrane f15eb91814 px4_fmu-v6x:HB Mini add Ver 3, Ver 4 init 2022-06-10 04:20:26 -07:00
PX4 BuildBot e33199c182 Update submodule mavlink to latest Fri Jun 10 00:38:25 UTC 2022
- mavlink in PX4/Firmware (59630bcc7e7e983db2d9138c8254144c77855adc): https://github.com/mavlink/mavlink/commit/0909631552187b998dd6359f998ee78ee8765728
    - mavlink current upstream: https://github.com/mavlink/mavlink/commit/05864e218e204f1ebeee5555988150fcddbd873e
    - Changes: https://github.com/mavlink/mavlink/compare/0909631552187b998dd6359f998ee78ee8765728...05864e218e204f1ebeee5555988150fcddbd873e

    05864e21 2022-06-09 Peter Barker - common.xml: add ignition_voltage to EFI_STATUS (#1854)
adc9c3f5 2022-06-01 olliw42 - update storm32.xml (nfc) (#1851)
49dbdb66 2022-06-01 Randy Mackay - ardupilotmega: add nav_attitude_time command (#1852)
2022-06-10 01:01:20 -04:00
Thomas Debrunner 46c9d1e288 SIH in SITL with lockstep (#19028)
* sih: Move sih out of work queue
This reverts commit bb7dd0cf00.

* sih-sim: Enable sih in sitl, together with lockstep

* sih-sim: new files for sih: quadx and airplane

* sih: Added tailsitter for sih-sitl simulation

* sitl_target: Added seperate target loop for sih

* jmavsim_run: Allow jmavsim to run in UDP mode

* lockstep: Post semaphore on last lockstep component removed

* sih-sim: Added display for effectively achieved speed

* sih: increase stack size

* sih-sim: Improved sleep time computation, fixes bug of running too fast

* sitl_target: place omnicopter in alphabethic order

Co-authored-by: romain-chiap <romain.chiap@gmail.com>
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2022-06-09 09:52:34 +02:00
Thomas Stastny a7e11464c1 fw pos ctrl: update method documentation 2022-06-09 09:23:02 +02:00
Thomas Stastny 594a6d6e80 fw pos ctrl: some incremental clean up of the class
- documentation of units, params, returns, and descriptions for variables and methods
- rename ambiguous or erroneous state variables
- remove unused or unecessary input arguments to functions
- remove ugly header white space
2022-06-09 09:23:02 +02:00
Silvan Fuhrer 9863c24b40 navigator_main: DO_REPOSITION: only trigger reposition setpoint update if vehicle is armed
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-06-08 21:47:06 +02:00
Thomas Stastny cbf0fe8803 fw pos ctrl: centralize parameter and state resets 2022-06-08 08:44:30 -05:00
Thomas Stastny ccfbbb553a fw pos ctrl: only manipulate heading hold yaw in manual position control mode 2022-06-08 08:44:30 -05:00
Thomas Stastny 67d8dd359d fw pos ctrl: calculate control interval once
- Use the same time interval for all position control logic (including TECS)
- Sync naming in control methods
- Remove some unused input arguments
2022-06-08 08:44:30 -05:00
Matthias Grob f5e7b1e6a8 Commander: switch battery bitflied to dedicated datatype 2022-06-08 11:32:26 +02:00
Matthias Grob 9b2166de72 manual_control_params: configure arm gesture doesn't require reboot
I added wrong documentation here.
2022-06-08 05:12:05 -04:00
Matthias Grob bd50a52c9c Commander: fix startup sound interrupted by safety button initialization
The safetyButtonHandler() reports that the safety statatus
changed on the first loop iteration when safety is disabled which makes
sense to inform the system that safety is off but the tune for the user
should not be played because it interrupts the startup tune.
2022-06-08 05:12:05 -04:00
Matthias Grob 71103e6114 Safety: keep initialized constant flags when safety disabled 2022-06-08 05:12:05 -04:00
Matthias Grob 44c4b8fa85 Style refactoring related to safety button 2022-06-08 05:12:05 -04:00
Daniel Agar ce70b6f4ac sensors/vehicle_angular_velocity: add IMU_GYRO_RATEMAX constraints 2022-06-07 15:45:47 -04:00
Daniel Agar 01f0992f49 sensors/vehicle_imu: don't bother checking IMU_GYRO_RATEMAX 2022-06-07 15:45:47 -04:00
Matthias Grob 5df266cedc MulticopterRateControl: use constructor to copy thrust setpoint array 2022-06-07 11:45:59 -04:00
bresch 4f1091792f ekf2 preflight: only check innovation of active height sources 2022-06-07 11:44:56 -04:00
Daniel Agar cb2738e187 Update submodule GPSDrivers to latest Sat Jun 4 12:38:49 UTC 2022 (#19766)
- GPSDrivers in PX4/Firmware (6e77a084cd43830c8b13018b7fd5470da9bc4ff5): https://github.com/PX4/PX4-GPSDrivers/commit/181fae1a4b5e33576d786755782adb2f195ecc48
    - GPSDrivers current upstream: https://github.com/PX4/PX4-GPSDrivers/commit/016c37cd1f18c716427e2465d8daa6aa1054b0f1
    - Changes: https://github.com/PX4/PX4-GPSDrivers/compare/181fae1a4b5e33576d786755782adb2f195ecc48...016c37cd1f18c716427e2465d8daa6aa1054b0f1

    016c37c 2022-06-01 Julian Oes - sbf: fix overrun on invalid length
2022-06-04 15:58:56 -04:00
PX4BuildBot a247b42907 [AUTO COMMIT] update change indication 2022-06-04 15:57:11 -04:00
PX4 BuildBot e86a74321e Update world_magnetic_model to latest Sat Jun 4 11:14:10 UTC 2022 2022-06-04 15:57:11 -04:00
Beat Küng da55256f2f test_multicopter_failure_injection: remove 'Reject before arming' test
Not sure why injection should fail before arming.
2022-06-04 07:40:29 +02:00
Beat Küng d1142008f6 FailureDetector: check if ESCs have current
And increase the timeout to 300ms, as some ESCs only update with 10Hz.
2022-06-04 07:40:29 +02:00
Beat Küng 8bf18e31be SITL: enable failure command (SYS_FAILURE_EN=1) 2022-06-04 07:40:29 +02:00
Beat Küng 56faaae959 failure: fix invalid memory access
failure_units[unit].key was incorrect
2022-06-04 07:40:29 +02:00
Beat Küng 0ab61aee2e control_allocator: show motor axis for MC (as advanced) 2022-06-04 07:40:29 +02:00
Beat Küng 99a329f937 mc_rate_control: pass through 3D thrust 2022-06-04 07:40:29 +02:00
Beat Küng 82eb71d70b failure_detector: allow disabling attitude failure (as already documented) 2022-06-04 07:40:29 +02:00
Jaeyoung-Lim bf68d3433e Add omnicopter SITL model
F
2022-06-04 07:40:29 +02:00
bresch e2955bdd61 terrain est: clear innovation/var/test ration when aiding stops 2022-06-03 17:31:14 -04:00
Matthias Grob fad3d46907 Use signNoZero() where possible 2022-06-03 16:08:16 +02:00
abarcis 4fc2640ee3 vehicle_command.msg: unneeded comment closings removed (#19759)
They cause problems with building px4_msgs in ROS2 Humble Hawksbill and removing them fixes the issue.

Co-authored-by: Agata Barcis <agata.barcis@tii.ae>
2022-06-03 07:25:05 +02:00
BA-ED b9be783b69 dshot: corrected DShot motor spin direction command
Some ESCs don't store DShot_cmd_spin_direction_reversed persistently
2022-06-02 13:36:40 +02:00
Thomas Watson d390e6d46d boards/mro/pixracerpro: fix voltage/current monitoring
This corrects the board definition to use the proper polarity
for the brick power valid signal, thus allowing the board to
detect the battery and monitor it properly.
2022-06-02 08:11:15 +02:00
Mark Sauder c19e74784a attitude_estimator_q: Run() method refactoring (#19526)
* Refactor attitude_estimator_q_main.cpp Run() method by breaking apart into separate method calls:
    * update_vehicle_local_position()
    * update_motion_capture_odometry()
    * update_visual_odometry()
    * update_magnetometer()
    * update_vehicle_attitude()
    * update_sensors()
 * Rename init_attitude_q()
 * Standardize whitespace formatting
 * Add remaining c++ style initializers.
2022-06-01 13:41:42 -04:00
Daniel Agar 21b1c933dc ekf2: EKFGSF_yaw delete unnecessary internal state 2022-06-01 13:16:06 -04:00
Daniel Agar 3889b79342 ekf2: yaw estimator add yaw_composite_valid boolean 2022-06-01 13:16:06 -04:00
Igor Mišić a218f4bfaf drivers/px4io: support legacy px4io firmware to enter BL 2022-06-01 13:15:13 -04:00
Igor Mišić 25488da944 px4io: replace safety_off state with safety button event (#19558)
internal PX4IO safety_off state is removed and replaced with a normal safety button event. From this 'commit' commander is taking care of the PX4IO safety.
2022-06-01 13:15:13 -04:00
Matthias Grob a9cdfff7a3 FlightModeManager: only execute flight task commands when multicopter 2022-06-01 15:14:07 +02:00
Matthias Grob 96b0304049 PreFlightCheck: disallow arming in land mode
after the automatic switch to Hold mode was introduced.
2022-06-01 12:08:32 +12:00
Matthias Grob 83c15fca9f Commander: switch back to Hold mode after autonomous landing 2022-06-01 12:08:32 +12:00
Matthias Grob 33df8b24f2 Commander: differentiate clearly between to arm and to disarm transition 2022-06-01 12:08:32 +12:00
Matthias Grob 400e1f8214 Commander: only initialize to tablet mode and don't switch back on RC loss 2022-06-01 12:08:32 +12:00
Daniel Agar 002579b3e0 Jenkins: reboot after ostest completes
- temporary workaround to ostest apparently leaving the system in a bad state
2022-05-31 01:41:07 -07:00
Daniel Agar 5b6e5a0968 boards: NuttX update all boards to preallocated sem holder list
- CONFIG_SEM_PREALLOCHOLDERS=32
 - CONFIG_SEM_NNESTPRIO=16 (default)
2022-05-31 01:41:07 -07:00
Beat Küng 0074894637 control_allocator: disable backup schedule with lockstep
The backup schedule triggers updates too early and leads to simulator errors:
ERROR [simulator] poll timeout 0, 22
2022-05-31 07:17:30 +02:00
Daniel Agar 132a07f53c boards: test boards add NuttX ostest and run on Jenkins test rack 2022-05-29 13:41:16 -04:00
Daniel Agar 0420d697e5 update NuttX and apps to latest with sem holder fixes and updated ostest 2022-05-29 13:41:16 -04:00
Daniel Agar cb8b5ae872 mavlink: MavlinkStatustextHandlerTest ignore Wcast-align 2022-05-29 09:44:48 -04:00
Daniel Agar d97bb168cf lib/motion_planning: VelocitySmoothingTest delete set but not used variable 2022-05-29 09:44:48 -04:00
Daniel Agar 095e0f0604 ekf2: sensor_simulator fix enum shadow 2022-05-29 00:21:08 -04:00
PX4 BuildBot 63155b5b01 Update submodule mavlink to latest Sat May 28 00:38:55 UTC 2022
- mavlink in PX4/Firmware (56106be4805cb2f70d22ad31b87fbd9774f0d0f3): https://github.com/mavlink/mavlink/commit/99e82cad70494903a23a67de08ff9cbb5918d8f3
    - mavlink current upstream: https://github.com/mavlink/mavlink/commit/0909631552187b998dd6359f998ee78ee8765728
    - Changes: https://github.com/mavlink/mavlink/compare/99e82cad70494903a23a67de08ff9cbb5918d8f3...0909631552187b998dd6359f998ee78ee8765728

    09096315 2022-05-26 Hamish Willee - Clarify and cross reference home position everywhere (#1836)
38c1a99f 2022-05-25 Julian Oes - WIND_COV: clarify description and unknown value (#1845)
2022-05-28 00:06:05 -04:00
David Lechner 995265c95e vscode: remove terminal settings
These terminal settings are a matter of personal preference and should
not be part of the project configuration.
2022-05-27 21:01:33 -04:00
Daniel Agar c27b9f3b1e boards: reduce SPI DMA buffers on older STM32F4 boards
- on common IMUs like the mpu6000, mpu9250, icm20602, etc each FIFO
sample is only 12 bytes so this is still more than large enough for the
worst case transfer
2022-05-27 16:27:41 -04:00
Daniel Agar 4561cf2ce6 boards: pixhawk 2 cube skip starting low quality l3gd20 gyro to save memory and cpu
- free memory is getting tight on these older boards (depending on
configuratoin) and the pixhawk 2 cube still has 2 other superior IMUs, so this is just
dropping dead weight
2022-05-27 16:27:41 -04:00
David Sidrane 74a2930315 px4_fmu-v6X:Added Holybro mini base board 2022-05-27 15:02:28 -04:00
David Sidrane dd6d7e9979 uc_stm32h7_can:Correct initalization of the mumber of interfaces
H7 Only supports 2 not 3 CAN interfaces.

   CanInitHelper passes in in the run time configuration of
   the number of interfaces. The code was ignoring these!
2022-05-27 15:02:28 -04:00
David Sidrane 9353c15e8a px4_fmu-v5X:Added Holybro mini base board 2022-05-27 15:02:28 -04:00
David Sidrane 479b52fd02 Update all H7 Bootloders 2022-05-27 14:25:25 -04:00
David Sidrane 645f4c3428 flash_cache:Flush complete cache line 2022-05-27 14:25:25 -04:00
David Sidrane fd81951391 boards: STM32H7 pad to 256 bit - 32 bytes (#19724) 2022-05-27 14:04:51 -04:00
Daniel Agar 1ba3610cfc boards: delete omnibus_f4sd_ekf2 due to flash overflow 2022-05-27 09:46:07 -04:00
David Sidrane 55cfd8597d px4_fmu-v6c:Fix mag rotation 2022-05-26 11:26:29 -07:00
Igor Misic 554283655c Revert "px4io: replace safety_off state with safety button event (#19558)"
This reverts commit 12a81979a8.
2022-05-26 10:06:32 -04:00
Igor Misic 6aefcbb6cf Revert "px4iofirmware: fix for bug introduced with #19558"
This reverts commit 79a34b5aed.
2022-05-26 10:06:32 -04:00
Matthias Grob c03f5b9481 Commander: fix overlooked rebase naming error 2022-05-25 21:10:19 +02:00
alessandro 29c4119e24 Match commander uORB var names to message names (#19707)
* match vehicle_status

* match home_position

* match vehicle_command_ack

* match actuator_armed

* match vehicle_control_mode

* match commander_state
2022-05-25 17:08:48 +02:00
Daniel Agar 98354ba10a Update submodule GPSDrivers to latest Wed May 25 12:38:58 UTC 2022
- devices in PX4/Firmware (7cc84e0f9e44697475b0f355df9a29de6ea6b9ff): https://github.com/PX4/PX4-GPSDrivers/commit/58968922b718176be8756f11113d16b2cfbc4022
    - devices current upstream: https://github.com/PX4/PX4-GPSDrivers/commit/181fae1a4b5e33576d786755782adb2f195ecc48
    - Changes: https://github.com/PX4/PX4-GPSDrivers/compare/58968922b718176be8756f11113d16b2cfbc4022...181fae1a4b5e33576d786755782adb2f195ecc48

    181fae1 2022-05-23 numan - README: add information for definition.h
2022-05-25 09:56:40 -04:00
Daniel Agar 58ea6235fe ekf2: estimator aid source status (range height) 2022-05-25 09:25:12 -04:00
Daniel Agar 1e25aee6fa ekf2: estimator aid source status (baro height) 2022-05-25 09:25:12 -04:00
Silvan Fuhrer 4dbe6f0a1c simulator_mavlink: fix MAV_TYPE_VTOL_TAILSITTER case
This type (23) doesn't specify a motor number, so it can't be properly handled.
There are duo (19) and quad (20) tailsitter types that still work in simulation.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-24 17:58:44 -04:00
Daniel Agar 376201e64d boards: px4_fmu-v5/v5x init all I2C pins 2022-05-24 11:02:03 -04:00
bresch d04a91a3ae ekf2_post-processing: use estimator_status_flags instead of bitmasks 2022-05-24 16:15:42 +02:00
Beat Küng 016b8aeb35 MulticopterRateControl: fix thrust sign for acro
Regression from fbc109436f
2022-05-24 15:03:17 +02:00
Matthias Grob 44be415e0e mission_block: make "Delay until" item work while landed
To enable landing, waiting and taking off again e.g. for delivery.
2022-05-24 13:42:03 +02:00
Matthias Grob 0be474430c Commander: don't disarm on landing amid a mission 2022-05-24 13:42:03 +02:00
Matthias Grob 4f34207c4e battery_params: increase default empty cellvoltage to 3.6v
Based on feedback that very often the battery is used down too low.
I observed this happens consistently when the cell voltage is properly
load compensated. The default load compensation before #19429 was very
inaccurate and resulted in unpredictable estimate.
After that if there is a usable current measurement and the battery is
within expected tolerances of the default internal resistance the
compensation is pretty good and 3.5V is too low for an empty compensated
cell voltage. That was seen in various logs where the compensated
cell voltage was already dropping fast after 3.6V.

In case the voltage is not load compensated the vehicle estimates the
state of charge a bit too low which is safer than to high
especially for a default configuration.
2022-05-24 11:26:58 +02:00
Mark Sauder a1fb9fb7c6 rcS: Keep Mag Cal with AUTOCONFIG param reset in rcS, deprecate rcS AUTOCNF param (#19693)
* Deprecate the rcS AUTOCNF script param and associated logic.

* Update posix rcS to match previous commit.
2022-05-23 20:35:22 -04:00
Daniel Agar 639222dd65 ekf2: estimator aid source status (GPS pos, GPS vel) 2022-05-23 16:21:49 -04:00
Daniel Agar 1ae467e9cd ekf2: estimator aid source status (starting with fake position) 2022-05-23 16:21:49 -04:00
Igor Misic 79a34b5aed px4iofirmware: fix for bug introduced with #19558 2022-05-23 14:59:11 -04:00
Daniel Agar d25a784a3a icm42688p: only check configured registers periodically (as intended) 2022-05-23 14:58:23 -04:00
bresch c57c575cfe ekf2: use explicit flags instead of bitmask position
This prevents bitmask mismatch when a new flag is inserted
2022-05-23 14:43:02 -04:00
Matthias Grob 62edcc7a57 battery: only compensate using sane current 2022-05-23 16:40:32 +02:00
Matthias Grob 2cbdcc9671 battery: default to reasonable internal resistance
instead of disabling the load compensation using current.
2022-05-23 16:40:32 +02:00
Matthias Grob 58b1139a21 battery: allow setting precise internal resistance with parameter 2022-05-23 16:40:32 +02:00
Matthias Grob 2c5a7ea118 battery: rather undercompensate for load
than over compensate which makes the estimate to high and breaks batteries
beause they get flown for too long.
2022-05-23 16:40:32 +02:00
Serhat Aksun bc220ddb82 sensors/vehicle_magnetometer: fix multi_mode check
Signed-off-by: Serhat Aksun <serhat.aksun@maxwell-innovations.com>
2022-05-23 10:09:41 -04:00
Igor Misic 12a81979a8 px4io: replace safety_off state with safety button event (#19558)
internal PX4IO safety_off state is removed and replaced with a normal safety button event. From this 'commit' commander is taking care of the PX4IO safety.
2022-05-23 06:54:37 +02:00
Igor Misic 08dcc72e1f commander/safety: replace safety.msg with Safety class (#19558) 2022-05-23 06:54:37 +02:00
Daniel Agar b800600a6c boards: px4_fmu-v2_fixeding disable fw_autotune_attitude_control to save flash 2022-05-22 12:32:24 -04:00
Daniel Agar 61d5a23445 Jenkinsfile: hardware test rack skip runing HITL airframes 2022-05-22 12:31:08 -04:00
Julian Oes 47bcee70c4 ROMFS: disable UAVCAN in HITL
Without this, uavcan creates MixingOutput classes which then create
empty actuator_outputs publications. This then prevents the motor
output in HITL to be forwarded to the simulator via mavlink.
2022-05-21 17:53:20 -04:00
bresch 00e88a02c0 baro bias: improve innovation sequence monitoring
The baro observation noise parameter is often over-estimated in order as
a measure to mitigate temporary offsets in the readings due to wind
gusts or poor pressure compensation tuning. The side effect is that the
innovation sequence monitoring based on normalized innovation struggles
to detect an offset in the state because the innovation isn't
statistically significant.
To counter this issue, a simpler check is added to trigger the process
noise boost when the innovation has the same sign for a long period of
time.
2022-05-21 22:37:04 +02:00
PX4 BuildBot c3f10c2cb1 Update submodule sitl_gazebo to latest Sat May 21 12:38:49 UTC 2022
- sitl_gazebo in PX4/Firmware (422be90140): https://github.com/PX4/PX4-SITL_gazebo/commit/48440d7b5c78a21182415266334981f1163f4b2c
    - sitl_gazebo current upstream: https://github.com/PX4/PX4-SITL_gazebo/commit/5eb5df80450a412076bfc24e7dd343839020f056
    - Changes: https://github.com/PX4/PX4-SITL_gazebo/compare/48440d7b5c78a21182415266334981f1163f4b2c...5eb5df80450a412076bfc24e7dd343839020f056

    5eb5df8 2022-04-28 stmoon - ROS2_PLUGIN set OFF by default
c8f4d5b 2022-04-28 stmoon - update the motor failure plugin for ros2
2022-05-21 14:58:42 -04:00
Daniel Agar db4545e442 Update world_magnetic_model to latest Sat May 21 11:14:10 UTC 2022 2022-05-21 14:57:55 -04:00
mcsauder 6b0788ff46 Standardize variable naming and formatting across vehicle attitude controller files. 2022-05-21 12:22:18 -04:00
Junwoo Hwang 422be90140 Update Issue and Pull Request Templates
1. Change the paragraph headings to proper Markdown headings (easier to
link / structure the Markdown)
2. Move PULL_REQUEST_TEMPLATE into .github folder
3. Change description in Issue template and remove outdated DevGuide
Repository information
4. Add a bug emoji to bug report isue template
5. Support automatically adding labels 'bug-report' and
'feature-request' to easily sort / filter appropriate issues in Github
2022-05-20 21:01:14 -04:00
Julian Oes d08e5eae2d sitl_gazebo: update submodule
This fixes the issue where HITL doesn't connect over USB.
2022-05-20 21:00:33 -04:00
Daniel Agar c40631c136 commander: handle RC loss timeout if manual_control_setpoint stops publishing (#19680)
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2022-05-20 19:37:30 -04:00
David Sidrane 2bdeb36ea3 px4_fmu-v6x:Add Rev 4 Sensors 2022-05-20 15:52:32 -04:00
David Sidrane 9d0e57230a boards: new px4_fmu-v6c board support (#19544) 2022-05-20 15:49:06 -04:00
Julian Oes 33a77c225c commander: lockdown is not termination
We use lockdown to prevent outputs like motors and servos from being
active in HITL simulation. This means that we can't treat the lockdown
flag as a flight_terminated, otherwise we can't arm in HITL at all.
2022-05-20 09:43:32 -04:00
Nicolas MARTIN a0cb7f6258 HITL: undefined time_remaining_s should be NAN 2022-05-20 09:38:43 -04:00
Nico van Duijn 04071b9456 Commander: ignore MAV_CMD_REQUEST_MSG
This commit adds the MAV_CMD_REQUEST_MESSAGE to the list of vehicle
commands which are ignored without generating a warning sound.
2022-05-20 15:36:42 +02:00
Matthias Grob 38e027ee45 ArmStateMachine: remove dependency on armed.armed
To have the internal state as single source of truth
for the arming state within Commander.
2022-05-20 13:51:51 +02:00
Matthias Grob 37c485ce89 ArmStateMachine: move arm state into the class 2022-05-20 13:51:51 +02:00
Matthias Grob 47532ca07b ArmStateMachine: replace state name array with method 2022-05-20 13:51:51 +02:00
alessandro c5bbf4553b ubuntu.sh: fix gazebo and openjdk for 22.04 2022-05-20 06:38:09 +02:00
Matthias Grob 887fe7dba2 commander_params: shorten low battery action delay
I got multiple times the feedback now that a consistent delay
is helpful and makes sense but the default delay
is too long
for low battery action where you're trying to come back in time
and possibly the emergency reaction kicks in while the critical action
is executing which leads to a longer accumulated delay.
2022-05-19 21:54:09 +02:00
Daniel Agar fd4b62032e commander: publish actuator_armed first on any change 2022-05-19 12:47:50 -04:00
PX4 BuildBot 9518b65f93 Update submodule mavlink to latest Thu May 19 00:38:59 UTC 2022
- mavlink in PX4/Firmware (87c73145b36a835b1635de0498a5613a7af5cafc): https://github.com/mavlink/mavlink/commit/a1cb2c0e71f191f04da3d92d92db8702a7e91ff6
    - mavlink current upstream: https://github.com/mavlink/mavlink/commit/99e82cad70494903a23a67de08ff9cbb5918d8f3
    - Changes: https://github.com/mavlink/mavlink/compare/a1cb2c0e71f191f04da3d92d92db8702a7e91ff6...99e82cad70494903a23a67de08ff9cbb5918d8f3

    99e82cad 2022-05-19 Hamish Willee - Deprecated GPS_INJECT_DATA (#1842)
bf3df03d 2022-05-16 Hamish Willee - WIND_COV - accuracy units are m/s (#1844)
a73d4864 2022-05-11 Hamish Willee - development.xml FIGURE_EIGHT_EXECUTION_STATUS - add a note about it being set at lower rate (#1841)
2022-05-18 21:41:08 -04:00
mcsauder e8da98fd14 Add gyro clipping to mirror accel clipping monitoring instances. 2022-05-18 21:16:05 -04:00
mcsauder ea10eacb99 Replace EKF/common.h #defines with enums. 2022-05-18 09:25:19 -04:00
Silvan Fuhrer 8f2c84d36f VTOL paras: add min of 0.1 to transition times
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Silvan Fuhrer c29ca6c959 tailsitter: guard against division by 0
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Silvan Fuhrer 3cf07e1be5 VTOL: rename params _PTCH to _PITCH
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Silvan Fuhrer 7c5f0121a5 VTOL: remove some unsued variables
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Silvan Fuhrer 2b7efeacca vtol_vehicle_status: replace several status bools by single vehicle_vtol_state
Replace vtol_in_rw_mode, vtol_in_trans_mode, in_transition_to_fw by vehicle_vtol_state.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Silvan Fuhrer 635f64a2e5 Commander: remove permanent stabilization option for fixed-wing flight
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Silvan Fuhrer d8444df11c Set tailsitter flag via vehicle status
Removes the necessity of including vtol_type.h in other modules.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Silvan Fuhrer 7292ce483c VTOL: move to cpp params API
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2022-05-18 10:01:04 +02:00
Daniel Agar ff16131874 icm42670p run at full speed 2022-05-17 08:14:22 -07:00
Daniel Agar 83daf648ef drivers/imu/invensense/icm42670p: cleanup and small fixes 2022-05-17 08:14:22 -07:00
Peter van der Perk 3ea492b7a2 UCANS32K146 Fix CAN1 STB pin 2022-05-17 03:13:05 -07:00
Matthias Grob 02e11eddce mavlink_mission: add more specific information to the error message 2022-05-17 07:49:00 +02:00
Junwoo Hwang 146f0cafe0 Add get*Expo() functions to the Sticks library
To return Exponential Values, which is helpful for reducing the
sensitivity of the stick around the centered value (0), since it's
exponential curve.

Useful for user adjustment implementations, where accidentally touching the stick
wouldn't have so much effect when using the Exponential value, compared
to using the raw position value.
2022-05-16 23:55:05 +02:00
Matthias Grob 4bd2d4cf35 rc_update: add unit tests for mode slot
To verify RC mode switch and mode button functionality works as expected.
2022-05-16 14:37:29 +02:00
achim 3fe4c6e3f5 boards: matek h743-mini specify drivers to still fit to flash
- the code has become a bit bigger again that now the drivers have to be specified a bit more precisely to still fit into the flash.
2022-05-13 14:05:04 -04:00
Beat Küng 32df76ca8a dshot: handle DSHOT_MIN for reversible outputs
Also ensures there's no deadband if dead_l == dead_h (the default).
2022-05-13 14:04:01 -04:00
Matthias Grob 57a0289627 trajectory_setpoint: correct comment typo "kinematically"
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com>
2022-05-12 17:19:48 +02:00
Matthias Grob 4017f4bb0b vehicle_local_position_setpoint: reorder fields for clarity 2022-05-12 17:19:48 +02:00
Matthias Grob b67fbac296 uuv_pos_control: siplify passing on trajectory position setpoint 2022-05-12 17:19:48 +02:00
Matthias Grob 200124f094 mavlink_receiver: check entire Vectors for NAN
Note: Behavioral change Inf also results in the flag being true.
2022-05-12 17:19:48 +02:00
Matthias Grob 8ca28f3796 Separate message for trajectory setpoint 2022-05-12 17:19:48 +02:00
580 changed files with 27774 additions and 13298 deletions
+1
View File
@@ -105,6 +105,7 @@ pipeline {
"px4_fmu-v5_stackcheck",
"px4_fmu-v5_uavcanv0periph",
"px4_fmu-v5x_default",
"px4_fmu-v6c_default",
"px4_fmu-v6u_default",
"px4_fmu-v6x_default",
"px4_io-v2_default",
+8 -2
View File
@@ -794,7 +794,7 @@ void resetParameters() {
void runTests() {
// test loading a range of airframes
sh './Tools/HIL/test_airframes.sh `find /dev/serial -name *usb-*` 1000 1001 2100 3000 4001 6001 8001 10016'
sh './Tools/HIL/test_airframes.sh `find /dev/serial -name *usb-*` 2100 3000 4001 6001 8001 10016'
resetParameters()
@@ -809,6 +809,9 @@ void runTests() {
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "top once"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "work_queue status"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "ostest"'
sh './Tools/HIL/reboot.py --device `find /dev/serial -name *usb-*`' // reboot after ostest
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander_tests" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "controllib_test"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "lightware_laser_test"'
@@ -864,12 +867,15 @@ void printTopics() {
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener cpuload" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener distance_sensor" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener ekf2_timestamps" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_gps_status" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener esc_status" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_aid_src_fake_pos" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_aid_src_gnss_pos" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_aid_src_gnss_vel" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_attitude" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_baro_bias" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_event_flags" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_global_position" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_gps_status" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_innovation_test_ratios" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_innovation_variances" || true'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "listener estimator_innovations" || true'
+10 -8
View File
@@ -1,32 +1,34 @@
---
name: Bug report
name: 🐛 Bug report
about: Create a report to help us improve
labels: bug-report
---
**Describe the bug**
## Describe the bug
A clear and concise description of the bug.
**To Reproduce**
## To Reproduce
Steps to reproduce the behavior:
1. Drone switched on '...'
2. Uploaded mission '....' (attach QGC mission file)
3. Took off '....'
4. See error
**Expected behavior**
## Expected behavior
A clear and concise description of what you expected to happen.
**Log Files and Screenshots**
## Log Files and Screenshots
*Always* provide a link to the flight log file:
- Download the flight log file from the vehicle ([tutorial](https://docs.px4.io/master/en/getting_started/flight_reporting.html)).
- Share the link to a log showing the problem on [PX4 Flight Review](http://logs.px4.io/).
- Upload the log to the [PX4 Flight Review](http://logs.px4.io/)
- Share the link to the log (Copy and paste the URL of the log)
Add screenshots to help explain your problem.
**Drone (please complete the following information):**
## Drone (please complete the following information):
- Describe the type of drone.
- Photo of the IMU / autopilot setup if possible.
**Additional context**
## Additional context
Add any other context about the problem here.
+5 -4
View File
@@ -1,19 +1,20 @@
---
name: 🚀 Feature Request
about: Suggest an idea for this project
labels: feature-request
---
For general questions please use [PX4 Discuss](http://discuss.px4.io/) or Slack (you can find an invite link on this project README).
**Describe problem solved by the proposed feature**
## Describe problem solved by the proposed feature
A clear and concise description of the problem, if any, this feature will solve. E.g. I'm always frustrated when ...
**Describe your preferred solution**
## Describe your preferred solution
A clear and concise description of what you want to happen.
**Describe possible alternatives**
## Describe possible alternatives
A clear and concise description of alternative solutions or features you've considered.
**Additional context**
## Additional context
Add any other context or screenshots for the feature request here.
+6 -3
View File
@@ -1,10 +1,13 @@
---
name: ⛔ Support Question
about: See [PX4 Discuss](http://discuss.px4.io/) for questions about using PX4.
about: See http://discuss.px4.io/ for questions about using PX4.
---
We use GitHub issues only to discuss PX4 bugs and new features. For
questions about using PX4 or related components, please use [PX4 Discuss](http://discuss.px4.io/).
## Attention! Please read the note below
We use GitHub issues only to discuss PX4 bugs and new features.
**For questions about using PX4 or related components, please use [PX4 Discuss](http://discuss.px4.io/).**
Thanks!
@@ -1,9 +1,11 @@
---
name: ⛔ Documentation Issue
about: See https://github.com/PX4/Devguide for documentation issues
about: See https://github.com/PX4/px4_user_guide for documentation issues
---
PX4 has dedicated repositories for developer documentation (https://github.com/PX4/Devguide) and user documentation (https://github.com/PX4/px4_user_guide).
## Attention! Please read the note below
**Please submit the documentation issue to the [User Guide](https://github.com/PX4/px4_user_guide) repository.**
Thanks!
@@ -1,17 +1,17 @@
Please use [PX4 Discuss](http://discuss.px4.io/) or [Slack](http://slack.px4.io/) to align on pull requests if necessary. You can then open draft pull requests to get early feedback.
**Describe problem solved by this pull request**
A clear and concise description of the problem this proposed change will solve.
## Describe problem solved by this pull request
A clear and concise description of the problem this proposed change will solve. Or, what it will improve.
E.g. For this use case I ran into...
**Describe your solution**
## Describe your solution
A clear and concise description of what you have implemented.
**Describe possible alternatives**
## Describe possible alternatives
A clear and concise description of alternative solutions or features you've considered.
**Test data / coverage**
## Test data / coverage
How was it tested? What cases were covered? Logs uploaded to https://review.px4.io/ and screenshots of the important plot parts.
**Additional context**
## Additional context
Add any other related context or media.
+1
View File
@@ -61,6 +61,7 @@ jobs:
px4_fmu-v4pro,
px4_fmu-v5,
px4_fmu-v5x,
px4_fmu-v6c,
px4_fmu-v6u,
px4_fmu-v6x,
raspberrypi_pico,
-2
View File
@@ -126,8 +126,6 @@
},
"search.showLineNumbers": true,
"telemetry.enableTelemetry": false,
"terminal.integrated.copyOnSelection": true,
"terminal.integrated.rightClickBehavior": "paste",
"terminal.integrated.scrollback": 5000,
"window.title": "${dirty} ${activeEditorMedium}${separator}${rootName}",
"workbench.editor.highlightModifiedTabs": true,
+2 -1
View File
@@ -325,12 +325,13 @@ px4io_update: px4_io-v2_default cubepilot_io-v2_default
cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v5/extras/px4_io-v2_default.bin
cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v5x/extras/px4_io-v2_default.bin
cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v6x/extras/px4_io-v2_default.bin
cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v6c/extras/px4_io-v2_default.bin
# cubepilot_io-v2_default
cp build/cubepilot_io-v2_default/cubepilot_io-v2_default.bin boards/cubepilot/cubeorange/extras/cubepilot_io-v2_default.bin
cp build/cubepilot_io-v2_default/cubepilot_io-v2_default.bin boards/cubepilot/cubeyellow/extras/cubepilot_io-v2_default.bin
git status
bootloaders_update: cuav_nora_bootloader cuav_x7pro_bootloader cubepilot_cubeorange_bootloader holybro_durandal-v1_bootloader matek_h743_bootloader matek_h743-mini_bootloader matek_h743-slim_bootloader modalai_fc-v2_bootloader mro_ctrl-zero-classic_bootloader mro_ctrl-zero-h7_bootloader mro_ctrl-zero-h7-oem_bootloader mro_pixracerpro_bootloader px4_fmu-v6u_bootloader px4_fmu-v6x_bootloader
bootloaders_update: cuav_nora_bootloader cuav_x7pro_bootloader cubepilot_cubeorange_bootloader holybro_durandal-v1_bootloader holybro_kakuteh7_bootloader matek_h743_bootloader matek_h743-mini_bootloader matek_h743-slim_bootloader modalai_fc-v2_bootloader mro_ctrl-zero-classic_bootloader mro_ctrl-zero-h7_bootloader mro_ctrl-zero-h7-oem_bootloader mro_pixracerpro_bootloader px4_fmu-v6c_bootloader px4_fmu-v6u_bootloader px4_fmu-v6x_bootloader
git status
.PHONY: coverity_scan
+19 -1
View File
@@ -86,10 +86,28 @@ unset BOARD_RC_SENSORS
. ${R}etc/init.d/rc.serial
# Check for flow sensor
if param compare SENS_EN_PX4FLOW 1
if param compare -s SENS_EN_PX4FLOW 1
then
px4flow start -X &
fi
if param compare -s IMU_GYRO_CAL_EN 1
then
gyro_calibration start
fi
if param compare -s MBE_ENABLE 1
then
# conservative mag bias estimation
param set-default MBE_LEARN_GAIN 5
param set-default IMU_GYRO_CUTOFF 20
mag_bias_estimator start
fi
param set-default SENS_MAG_RATE 100
sensors start
uavcannode start
unset R
@@ -0,0 +1,101 @@
#!/bin/sh
#
# @name 6DoF Omnicopter SITL
#
# @type Quadrotor Wide
#
# @maintainer Jaeyoung Lim <jalim@ethz.ch>
#
. ${R}etc/init.d/rc.mc_defaults
param set-default SYS_CTRL_ALLOC 1
param set-default CA_AIRFRAME 0
param set-default CA_ROTOR_COUNT 8
param set-default CA_R_REV 255
param set-default CA_ROTOR0_PX 0.14435
param set-default CA_ROTOR0_PY -0.14435
param set-default CA_ROTOR0_PZ -0.14435
param set-default CA_ROTOR0_KM 0.05 # CCW
param set-default CA_ROTOR0_AX -0.788675
param set-default CA_ROTOR0_AY -0.211325
param set-default CA_ROTOR0_AZ -0.57735
param set-default CA_ROTOR1_PX -0.14435
param set-default CA_ROTOR1_PY -0.14435
param set-default CA_ROTOR1_PZ -0.14435
param set-default CA_ROTOR1_KM 0.05
param set-default CA_ROTOR1_AX 0.211325
param set-default CA_ROTOR1_AY -0.788675
param set-default CA_ROTOR1_AZ 0.57735
param set-default CA_ROTOR2_PX 0.14435
param set-default CA_ROTOR2_PY 0.14435
param set-default CA_ROTOR2_PZ -0.14435
param set-default CA_ROTOR2_KM 0.05
param set-default CA_ROTOR2_AX -0.211325
param set-default CA_ROTOR2_AY 0.788675
param set-default CA_ROTOR2_AZ 0.57735
param set-default CA_ROTOR3_PX -0.14435
param set-default CA_ROTOR3_PY 0.14435
param set-default CA_ROTOR3_PZ -0.14435
param set-default CA_ROTOR3_KM 0.05
param set-default CA_ROTOR3_AX 0.788675
param set-default CA_ROTOR3_AY 0.211325
param set-default CA_ROTOR3_AZ -0.57735
param set-default CA_ROTOR4_PX 0.14435
param set-default CA_ROTOR4_PY -0.14435
param set-default CA_ROTOR4_PZ 0.14435
param set-default CA_ROTOR4_KM 0.05
param set-default CA_ROTOR4_AX 0.788675
param set-default CA_ROTOR4_AY 0.211325
param set-default CA_ROTOR4_AZ -0.57735
param set-default CA_ROTOR5_PX -0.14435
param set-default CA_ROTOR5_PY -0.14435
param set-default CA_ROTOR5_PZ 0.14435
param set-default CA_ROTOR5_KM 0.05
param set-default CA_ROTOR5_AX -0.211325
param set-default CA_ROTOR5_AY 0.788675
param set-default CA_ROTOR5_AZ 0.57735
param set-default CA_ROTOR6_PX 0.14435
param set-default CA_ROTOR6_PY 0.14435
param set-default CA_ROTOR6_PZ 0.14435
param set-default CA_ROTOR6_KM 0.05
param set-default CA_ROTOR6_AX 0.211325
param set-default CA_ROTOR6_AY -0.788675
param set-default CA_ROTOR6_AZ 0.57735
param set-default CA_ROTOR7_PX -0.14435
param set-default CA_ROTOR7_PY 0.14435
param set-default CA_ROTOR7_PZ 0.14435
param set-default CA_ROTOR7_KM 0.05
param set-default CA_ROTOR7_AX -0.788675
param set-default CA_ROTOR7_AY -0.211325
param set-default CA_ROTOR7_AZ -0.57735
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
param set-default PWM_MAIN_FUNC3 103
param set-default PWM_MAIN_FUNC4 104
param set-default PWM_MAIN_FUNC5 105
param set-default PWM_MAIN_FUNC6 106
param set-default PWM_MAIN_FUNC7 107
param set-default PWM_MAIN_FUNC8 108
# disable MC desaturation which improves attitude tracking
param set-default CA_METHOD 0
# disable attitude failure detection
param set-default FD_FAIL_P 0
param set-default FD_FAIL_R 0
set MIXER skip
set MIXER_AUX none
@@ -0,0 +1,23 @@
#!/bin/sh
#
# @name QuadrotorX SITL for SIH
#
# @type Quadrotor
#
# @maintainer Romain Chiappinelli <romain.chiap@gmail.com>
#
. ${R}etc/init.d/rc.mc_defaults
set MIXER quad_x
# disable some checks to allow to fly:
# - with usb
param set-default CBRK_USB_CHK 197848
# - without real battery
param set-default CBRK_SUPPLY_CHK 894281
# - without safety switch
param set-default COM_PREARM_MODE 0
param set-default CBRK_IO_SAFETY 22027
param set SIH_VEHICLE_TYPE 0
@@ -0,0 +1,33 @@
#!/bin/sh
#
# @name Plane SITL for SIH
#
# @type Plane
#
# @maintainer Romain Chiappinelli <romain.chiap@gmail.com>
. ${R}etc/init.d/rc.fw_defaults
set MIXER AERT
# disable some checks to allow to fly:
# - with usb
param set-default CBRK_USB_CHK 197848
# - without real battery
param set-default CBRK_SUPPLY_CHK 894281
# - without safety switch
param set-default COM_PREARM_MODE 0
param set-default CBRK_IO_SAFETY 22027
param set-default BAT_N_CELLS 3
param set SIH_T_MAX 6.0
param set SIH_MASS 0.3
param set SIH_IXX 0.00402
param set SIH_IYY 0.0144
param set SIH_IZZ 0.0177
param set SIH_IXZ 0.00046
param set SIH_KDV 0.2
param set SIH_VEHICLE_TYPE 1 # sih as fixed wing
param set RWTO_TKOFF 1 # enable takeoff from runway (as opposed to launched)
@@ -0,0 +1,45 @@
#!/bin/sh
#
# @name SIH Tailsitter Duo
#
# @type VTOL
#
# @maintainer Romain Chiappinelli <romain.chiap@gmail.com>
. ${R}etc/init.d/rc.vtol_defaults
param set-default VT_ELEV_MC_LOCK 0
param set-default VT_TYPE 0
param set-default VT_FW_DIFTHR_EN 1
param set-default VT_FW_DIFTHR_SC 0.3
param set-default MPC_MAN_Y_MAX 60
param set-default MC_PITCH_P 5
param set-default MAV_TYPE 19
set MAV_TYPE 19
set MIXER vtol_tailsitter_duo_sat
# disable some checks to allow to fly:
# - with usb
param set-default CBRK_USB_CHK 197848
# - without real battery
param set-default CBRK_SUPPLY_CHK 894281
# - without safety switch
param set-default COM_PREARM_MODE 0
param set-default CBRK_IO_SAFETY 22027
param set-default BAT_N_CELLS 3
param set SIH_T_MAX 2.0
param set SIH_Q_MAX 0.0165
param set SIH_MASS 0.2
# IXX and IZZ are inverted from the thesis as the body frame is pitched by 90 deg
param set SIH_IXX 0.00354
param set SIH_IYY 0.000625
param set SIH_IZZ 0.00300
param set SIH_IXZ 0.0
param set SIH_KDV 0.2
param set SIH_L_ROLL 0.145
# sih as tailsitter
param set SIH_VEHICLE_TYPE 2
@@ -18,3 +18,7 @@ param set-default LPE_FAKE_ORIGIN 1
param set-default MPC_ALT_MODE 2
param set-default SENS_FLOW_ROT 6
param set-default SENS_FLOW_MINHGT 0.7
param set-default SENS_FLOW_MAXHGT 3.0
param set-default SENS_FLOW_MAXR 2.5
@@ -9,7 +9,6 @@
# EKF2
param set-default EKF2_AID_MASK 2
param set-default SENS_FLOW_ROT 0
# LPE: Flow-only mode
param set-default LPE_FUSION 242
@@ -35,8 +35,12 @@ px4_add_romfs_files(
10016_iris
10017_iris_ctrlalloc
10018_iris_foggy_lidar
10019_omnicopter
10020_if750a
10030_px4vision
10040_quadx
10041_airplane
10042_xvert
1010_iris_opt_flow
1010_iris_opt_flow.post
1011_iris_irlock
@@ -30,3 +30,12 @@ mavlink start -x -u $udp_onboard_payload_port_local -r 4000 -f -m onboard -o $ud
# Onboard link to gimbal
mavlink start -x -u $udp_onboard_gimbal_port_local -r 400000 -m gimbal -o $udp_onboard_gimbal_port_remote
# To display for SIH sitl
if [ "$SIM_MODE" = "sihsim" ]; then
udp_sihsim_port_local=$((19450+px4_instance))
udp_sihsim_port_remote=$((19410+px4_instance))
mavlink start -x -u $udp_sihsim_port_local -r 400000 -m custom -o $udp_sihsim_port_remote
mavlink stream -r 200 -s HIL_ACTUATOR_CONTROLS -u $udp_sihsim_port_local
mavlink stream -r 25 -s HIL_STATE_QUATERNION -u $udp_sihsim_port_local
fi
+8 -12
View File
@@ -95,10 +95,9 @@ fi
if param compare SYS_AUTOCONFIG 1
then
# Reset params except Airframe, RC calibration, sensor calibration, flight modes, total flight time, and next flight UUID.
param reset_all SYS_AUTOSTART RC* CAL_* COM_FLTMODE* LND_FLIGHT* TC_* COM_FLIGHT*
set AUTOCNF yes
# Wipe out params except RC*, flight modes, total flight time, accel cal, gyro cal, next flight UUID
param reset_all SYS_AUTO* RC* COM_FLTMODE* LND_FLIGHT* TC_* CAL_ACC* CAL_GYRO* COM_FLIGHT*
fi
# multi-instance setup
@@ -155,6 +154,8 @@ param set-default SDLOG_DIRS_MAX 7
param set-default TRIG_INTERFACE 3
param set-default SYS_FAILURE_EN 1
# Adapt timeout parameters if simulation runs faster or slower than realtime.
if [ -n "$PX4_SIM_SPEED_FACTOR" ]; then
COM_DL_LOSS_T_LONGER=$(echo "$PX4_SIM_SPEED_FACTOR * 10" | bc)
@@ -196,14 +197,6 @@ fi
. "$autostart_file"
#
# If autoconfig parameter was set, reset it and save parameters.
#
if [ $AUTOCNF = yes ]
then
param set SYS_AUTOCONFIG 0
fi
# Simulator IMU data provided at 250 Hz
param set IMU_INTEG_RATE 250
@@ -211,8 +204,11 @@ param set IMU_INTEG_RATE 250
. px4-rc.params
dataman start
# start sih in sih_sim mode, otherwise simulator module
if [ "$SIM_MODE" = "sihsim" ]; then
sih start
# only start the simulator if not in replay mode, as both control the lockstep time
if ! replay tryapplyparams
elif ! replay tryapplyparams
then
. px4-rc.simulator
fi
@@ -61,6 +61,8 @@ param set-default HIL_ACT_FUNC6 400
param set SYS_HITL 1
param set UAVCAN_ENABLE 0
# disable some checks to allow to fly
# - with usb
param set-default CBRK_USB_CHK 197848
@@ -15,6 +15,8 @@ set MIXER quad_x
param set SYS_HITL 1
param set UAVCAN_ENABLE 0
param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 0.15
param set-default CA_ROTOR0_PY 0.15
@@ -94,6 +94,8 @@ param set-default HIL_ACT_FUNC8 203
param set SYS_HITL 1
param set UAVCAN_ENABLE 0
# disable some checks to allow to fly
# - with usb
param set-default CBRK_USB_CHK 197848
@@ -131,7 +131,6 @@ param set-default VT_F_TRANS_DUR 1
param set-default VT_IDLE_PWM_MC 1025
param set-default VT_B_REV_OUT 0.5
param set-default VT_B_TRANS_THR 0.7
param set-default VT_FW_PERM_STAB 1
param set-default VT_TRANS_TIMEOUT 22
param set-default VT_F_TRANS_RAMP 4
@@ -62,7 +62,7 @@ param set-default MPC_JERK_AUTO 4
param set-default MPC_LAND_SPEED 1
param set-default MPC_MAN_TILT_MAX 25
param set-default MPC_MAN_Y_MAX 40
param set-default MPC_SPOOLUP_TIME 1.5
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
@@ -104,7 +104,6 @@ param set-default SDLOG_PROFILE 131
param set-default SENS_CM8JL65_CFG 104
param set-default SENS_FLOW_MAXHGT 25
param set-default SENS_FLOW_MINHGT 0.5
param set-default SENS_FLOW_ROT 0
param set-default IMU_GYRO_CUTOFF 100
param set-default SENS_EN_PMW3901 1
@@ -47,6 +47,7 @@ param set-default COM_RC_LOSS_T 3
# ekf2
param set-default EKF2_AID_MASK 33
param set-default EKF2_TERR_MASK 1
param set-default EKF2_BARO_DELAY 0
param set-default EKF2_BARO_NOISE 2.0
@@ -173,7 +174,7 @@ param set-default RC1_TRIM 1000
param set-default SENS_FLOW_MAXR 7.4
param set-default SENS_FLOW_MINHGT 0.15
param set-default SENS_FLOW_MAXHGT 5.0
param set-default SENS_FLOW_ROT 0
param set-default SENS_FLOW_ROT 0
# ignore the SD card errors and use normal startup sound
set STARTUP_TUNE "1"
+3 -14
View File
@@ -21,7 +21,6 @@ set +e
# it wastes flash
#
set R /
set AUTOCNF no
set FCONFIG /fs/microsd/etc/config.txt
set FEXTRAS /fs/microsd/etc/extras.txt
set FRC /fs/microsd/etc/rc.txt
@@ -177,13 +176,12 @@ else
fi
#
# Set AUTOCNF flag to use it in AUTOSTART scripts.
# If the airframe has been previously reset SYS_AUTCONFIG will have been set to 1 and other params will be reset on the next boot.
#
if param greater SYS_AUTOCONFIG 0
then
# Wipe out params except RC*, flight modes, total flight time, calibration parameters, next flight UUID
param reset_all SYS_AUTO* RC* COM_FLTMODE* LND_FLIGHT* TC_* CAL_ACC* CAL_GYRO* COM_FLIGHT*
set AUTOCNF yes
# Reset params except Airframe, RC calibration, sensor calibration, flight modes, total flight time, and next flight UUID.
param reset_all SYS_AUTOSTART RC* CAL_* COM_FLTMODE* LND_FLIGHT* TC_* COM_FLIGHT*
fi
#
@@ -274,14 +272,6 @@ else
. $FCONFIG
fi
#
# If autoconfig parameter was set, reset it and save parameters.
#
if [ $AUTOCNF = yes ]
then
param set SYS_AUTOCONFIG 0
fi
#
# Check if UAVCAN is enabled, default to it for ESCs.
#
@@ -565,7 +555,6 @@ fi
# Unset all script parameters to free RAM.
#
unset R
unset AUTOCNF
unset FCONFIG
unset FEXTRAS
unset FRC
+1 -1
View File
@@ -95,7 +95,7 @@ def do_nsh_cmd(port_url, baudrate, cmd):
timeout_start = time.monotonic()
timeout = 240 # 4 minutes
timeout = 600 # 10 minutes
return_code = 0
+18 -12
View File
@@ -11,7 +11,7 @@ from pyulog import ULog
from analysis.detectors import InAirDetector, PreconditionError
from analysis.metrics import calculate_ecl_ekf_metrics
from analysis.checks import perform_ecl_ekf_checks
from analysis.post_processing import get_estimator_check_flags
from analysis.post_processing import get_gps_check_fail_flags
def analyse_ekf(
ulog: ULog, check_levels: Dict[str, float], multi_instance: int = 0,
@@ -40,6 +40,11 @@ def analyse_ekf(
except:
raise PreconditionError('could not find estimator_status instance', multi_instance)
try:
estimator_status_flags = ulog.get_dataset('estimator_status_flags', multi_instance).data
except:
raise PreconditionError('could not find estimator_status_flags instance', multi_instance)
try:
_ = ulog.get_dataset('estimator_innovations', multi_instance).data
except:
@@ -61,14 +66,14 @@ def analyse_ekf(
'in_air_transition_time': round(in_air.take_off + in_air.log_start, 2),
'on_ground_transition_time': round(in_air.landing + in_air.log_start, 2)}
control_mode, innov_flags, gps_fail_flags = get_estimator_check_flags(estimator_status)
gps_fail_flags = get_gps_check_fail_flags(estimator_status)
sensor_checks, innov_fail_checks = find_checks_that_apply(
control_mode, estimator_status,
estimator_status_flags, estimator_status,
pos_checks_when_sensors_not_fused=pos_checks_when_sensors_not_fused)
metrics = calculate_ecl_ekf_metrics(
ulog, innov_flags, innov_fail_checks, sensor_checks, in_air, in_air_no_ground_effects,
ulog, estimator_status_flags, innov_fail_checks, sensor_checks, in_air, in_air_no_ground_effects,
multi_instance, red_thresh=red_thresh, amb_thresh=amb_thresh)
check_status, master_status = perform_ecl_ekf_checks(
@@ -78,12 +83,12 @@ def analyse_ekf(
def find_checks_that_apply(
control_mode: dict, estimator_status: dict, pos_checks_when_sensors_not_fused: bool = False) ->\
estimator_status_flags: dict, estimator_status: dict, pos_checks_when_sensors_not_fused: bool = False) ->\
Tuple[List[str], List[str]]:
"""
finds the checks that apply and stores them in lists for the std checks and the innovation
fail checks.
:param control_mode:
:param estimator_status_flags:
:param estimator_status:
:param b_pos_only_when_sensors_fused:
:return: a tuple of two lists that contain strings for the std checks and for the innovation
@@ -97,7 +102,7 @@ def find_checks_that_apply(
innov_fail_checks.append('posv')
# Magnetometer Sensor Checks
if (np.amax(control_mode['yaw_aligned']) > 0.5):
if (np.amax(estimator_status_flags['cs_yaw_align']) > 0.5):
sensor_checks.append('mag')
innov_fail_checks.append('magx')
@@ -106,13 +111,14 @@ def find_checks_that_apply(
innov_fail_checks.append('yaw')
# Velocity Sensor Checks
if (np.amax(control_mode['using_gps']) > 0.5):
if (np.amax(estimator_status_flags['cs_gps']) > 0.5):
sensor_checks.append('vel')
innov_fail_checks.append('vel')
innov_fail_checks.append('velh')
innov_fail_checks.append('velv')
# Position Sensor Checks
if (pos_checks_when_sensors_not_fused or (np.amax(control_mode['using_gps']) > 0.5)
or (np.amax(control_mode['using_evpos']) > 0.5)):
if (pos_checks_when_sensors_not_fused or (np.amax(estimator_status_flags['cs_gps']) > 0.5)
or (np.amax(estimator_status_flags['cs_ev_pos']) > 0.5)):
sensor_checks.append('pos')
innov_fail_checks.append('posh')
@@ -128,7 +134,7 @@ def find_checks_that_apply(
innov_fail_checks.append('hagl')
# optical flow sensor checks
if (np.amax(control_mode['using_optflow']) > 0.5):
if (np.amax(estimator_status_flags['cs_opt_flow']) > 0.5):
innov_fail_checks.append('ofx')
innov_fail_checks.append('ofy')
+2 -1
View File
@@ -123,7 +123,8 @@ def perform_sensor_innov_checks(
('magy', 'magy_fail_percentage', 'mag'),
('magz', 'magz_fail_percentage', 'mag'),
('yaw', 'yaw_fail_percentage', 'yaw'),
('vel', 'vel_fail_percentage', 'vel'),
('velh', 'vel_fail_percentage', 'vel'),
('velv', 'vel_fail_percentage', 'vel'),
('posh', 'pos_fail_percentage', 'pos'),
('tas', 'tas_fail_percentage', 'tas'),
('hagl', 'hagl_fail_percentage', 'hagl'),
+18 -17
View File
@@ -11,7 +11,7 @@ import numpy as np
from analysis.detectors import InAirDetector
def calculate_ecl_ekf_metrics(
ulog: ULog, innov_flags: Dict[str, float], innov_fail_checks: List[str],
ulog: ULog, estimator_status_flags: Dict[str, float], innov_fail_checks: List[str],
sensor_checks: List[str], in_air: InAirDetector, in_air_no_ground_effects: InAirDetector,
multi_instance: int = 0, red_thresh: float = 1.0, amb_thresh: float = 0.5) -> Tuple[dict, dict, dict, dict]:
@@ -20,7 +20,7 @@ def calculate_ecl_ekf_metrics(
red_thresh=red_thresh, amb_thresh=amb_thresh)
innov_fail_metrics = calculate_innov_fail_metrics(
innov_flags, innov_fail_checks, in_air, in_air_no_ground_effects)
estimator_status_flags, innov_fail_checks, in_air, in_air_no_ground_effects)
imu_metrics = calculate_imu_metrics(ulog, multi_instance, in_air_no_ground_effects)
@@ -90,10 +90,10 @@ def calculate_sensor_metrics(
def calculate_innov_fail_metrics(
innov_flags: dict, innov_fail_checks: List[str], in_air: InAirDetector,
estimator_status_flags: dict, innov_fail_checks: List[str], in_air: InAirDetector,
in_air_no_ground_effects: InAirDetector) -> dict:
"""
:param innov_flags:
:param estimator_status_flags:
:param innov_fail_checks:
:param in_air:
:param in_air_no_ground_effects:
@@ -103,17 +103,18 @@ def calculate_innov_fail_metrics(
innov_fail_metrics = dict()
# calculate innovation check fail metrics
for signal_id, signal, result in [('posv', 'posv_innov_fail', 'hgt_fail_percentage'),
('magx', 'magx_innov_fail', 'magx_fail_percentage'),
('magy', 'magy_innov_fail', 'magy_fail_percentage'),
('magz', 'magz_innov_fail', 'magz_fail_percentage'),
('yaw', 'yaw_innov_fail', 'yaw_fail_percentage'),
('vel', 'vel_innov_fail', 'vel_fail_percentage'),
('posh', 'posh_innov_fail', 'pos_fail_percentage'),
('tas', 'tas_innov_fail', 'tas_fail_percentage'),
('hagl', 'hagl_innov_fail', 'hagl_fail_percentage'),
('ofx', 'ofx_innov_fail', 'ofx_fail_percentage'),
('ofy', 'ofy_innov_fail', 'ofy_fail_percentage')]:
for signal_id, signal, result in [('posv', 'reject_ver_pos', 'hgt_fail_percentage'),
('magx', 'reject_mag_x', 'magx_fail_percentage'),
('magy', 'reject_mag_y', 'magy_fail_percentage'),
('magz', 'reject_mag_z', 'magz_fail_percentage'),
('yaw', 'reject_yaw', 'yaw_fail_percentage'),
('velh', 'reject_hor_vel', 'vel_fail_percentage'),
('velv', 'reject_ver_vel', 'vel_fail_percentage'),
('posh', 'reject_hor_pos', 'pos_fail_percentage'),
('tas', 'reject_airspeed', 'tas_fail_percentage'),
('hagl', 'reject_hagl', 'hagl_fail_percentage'),
('ofx', 'reject_optflow_x', 'ofx_fail_percentage'),
('ofy', 'reject_optflow_y', 'ofy_fail_percentage')]:
# only run innov fail checks, if they apply.
if signal_id in innov_fail_checks:
@@ -125,7 +126,7 @@ def calculate_innov_fail_metrics(
in_air_detector = in_air
innov_fail_metrics[result] = calculate_stat_from_signal(
innov_flags, 'estimator_status', signal, in_air_detector,
estimator_status_flags, 'estimator_status_flags', signal, in_air_detector,
lambda x: 100.0 * np.mean(x > 0.5))
return innov_fail_metrics
@@ -152,7 +153,7 @@ def calculate_imu_metrics(ulog: ULog, multi_instance, in_air_no_ground_effects:
if vehicle_imu_status_data['accel_device_id'][0] == estimator_status_data['accel_device_id'][0]:
for signal, result in [('delta_angle_coning_metric', 'imu_coning'),
for signal, result in [('gyro_coning_vibration', 'imu_coning'),
('gyro_vibration_metric', 'imu_hfgyro'),
('accel_vibration_metric', 'imu_hfaccel')]:
-109
View File
@@ -7,115 +7,6 @@ from typing import Tuple
import numpy as np
def get_estimator_check_flags(estimator_status: dict) -> Tuple[dict, dict, dict]:
"""
:param estimator_status:
:return:
"""
control_mode = get_control_mode_flags(estimator_status)
innov_flags = get_innovation_check_flags(estimator_status)
gps_fail_flags = get_gps_check_fail_flags(estimator_status)
return control_mode, innov_flags, gps_fail_flags
def get_control_mode_flags(estimator_status: dict) -> dict:
"""
:param estimator_status:
:return:
"""
control_mode = dict()
# extract control mode metadata from estimator_status.control_mode_flags
# 0 - true if the filter tilt alignment is complete
# 1 - true if the filter yaw alignment is complete
# 2 - true if GPS measurements are being fused
# 3 - true if optical flow measurements are being fused
# 4 - true if a simple magnetic yaw heading is being fused
# 5 - true if 3-axis magnetometer measurement are being fused
# 6 - true if synthetic magnetic declination measurements are being fused
# 7 - true when the vehicle is airborne
# 8 - true when wind velocity is being estimated
# 9 - true when baro height is being fused as a primary height reference
# 10 - true when range finder height is being fused as a primary height reference
# 11 - true when range finder height is being fused as a primary height reference
# 12 - true when local position data from external vision is being fused
# 13 - true when yaw data from external vision measurements is being fused
# 14 - true when height data from external vision measurements is being fused
# 15 - true when synthetic sideslip measurements are being fused
# 16 - true true when the mag field does not match the expected strength
# 17 - true true when the vehicle is operating as a fixed wing vehicle
# 18 - true when the magnetometer has been declared faulty and is no longer being used
# 19 - true true when airspeed measurements are being fused
# 20 - true true when protection from ground effect induced static pressure rise is active
# 21 - true when rng data wasn't ready for more than 10s and new rng values haven't changed enough
# 22 - true when yaw (not ground course) data from a GPS receiver is being fused
# 23 - true when the in-flight mag field alignment has been completed
# 24 - true when local earth frame velocity data from external vision measurements are being fused
# 25 - true when we are using a synthesized measurement for the magnetometer Z component
control_mode['tilt_aligned'] = ((2 ** 0 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['yaw_aligned'] = ((2 ** 1 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_gps'] = ((2 ** 2 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_optflow'] = ((2 ** 3 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_magyaw'] = ((2 ** 4 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_mag3d'] = ((2 ** 5 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_magdecl'] = ((2 ** 6 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['airborne'] = ((2 ** 7 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['estimating_wind'] = ((2 ** 8 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_barohgt'] = ((2 ** 9 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_rnghgt'] = ((2 ** 10 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_gpshgt'] = ((2 ** 11 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_evpos'] = ((2 ** 12 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_evyaw'] = ((2 ** 13 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['using_evhgt'] = ((2 ** 14 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['fuse_beta'] = ((2 ** 15 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['mag_field_disturbed'] = ((2 ** 16 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['fixed_wing'] = ((2 ** 17 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['mag_fault'] = ((2 ** 18 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['fuse_aspd'] = ((2 ** 19 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['gnd_effect'] = ((2 ** 20 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['rng_stuck'] = ((2 ** 21 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['gps_yaw'] = ((2 ** 22 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['mag_aligned_in_flight'] = ((2 ** 23 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['ev_vel'] = ((2 ** 24 & estimator_status['control_mode_flags']) > 0) * 1
control_mode['synthetic_mag_z'] = ((2 ** 25 & estimator_status['control_mode_flags']) > 0) * 1
return control_mode
def get_innovation_check_flags(estimator_status: dict) -> dict:
"""
:param estimator_status:
:return:
"""
innov_flags = dict()
# innovation_check_flags summary
# 0 - true if velocity observations have been rejected
# 1 - true if horizontal position observations have been rejected
# 2 - true if true if vertical position observations have been rejected
# 3 - true if the X magnetometer observation has been rejected
# 4 - true if the Y magnetometer observation has been rejected
# 5 - true if the Z magnetometer observation has been rejected
# 6 - true if the yaw observation has been rejected
# 7 - true if the airspeed observation has been rejected
# 8 - true if synthetic sideslip observation has been rejected
# 9 - true if the height above ground observation has been rejected
# 10 - true if the X optical flow observation has been rejected
# 11 - true if the Y optical flow observation has been rejected
innov_flags['vel_innov_fail'] = ((2 ** 0 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['posh_innov_fail'] = ((2 ** 1 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['posv_innov_fail'] = ((2 ** 2 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['magx_innov_fail'] = ((2 ** 3 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['magy_innov_fail'] = ((2 ** 4 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['magz_innov_fail'] = ((2 ** 5 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['yaw_innov_fail'] = ((2 ** 6 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['tas_innov_fail'] = ((2 ** 7 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['sli_innov_fail'] = ((2 ** 8 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['hagl_innov_fail'] = ((2 ** 9 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['ofx_innov_fail'] = ((2 ** 10 & estimator_status['innovation_check_flags']) > 0) * 1
innov_flags['ofy_innov_fail'] = ((2 ** 11 & estimator_status['innovation_check_flags']) > 0) * 1
return innov_flags
def get_gps_check_fail_flags(estimator_status: dict) -> dict:
"""
:param estimator_status:
+34 -28
View File
@@ -11,7 +11,7 @@ import numpy as np
from matplotlib.backends.backend_pdf import PdfPages
from pyulog import ULog
from analysis.post_processing import magnetic_field_estimates_from_states, get_estimator_check_flags
from analysis.post_processing import magnetic_field_estimates_from_states, get_gps_check_fail_flags
from plotting.data_plots import TimeSeriesPlot, InnovationPlot, ControlModeSummaryPlot, \
CheckFlagsPlot
from analysis.detectors import PreconditionError
@@ -33,6 +33,11 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
except:
raise PreconditionError('could not find estimator_status instance', multi_instance)
try:
estimator_status_flags = ulog.get_dataset('estimator_status_flags', multi_instance).data
except:
raise PreconditionError('could not find estimator_status_flags instance', multi_instance)
try:
estimator_states = ulog.get_dataset('estimator_states', multi_instance).data
except:
@@ -68,12 +73,13 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
except:
raise PreconditionError('could not find innovation data')
control_mode, innov_flags, gps_fail_flags = get_estimator_check_flags(estimator_status)
gps_fail_flags = get_gps_check_fail_flags(estimator_status)
status_time = 1e-6 * estimator_status['timestamp']
status_flags_time = 1e-6 * estimator_status_flags['timestamp']
b_finishes_in_air, b_starts_in_air, in_air_duration, in_air_transition_time, \
on_ground_transition_time = detect_airtime(control_mode, status_time)
on_ground_transition_time = detect_airtime(estimator_status_flags, status_flags_time)
with PdfPages(output_plot_filename) as pdf_pages:
@@ -173,9 +179,9 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
# plot control mode summary A
data_plot = ControlModeSummaryPlot(
status_time, control_mode, [['tilt_aligned', 'yaw_aligned'],
['using_gps', 'using_optflow', 'using_evpos'], ['using_barohgt', 'using_gpshgt',
'using_rnghgt', 'using_evhgt'], ['using_magyaw', 'using_mag3d', 'using_magdecl']],
status_flags_time, estimator_status_flags, [['cs_tilt_align', 'cs_yaw_align'],
['cs_gps', 'cs_opt_flow', 'cs_ev_pos'], ['cs_baro_hgt', 'cs_gps_hgt',
'cs_rng_hgt', 'cs_ev_hgt'], ['cs_mag_hdg', 'cs_mag_3d', 'cs_mag_dec']],
x_label='time (sec)', y_labels=['aligned', 'pos aiding', 'hgt aiding', 'mag aiding'],
annotation_text=[['tilt alignment', 'yaw alignment'], ['GPS aiding', 'optical flow aiding',
'external vision aiding'], ['Baro aiding', 'GPS aiding', 'rangefinder aiding',
@@ -188,7 +194,7 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
# plot control mode summary B
# construct additional annotations for the airborne plot
airborne_annotations = list()
if np.amin(np.diff(control_mode['airborne'])) > -0.5:
if np.amin(np.diff(estimator_status_flags['cs_in_air'])) > -0.5:
airborne_annotations.append(
(on_ground_transition_time, 'air to ground transition not detected'))
else:
@@ -197,7 +203,7 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
if in_air_duration > 0.0:
airborne_annotations.append(((in_air_transition_time + on_ground_transition_time) / 2,
'duration = {:.1f} sec'.format(in_air_duration)))
if np.amax(np.diff(control_mode['airborne'])) < 0.5:
if np.amax(np.diff(estimator_status_flags['cs_in_air'])) < 0.5:
airborne_annotations.append(
(in_air_transition_time, 'ground to air transition not detected'))
else:
@@ -205,7 +211,7 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
(in_air_transition_time, 'in-air at {:.1f} sec'.format(in_air_transition_time)))
data_plot = ControlModeSummaryPlot(
status_time, control_mode, [['airborne'], ['estimating_wind']],
status_flags_time, estimator_status_flags, [['cs_in_air'], ['cs_wind']],
x_label='time (sec)', y_labels=['airborne', 'estimating wind'], annotation_text=[[], []],
additional_annotation=[airborne_annotations, []],
plot_title='EKF Control Status - Figure B', pdf_handle=pdf_pages)
@@ -214,15 +220,15 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
# plot innovation_check_flags summary
data_plot = CheckFlagsPlot(
status_time, innov_flags, [['vel_innov_fail', 'posh_innov_fail'], ['posv_innov_fail',
'hagl_innov_fail'],
['magx_innov_fail', 'magy_innov_fail', 'magz_innov_fail',
'yaw_innov_fail'], ['tas_innov_fail'], ['sli_innov_fail'],
['ofx_innov_fail',
'ofy_innov_fail']], x_label='time (sec)',
status_flags_time, estimator_status_flags, [['reject_hor_vel', 'reject_hor_pos'], ['reject_ver_vel', 'reject_ver_pos',
'reject_hagl'],
['reject_mag_x', 'reject_mag_y', 'reject_mag_z',
'reject_yaw'], ['reject_airspeed'], ['reject_sideslip'],
['reject_optflow_x',
'reject_optflow_y']], x_label='time (sec)',
y_labels=['failed', 'failed', 'failed', 'failed', 'failed', 'failed'],
y_lim=(-0.1, 1.1),
legend=[['vel NED', 'pos NE'], ['hgt absolute', 'hgt above ground'],
legend=[['vel NE', 'pos NE'], ['vel D', 'hgt absolute', 'hgt above ground'],
['mag_x', 'mag_y', 'mag_z', 'yaw'], ['airspeed'], ['sideslip'],
['flow X', 'flow Y']],
plot_title='EKF Innovation Test Fails', annotate=False, pdf_handle=pdf_pages)
@@ -344,33 +350,33 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
data_plot.close()
def detect_airtime(control_mode, status_time):
def detect_airtime(estimator_status_flags, status_flags_time):
# define flags for starting and finishing in air
b_starts_in_air = False
b_finishes_in_air = False
# calculate in-air transition time
if (np.amin(control_mode['airborne']) < 0.5) and (np.amax(control_mode['airborne']) > 0.5):
in_air_transtion_time_arg = np.argmax(np.diff(control_mode['airborne']))
in_air_transition_time = status_time[in_air_transtion_time_arg]
elif (np.amax(control_mode['airborne']) > 0.5):
in_air_transition_time = np.amin(status_time)
if (np.amin(estimator_status_flags['cs_in_air']) < 0.5) and (np.amax(estimator_status_flags['cs_in_air']) > 0.5):
in_air_transtion_time_arg = np.argmax(np.diff(estimator_status_flags['cs_in_air']))
in_air_transition_time = status_flags_time[in_air_transtion_time_arg]
elif (np.amax(estimator_status_flags['cs_in_air']) > 0.5):
in_air_transition_time = np.amin(status_flags_time)
print('log starts while in-air at ' + str(round(in_air_transition_time, 1)) + ' sec')
b_starts_in_air = True
else:
in_air_transition_time = float('NaN')
print('always on ground')
# calculate on-ground transition time
if (np.amin(np.diff(control_mode['airborne'])) < 0.0):
on_ground_transition_time_arg = np.argmin(np.diff(control_mode['airborne']))
on_ground_transition_time = status_time[on_ground_transition_time_arg]
elif (np.amax(control_mode['airborne']) > 0.5):
on_ground_transition_time = np.amax(status_time)
if (np.amin(np.diff(estimator_status_flags['cs_in_air'])) < 0.0):
on_ground_transition_time_arg = np.argmin(np.diff(estimator_status_flags['cs_in_air']))
on_ground_transition_time = status_flags_time[on_ground_transition_time_arg]
elif (np.amax(estimator_status_flags['cs_in_air']) > 0.5):
on_ground_transition_time = np.amax(status_flags_time)
print('log finishes while in-air at ' + str(round(on_ground_transition_time, 1)) + ' sec')
b_finishes_in_air = True
else:
on_ground_transition_time = float('NaN')
print('always on ground')
if (np.amax(np.diff(control_mode['airborne'])) > 0.5) and (np.amin(np.diff(control_mode['airborne'])) < -0.5):
if (np.amax(np.diff(estimator_status_flags['cs_in_air'])) > 0.5) and (np.amin(np.diff(estimator_status_flags['cs_in_air'])) < -0.5):
if ((on_ground_transition_time - in_air_transition_time) > 0.0):
in_air_duration = on_ground_transition_time - in_air_transition_time
else:
+12 -4
View File
@@ -5,12 +5,13 @@ set -e
SCRIPT_DIR="$( cd "$( dirname "${BASH_SOURCE[0]}" )" && pwd )"
cd "$SCRIPT_DIR/jMAVSim"
tcp_port=4560
port=4560
extra_args=
baudrate=921600
device=
ip="127.0.0.1"
while getopts ":b:d:p:qsr:f:i:loat" opt; do
protocol="tcp"
while getopts ":b:d:u:p:qsr:f:i:loat" opt; do
case $opt in
b)
baudrate=$OPTARG
@@ -18,11 +19,14 @@ while getopts ":b:d:p:qsr:f:i:loat" opt; do
d)
device="$OPTARG"
;;
u)
protocol="udp"
;;
i)
ip="$OPTARG"
;;
p)
tcp_port=$OPTARG
port=$OPTARG
;;
q)
extra_args="$extra_args -qgc"
@@ -53,7 +57,11 @@ while getopts ":b:d:p:qsr:f:i:loat" opt; do
done
if [ "$device" == "" ]; then
device="-tcp $ip:$tcp_port"
if [ "$protocol" == "tcp" ]; then
device="-tcp $ip:$port"
else
device="-udp $port"
fi
else
device="-serial $device $baudrate"
fi
-72
View File
@@ -1,72 +0,0 @@
#!/bin/python3
import parse_cmake.parsing as cmp
import glob
import pprint
import re
import os
__location__ = os.path.realpath(
os.path.join(os.getcwd(), os.path.dirname(__file__)))
serial_regex = r"(\D\D\D\d):(/dev/ttyS\d+)"
io_regex = r"IO (.*)"
romfs_regex = r"ROMFSROOT (.*)"
arch_regex = r"ARCHITECTURE (.*)"
toolchain_regex = r"TOOLCHAIN (.*)"
def stripComments(code):
code = str(code)
return re.sub(r'(?m) *#.*\n?', '', code)
lut = {}
with open(os.path.join(__location__, "cmake_kconfig_lut.txt"),'r') as lookup:
for line in lookup:
if ',' in line:
key, value = line.strip().split(',')
lut[key] = value
#for name in glob.glob('boards/*/*/*.cmake'):
px4_dir = os.path.abspath(os.path.join(os.path.dirname(__file__), '../../'))
for name in glob.glob(px4_dir + '/boards/*/*/*.cmake'):
print(name)
with open(name, 'r') as f:
romfs_set = False
w = open(name.replace(".cmake",".px4board"), "w")
for line in f:
clean_line = stripComments(line.strip())
value = lut.get(clean_line)
if value is not None:
print(value, file=w)
print(value)
else:
matches = re.finditer(serial_regex, clean_line, re.MULTILINE)
for matchNum, match in enumerate(matches, start=1):
print("CONFIG_BOARD_SERIAL_" + match.groups()[0] + "=\"" + match.groups()[1] + "\"")
print("CONFIG_BOARD_SERIAL_" + match.groups()[0] + "=\"" + match.groups()[1] + "\"", file=w)
matches = re.finditer(io_regex, clean_line, re.MULTILINE)
for matchNum, match in enumerate(matches, start=1):
print("CONFIG_BOARD_IO=\"" + match.groups()[0] + "\"")
print("CONFIG_BOARD_IO=\"" + match.groups()[0] + "\"", file=w)
matches = re.finditer(romfs_regex, clean_line, re.MULTILINE)
for matchNum, match in enumerate(matches, start=1):
print("CONFIG_BOARD_ROMFSROOT=\"" + match.groups()[0] + "\"")
print("CONFIG_BOARD_ROMFSROOT=\"" + match.groups()[0] + "\"", file=w)
romfs_set = True
matches = re.finditer(arch_regex, clean_line, re.MULTILINE)
for matchNum, match in enumerate(matches, start=1):
print("CONFIG_BOARD_ARCHITECTURE=\"" + match.groups()[0] + "\"")
print("CONFIG_BOARD_ARCHITECTURE=\"" + match.groups()[0] + "\"", file=w)
matches = re.finditer(toolchain_regex, clean_line, re.MULTILINE)
for matchNum, match in enumerate(matches, start=1):
print("CONFIG_BOARD_TOOLCHAIN=\"" + match.groups()[0] + "\"")
print("CONFIG_BOARD_TOOLCHAIN=\"" + match.groups()[0] + "\"", file=w)
if(romfs_set == False):
print("CONFIG_BOARD_ROMFSROOT=\"\"", file=w)
w.close()
-204
View File
@@ -1,204 +0,0 @@
PLATFORM nuttx,CONFIG_PLATFORM_NUTTX=y
PLATFORM posix,CONFIG_PLATFORM_POSIX=y
CONSTRAINED_MEMORY,CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONSTRAINED_FLASH,CONFIG_BOARD_CONSTRAINED_FLASH=y
NO_HELP,CONFIG_BOARD_NO_HELP=y
EXTERNAL_METADATA,CONFIG_BOARD_EXTERNAL_METADATA=y
BUILD_BOOTLOADER,CONFIG_BOARD_BUILD_BOOTLOADER=y
UAVCAN_INTERFACES 2,CONFIG_BOARD_UAVCAN_INTERFACES=2
UAVCAN_INTERFACES 1,CONFIG_BOARD_UAVCAN_INTERFACES=1
UAVCAN_TIMER_OVERRIDE 2,CONFIG_BOARD_UAVCAN_TIMER_OVERRIDE=2
UAVCAN_TIMER_OVERRIDE 1,CONFIG_BOARD_UAVCAN_TIMER_OVERRIDE=1
UAVCAN_TIMER_OVERRIDE 1,CONFIG_BOARD_UAVCAN_TIMER_OVERRIDE=0
TESTING,CONFIG_BOARD_TESTING=y
ETHERNET,CONFIG_BOARD_ETHERNET=y
adc/ads1115,CONFIG_DRIVERS_ADC_ADS1115=y
adc/board_adc,CONFIG_DRIVERS_ADC_BOARD_ADC=y
barometer,CONFIG_COMMON_BAROMETERS=y
barometer/bmp280,CONFIG_DRIVERS_BAROMETER_BMP280=y
barometer/bmp388,CONFIG_DRIVERS_BAROMETER_BMP388=y
barometer/dps310,CONFIG_DRIVERS_BAROMETER_DPS310=y
barometer/lps22hb,CONFIG_DRIVERS_BAROMETER_LPS22HB=y
barometer/lps25h,CONFIG_DRIVERS_BAROMETER_LPS25H=y
barometer/lps33hw,CONFIG_DRIVERS_BAROMETER_LPS33HW=y
barometer/mpl3115a2,CONFIG_DRIVERS_BAROMETER_MPL3115A2=y
barometer/ms5611,CONFIG_DRIVERS_BAROMETER_MS5611=y
barometer/tcbp001ta,CONFIG_DRIVERS_BAROMETER_TCBP001TA=y
batt_smbus,CONFIG_DRIVERS_BATT_SMBUS=y
bootloaders,CONFIG_DRIVERS_BOOTLOADERS=y
camera_capture,CONFIG_DRIVERS_CAMERA_CAPTURE=y
camera_trigger,CONFIG_DRIVERS_CAMERA_TRIGGER=y
differential_pressure,CONFIG_DRIVERS_DIFFERENTIAL_PRESSURE=y
distance_sensor,CONFIG_COMMON_DISTANCE_SENSOR=y
distance_sensor/ll40ls,CONFIG_DRIVERS_DISTANCE_SENSOR_LL40LS=y
distance_sensor/lightware_laser_serial,CONFIG_DRIVERS_DISTANCE_SENSOR_LIGHTWARE_LASER_SERIAL=y
distance_sensor/broadcom/afbrs50,CONFIG_DRIVERS_DISTANCE_SENSOR_BROADCOM_AFBRS50=y
distance_sensor/vl53l0x,CONFIG_DRIVERS_DISTANCE_SENSOR_VL53L0X=y
distance_sensor/vl53l1x,CONFIG_DRIVERS_DISTANCE_SENSOR_VL53L1X=y
distance_sensor/srf05,CONFIG_DRIVERS_DISTANCE_SENSOR_SRF05=y
dshot,CONFIG_DRIVERS_DSHOT=y
gps,CONFIG_DRIVERS_GPS=y
heater,CONFIG_DRIVERS_HEATER=y
imu,CONFIG_COMMON_IMU=y
imu/adis16477,CONFIG_DRIVERS_IMU_ADIS16477=y
imu/adis16497,CONFIG_DRIVERS_IMU_ADIS16497=y
imu/analog_devices/adis16448,CONFIG_DRIVERS_IMU_ANALOG_DEVICES_ADIS16448=y
imu/analog_devices/adis16470,CONFIG_DRIVERS_IMU_ANALOG_DEVICES_ADIS16470=y
imu/bosch/bmi055,CONFIG_DRIVERS_IMU_BOSCH_BMI055=y
imu/bosch/bmi088,CONFIG_DRIVERS_IMU_BOSCH_BMI088=y
imu/fxas21002c,CONFIG_DRIVERS_IMU_FXAS21002C=y
imu/fxos8701cq,CONFIG_DRIVERS_IMU_FXOS8701CQ=y
imu/invensense/icm20602,CONFIG_DRIVERS_IMU_INVENSENSE_ICM20602=y
imu/invensense/icm20608g,CONFIG_DRIVERS_IMU_INVENSENSE_ICM20608G=y
imu/invensense/icm20649,CONFIG_DRIVERS_IMU_INVENSENSE_ICM20649=y
imu/invensense/icm20689,CONFIG_DRIVERS_IMU_INVENSENSE_ICM20689=y
imu/invensense/icm20948,CONFIG_DRIVERS_IMU_INVENSENSE_ICM20948=y
imu/invensense/icm40609d,CONFIG_DRIVERS_IMU_INVENSENSE_ICM40609D=y
imu/invensense/icm42605,CONFIG_DRIVERS_IMU_INVENSENSE_ICM42605=y
imu/invensense/icm42688p,CONFIG_DRIVERS_IMU_INVENSENSE_ICM42688P=y
imu/invensense/mpu6000,CONFIG_DRIVERS_IMU_INVENSENSE_MPU6000=y
imu/invensense/mpu6500,CONFIG_DRIVERS_IMU_INVENSENSE_MPU6500=y
imu/invensense/mpu9250,CONFIG_DRIVERS_IMU_INVENSENSE_MPU9250=y
imu/l3gd20,CONFIG_DRIVERS_IMU_L3GD20=y
imu/lsm303d,CONFIG_DRIVERS_IMU_LSM303D=y
imu/st,CONFIG_DRIVERS_IMU_ST=y
irlock,CONFIG_DRIVERS_IRLOCK=y
lights,CONFIG_COMMON_LIGHT=y
lights/neopixel,CONFIG_DRIVERS_LIGHTS_NEOPIXEL=y
lights/rgbled,CONFIG_DRIVERS_LIGHTS_RGBLED=y
lights/rgbled_ncp5623c,CONFIG_DRIVERS_LIGHTS_RGBLED_NCP5623C=y
lights/rgbled_pwm,CONFIG_DRIVERS_LIGHTS_RGBLED_PWM=y
magnetometer,CONFIG_COMMON_MAGNETOMETER=y
magnetometer/akm/ak09916,CONFIG_DRIVERS_MAGNETOMETER_AKM_AK09916=y
magnetometer/akm/ak8963,CONFIG_DRIVERS_MAGNETOMETER_AKM_AK8963=y
magnetometer/bosch/bmm150,CONFIG_DRIVERS_MAGNETOMETER_BOSCH_BMM150=y
magnetometer/hmc5883,CONFIG_DRIVERS_MAGNETOMETER_HMC5883=y
magnetometer/isentek/ist8308,CONFIG_DRIVERS_MAGNETOMETER_ISENTEK_IST8308=y
magnetometer/isentek/ist8310,CONFIG_DRIVERS_MAGNETOMETER_ISENTEK_IST8310=y
magnetometer/lis2mdl,CONFIG_DRIVERS_MAGNETOMETER_LIS2MDL=y
magnetometer/lis3mdl,CONFIG_DRIVERS_MAGNETOMETER_LIS3MDL=y
magnetometer/lsm303agr,CONFIG_DRIVERS_MAGNETOMETER_LSM303AGR=y
magnetometer/lsm9ds1_mag,CONFIG_DRIVERS_MAGNETOMETER_LSM9DS1_MAG=y
magnetometer/qmc5883l,CONFIG_DRIVERS_MAGNETOMETER_QMC5883L=y
magnetometer/rm3100,CONFIG_DRIVERS_MAGNETOMETER_RM3100=y
magnetometer/vtrantech/vcm1193l,CONFIG_DRIVERS_MAGNETOMETER_VTRANTECH_VCM1193L=y
optical_flow,CONFIG_COMMON_OPTICAL_FLOW=y
optical_flow/paw3902,CONFIG_DRIVERS_OPTICAL_FLOW_PAW3902=y
optical_flow/paw3901,CONFIG_DRIVERS_OPTICAL_FLOW_PMW3901=y
optical_flow/px4flow,CONFIG_DRIVERS_OPTICAL_FLOW_PX4FLOW=y
optical_flow/thoneflow,CONFIG_DRIVERS_OPTICAL_FLOW_THONEFLOW=y
osd,CONFIG_DRIVERS_OSD=y
pca9685,CONFIG_DRIVERS_PCA9685=y
pca9685_pwm_out,CONFIG_DRIVERS_PCA9685_PWM_OUT=y
power_monitor/ina226,CONFIG_DRIVERS_POWER_MONITOR_INA226=y
power_monitor/voxlpm,CONFIG_DRIVERS_POWER_MONITOR_VOXLPM=y
pps_capture,CONFIG_DRIVERS_PPS_CAPTURE=y
protocol_splitter,CONFIG_DRIVERS_PROTOCOL_SPLITTER=y
pwm_input,CONFIG_DRIVERS_PWM_INPUT=y
pwm_out_sim,CONFIG_DRIVERS_PWM_OUT_SIM=y
pwm_out,CONFIG_DRIVERS_PWM_OUT=y
px4io,CONFIG_DRIVERS_PX4IO=y
rc_input,CONFIG_DRIVERS_RC_INPUT=y
roboclaw,CONFIG_DRIVERS_ROBOCLAW=y
rpi_rc_in,CONFIG_DRIVERS_RPI_RC_IN=y
rpm,CONFIG_DRIVERS_RPM=y
safety_button,CONFIG_DRIVERS_SAFETY_BUTTON=y
smart_battery/batmon,CONFIG_DRIVERS_SMART_BATTERY_BATMON=y
spektrum_rc,CONFIG_DRIVERS_SPEKTRUM_RC=y
telemetry,CONFIG_DRIVERS_TELEMETRY=y
test_ppm,CONFIG_DRIVERS_TEST_PPM=y
tone_alarm,CONFIG_DRIVERS_TONE_ALARM=y
uavcan,CONFIG_DRIVERS_UAVCAN=y
uavcannode,CONFIG_DRIVERS_UAVCANNODE=y
uavcannode_gps_demo,CONFIG_DRIVERS_UAVCANNODE_GPS_DEMO=y
airship_att_control,CONFIG_MODULES_AIRSHIP_ATT_CONTROL=y
airspeed_selector,CONFIG_MODULES_AIRSPEED_SELECTOR=y
velocity_controller,CONFIG_MODULES_ANGULAR_VELOCITY_CONTROLLER=y
attitude_estimator_q,CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
battery_status,CONFIG_MODULES_BATTERY_STATUS=y
camera_feedback,CONFIG_MODULES_CAMERA_FEEDBACK=y
commander,CONFIG_MODULES_COMMANDER=y
control_allocator,CONFIG_MODULES_CONTROL_ALLOCATOR=y
dataman,CONFIG_MODULES_DATAMAN=y
ekf2,CONFIG_MODULES_EKF2=y
esc_battery,CONFIG_MODULES_ESC_BATTERY=y
events,CONFIG_MODULES_EVENTS=y
flight_mode_manager,CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
fw_att_control,CONFIG_MODULES_FW_ATT_CONTROL=y
fw_pos_control_l1,CONFIG_MODULES_FW_POS_CONTROL_L1=y
gyro_calibration,CONFIG_MODULES_GYRO_CALIBRATION=y
gyro_fft,CONFIG_MODULES_GYRO_FFT=y
land_detector,CONFIG_MODULES_LAND_DETECTOR=y
landing_target_estimator,CONFIG_MODULES_LANDING_TARGET_ESTIMATOR=y
load_mon,CONFIG_MODULES_LOAD_MON=y
local_position_estimator,CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=y
logger,CONFIG_MODULES_LOGGER=y
mavlink,CONFIG_MODULES_MAVLINK=y
mc_att_control,CONFIG_MODULES_MC_ATT_CONTROL=y
mc_hover_thrust_estimator,CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=y
mc_pos_control,CONFIG_MODULES_MC_POS_CONTROL=y
mc_rate_control,CONFIG_MODULES_MC_RATE_CONTROL=y
micrortps_bridge,CONFIG_MODULES_MICRORTPS_BRIDGE=y
microdds_client,CONFIG_MODULES_MICRODDS_CLIENT=y
navigator,CONFIG_MODULES_NAVIGATOR=y
px4iofirmware,CONFIG_MODULES_PX4IOFIRMWARE=y
rc_update,CONFIG_MODULES_RC_UPDATE=y
replay,CONFIG_MODULES_REPLAY=y
rover_pos_control,CONFIG_MODULES_ROVER_POS_CONTROL=y
sensors,CONFIG_MODULES_SENSORS=y
sih,CONFIG_MODULES_SIH=y
simulator,CONFIG_MODULES_SIMULATOR=y
temperature_compensation,CONFIG_MODULES_TEMPERATURE_COMPENSATION=y
uuv_att_control,CONFIG_MODULES_UUV_ATT_CONTROL=y
uuv_pos_control,CONFIG_MODULES_UUV_POS_CONTROL=y
gimbal,CONFIG_MODULES_GIMBAL=y
vtol_att_control,CONFIG_MODULES_VTOL_ATT_CONTROL=y
bl_update,CONFIG_SYSTEMCMDS_BL_UPDATE=y
dmesg,CONFIG_SYSTEMCMDS_DMESG=y
dumpfile,CONFIG_SYSTEMCMDS_DUMPFILE=y
dyn,CONFIG_SYSTEMCMDS_DYN=y
failure,CONFIG_SYSTEMCMDS_FAILURE=y
gpio,CONFIG_SYSTEMCMDS_GPIO=y
hardfault_log,CONFIG_SYSTEMCMDS_HARDFAULT_LOG=y
i2cdetect,CONFIG_SYSTEMCMDS_I2CDETECT=y
led_control,CONFIG_SYSTEMCMDS_LED_CONTROL=y
mft,CONFIG_SYSTEMCMDS_MFT=y
microbench,CONFIG_SYSTEMCMDS_MICROBENCH=y
mixer,CONFIG_SYSTEMCMDS_MIXER=y
motor_test,CONFIG_SYSTEMCMDS_MOTOR_TEST=y
mtd,CONFIG_SYSTEMCMDS_MTD=y
netman,CONFIG_SYSTEMCMDS_NETMAN=y
nshterm,CONFIG_SYSTEMCMDS_NSHTERM=y
param,CONFIG_SYSTEMCMDS_PARAM=y
perf,CONFIG_SYSTEMCMDS_PERF=y
pwm,CONFIG_SYSTEMCMDS_PWM=y
reboot,CONFIG_SYSTEMCMDS_REBOOT=y
reflect,CONFIG_SYSTEMCMDS_REFLECT=y
sd_bench,CONFIG_SYSTEMCMDS_SD_BENCH=y
serial_tet,CONFIG_SYSTEMCMDS_SERIAL_TEST=y
shutdown,CONFIG_SYSTEMCMDS_SHUTDOWN=y
system_time,CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
tests,CONFIG_SYSTEMCMDS_TESTS=y
top,CONFIG_SYSTEMCMDS_TOP=y
topic_listener,CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
tune_control,CONFIG_SYSTEMCMDS_TUNE_CONTROL=y
uorb,CONFIG_SYSTEMCMDS_UORB=y
usb_connected,CONFIG_SYSTEMCMDS_USB_CONNECTED=y
ver,CONFIG_SYSTEMCMDS_VER=y
work_queue,CONFIG_SYSTEMCMDS_WORK_QUEUE=y
dyn_hello,CONFIG_EXAMPLES_DYN_HELLO=y
fake_gps,CONFIG_EXAMPLES_FAKE_GPS=y
fake_gyro,CONFIG_EXAMPLES_FAKE_GYRO=y
fake_imu,CONFIG_EXAMPLES_FAKE_IMU=y
fake_magnetometer,CONFIG_EXAMPLES_FAKE_MAGNETOMETER=y
fixedwing_control,CONFIG_EXAMPLES_FIXEDWING_CONTROL=y
hello,CONFIG_EXAMPLES_HELLO=y
hwtest,CONFIG_EXAMPLES_HWTEST=y
matlab_csv_serial,CONFIG_EXAMPLES_MATLAB_CSV_SERIAL=y
px4_mavlink_debug,CONFIG_EXAMPLES_PX4_MAVLINK_DEBUG=y
px4_simple_app,CONFIG_EXAMPLES_PX4_SIMPLE_APP=y
rover_steering_control,CONFIG_EXAMPLES_ROVER_STEERING_CONTROL=y
uuv_example_app,CONFIG_EXAMPLES_UUV_EXAMPLE_APP=y
work_item,CONFIG_EXAMPLES_WORK_ITEM=y
add_compile_options(-Wno-narrowing),CONFIG_BOARD_COMPILE_DEFINITIONS="-Wno-narrowing"
-D__PX4_LINUX,CONFIG_BOARD_LINUX=y
+1 -1
View File
@@ -16,7 +16,7 @@ class ModuleDocumentation(object):
valid_categories = ['driver', 'estimator', 'controller', 'system',
'communication', 'command', 'template', 'simulation', 'autotune']
valid_subcategories = ['', 'distance_sensor', 'imu', 'airspeed_sensor',
'magnetometer', 'baro', 'optical_flow', 'rpm_sensor']
'magnetometer', 'baro', 'optical_flow', 'rpm_sensor', 'transponder']
max_line_length = 80 # wrap lines that are longer than this
+14 -5
View File
@@ -200,13 +200,12 @@ if [[ $INSTALL_SIM == "true" ]]; then
if [[ "${UBUNTU_RELEASE}" == "18.04" ]]; then
java_version=11
gazebo_version=9
elif [[ "${UBUNTU_RELEASE}" == "20.04" ]]; then
java_version=13
gazebo_version=11
elif [[ "${UBUNTU_RELEASE}" == "22.04" ]]; then
java_version=11
else
java_version=14
gazebo_version=11
fi
# Java (jmavsim or fastrtps)
sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
@@ -220,20 +219,30 @@ if [[ $INSTALL_SIM == "true" ]]; then
sudo update-alternatives --set java $(update-alternatives --list java | grep "java-$java_version")
# Gazebo
if [[ "${UBUNTU_RELEASE}" == "18.04" ]]; then
gazebo_version=9
gazebo_packages="gazebo$gazebo_version libgazebo$gazebo_version-dev"
elif [[ "${UBUNTU_RELEASE}" == "22.04" ]]; then
gazebo_packages="gazebo libgazebo-dev"
else
# default and Ubuntu 20.04
gazebo_version=11
gazebo_packages="gazebo$gazebo_version libgazebo$gazebo_version-dev"
fi
sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
wget http://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
# Update list, since new gazebo-stable.list has been added
sudo apt-get update -y --quiet
sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
dmidecode \
gazebo$gazebo_version \
$gazebo_packages \
gstreamer1.0-plugins-bad \
gstreamer1.0-plugins-base \
gstreamer1.0-plugins-good \
gstreamer1.0-plugins-ugly \
gstreamer1.0-libav \
libeigen3-dev \
libgazebo$gazebo_version-dev \
libgstreamer-plugins-base1.0-dev \
libimage-exiftool-perl \
libopencv-dev \
+9
View File
@@ -74,6 +74,9 @@ if [ "$model" == "" ] || [ "$model" == "none" ]; then
if [ "$program" == "jsbsim" ]; then
echo "empty model, setting rascal as default for jsbsim"
model="rascal"
elif [ "$program" == "sihsim" ]; then
echo "empty model, setting quadx as default for sihsim"
model="quadx"
else
echo "empty model, setting iris as default"
model="iris"
@@ -214,6 +217,12 @@ elif [ "$program" == "jsbsim" ] && [ -z "$no_sim" ]; then
fi
"${build_path}/build_jsbsim_bridge/jsbsim_bridge" ${model} -s "${src_path}/Tools/jsbsim_bridge/scene/${world}.xml" 2> /dev/null &
JSBSIM_PID=$!
elif [ "$program" == "sihsim" ] && [ ! -n "$no_sim" ]; then
export SIM_MODE="sihsim"
if [ "$model" != "airplane" ] && [ "$model" != "quadx" ] && [ "$model" != "xvert" ]; then
echo "Model ${model} not compatible with with sih. sih supports [quadx,airplane,xvert]."
exit 1
fi
fi
pushd "$rootfs" >/dev/null
@@ -130,8 +130,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDIO_BLOCKSETUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -174,7 +173,7 @@ CONFIG_STM32_SPI1=y
CONFIG_STM32_SPI2=y
CONFIG_STM32_SPI4=y
CONFIG_STM32_SPI4_DMA=y
CONFIG_STM32_SPI4_DMA_BUFFER=1024
CONFIG_STM32_SPI4_DMA_BUFFER=512
CONFIG_STM32_SPI_DMA=y
CONFIG_STM32_SPI_DMATHRESHOLD=8
CONFIG_STM32_TIM10=y
+10
View File
@@ -2,6 +2,7 @@ CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_BOOTLOADERS=y
CONFIG_DRIVERS_DISTANCE_SENSOR_BROADCOM_AFBRS50=y
@@ -10,7 +11,16 @@ CONFIG_DRIVERS_IMU_INVENSENSE_ICM42688P=y
CONFIG_DRIVERS_OPTICAL_FLOW_PAW3902=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
# CONFIG_SENSORS_VEHICLE_MAGNETOMETER is not set
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
@@ -3,6 +3,8 @@
# board sensors init
#------------------------------------------------------------------------------
param set-default IMU_GYRO_RATEMAX 1000
# Internal SPI
paw3902 -s start -Y 180
@@ -105,8 +105,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
+13 -1
View File
@@ -4,7 +4,6 @@ CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_BOARD_EXTERNAL_METADATA=y
CONFIG_DRIVERS_BAROMETER_BMP388=y
CONFIG_DRIVERS_BOOTLOADERS=y
CONFIG_DRIVERS_GPS=y
@@ -14,5 +13,18 @@ CONFIG_DRIVERS_SAFETY_BUTTON=y
CONFIG_DRIVERS_TONE_ALARM=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
@@ -4,6 +4,7 @@
#------------------------------------------------------------------------------
param set-default CBRK_IO_SAFETY 0
param set-default MBE_ENABLE 1
safety_button start
tone_alarm start
@@ -107,8 +107,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
+13 -1
View File
@@ -4,7 +4,6 @@ CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_BOARD_EXTERNAL_METADATA=y
CONFIG_DRIVERS_BAROMETER_BMP388=y
CONFIG_DRIVERS_BOOTLOADERS=y
CONFIG_DRIVERS_GPS=y
@@ -14,5 +13,18 @@ CONFIG_DRIVERS_SAFETY_BUTTON=y
CONFIG_DRIVERS_TONE_ALARM=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
@@ -5,6 +5,7 @@
param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_GPS_RTCM 1
param set-default MBE_ENABLE 1
safety_button start
tone_alarm start
@@ -107,8 +107,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -107,8 +107,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -140,8 +140,7 @@ CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_MODE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
+1 -2
View File
@@ -162,8 +162,7 @@ CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_MODE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -30,6 +30,7 @@ CONFIG_MODULES_MC_RATE_CONTROL=y
CONFIG_MODULES_NAVIGATOR=y
CONFIG_MODULES_RC_UPDATE=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
CONFIG_SYSTEMCMDS_DMESG=y
CONFIG_SYSTEMCMDS_HARDFAULT_LOG=y
CONFIG_SYSTEMCMDS_MFT=y
@@ -126,8 +126,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -141,6 +141,7 @@
#define PX4_PWM_ALTERNATE_RANGES
#define PWM_LOWEST_MIN 0
#define PWM_MOTOR_OFF 0
#define PWM_SERVO_STOP 0
#define PWM_DEFAULT_MIN 20
#define PWM_HIGHEST_MIN 0
#define PWM_HIGHEST_MAX 255
@@ -30,6 +30,7 @@ CONFIG_MODULES_MC_RATE_CONTROL=y
CONFIG_MODULES_NAVIGATOR=y
CONFIG_MODULES_RC_UPDATE=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
CONFIG_SYSTEMCMDS_DMESG=y
CONFIG_SYSTEMCMDS_HARDFAULT_LOG=y
CONFIG_SYSTEMCMDS_MIXER=y
@@ -125,8 +125,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -142,6 +142,7 @@
#define PX4_PWM_ALTERNATE_RANGES
#define PWM_LOWEST_MIN 0
#define PWM_MOTOR_OFF 0
#define PWM_SERVO_STOP 0
#define PWM_DEFAULT_MIN 20
#define PWM_HIGHEST_MIN 0
#define PWM_HIGHEST_MAX 255
+13
View File
@@ -1,6 +1,8 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_BOARD_COMPILE_DEFINITIONS="-DUSE_S_RGB_LED_DMA"
CONFIG_DRIVERS_BAROMETER_MS5611=y
@@ -12,5 +14,16 @@ CONFIG_DRIVERS_SAFETY_BUTTON=y
CONFIG_DRIVERS_TONE_ALARM=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
@@ -108,8 +108,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
Binary file not shown.
+1 -2
View File
@@ -139,8 +139,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -111,6 +111,7 @@ MEMORY
{
ITCM_RAM (rwx) : ORIGIN = 0x00000000, LENGTH = 64K
FLASH (rx) : ORIGIN = 0x08020000, LENGTH = 1920K
DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH = 64K
DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH = 64K
AXI_SRAM (rwx) : ORIGIN = 0x24000000, LENGTH = 512K /* D1 domain AXI bus */
@@ -186,7 +187,12 @@ SECTIONS
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > AXI_SRAM AT > FLASH
/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
. = ALIGN(16);
FILL(0xffff)
. += 16;
} > AXI_SRAM AT > FLASH = 0xffff
.bss : {
_sbss = ABSOLUTE(.);
+2 -2
View File
@@ -118,8 +118,8 @@
#define GPIO_nPOWER_IN_CAN /* PG2 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN2)
#define GPIO_nPOWER_IN_C /* PG0 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN0)
#define GPIO_nVDD_BRICK1_VALID GPIO_nPOWER_IN_CAN /* Brick 1 is Chosen */
#define GPIO_nVDD_BRICK2_VALID GPIO_nPOWER_IN_ADC /* Brick 2 is Chosen */
#define GPIO_nVDD_BRICK1_VALID GPIO_nPOWER_IN_ADC /* Brick 1 is Chosen */
#define GPIO_nVDD_BRICK2_VALID GPIO_nPOWER_IN_CAN /* Brick 2 is Chosen */
#define GPIO_nVDD_USB_VALID GPIO_nPOWER_IN_C /* USB is Chosen */
#define GPIO_VDD_5V_HIPOWER_EN /* PD11 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTD|GPIO_PIN11)
+1
View File
@@ -106,3 +106,4 @@ CONFIG_SYSTEMCMDS_USB_CONNECTED=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
CONFIG_EXAMPLES_FAKE_GPS=y
#CONFIG_DRIVERS_TRANSPONDER_SAGETECH_MXS=y
Binary file not shown.
+2 -2
View File
@@ -60,6 +60,7 @@ CONFIG_DEFAULT_SMALL=y
CONFIG_DEV_FIFO_SIZE=0
CONFIG_DEV_PIPE_MAXSIZE=1024
CONFIG_DEV_PIPE_SIZE=70
CONFIG_DISABLE_MQUEUE=y
CONFIG_EXAMPLES_CALIB_UDELAY=y
CONFIG_EXPERIMENTAL=y
CONFIG_FAT_DMAMEMORY=y
@@ -138,8 +139,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -111,6 +111,7 @@ MEMORY
{
ITCM_RAM (rwx) : ORIGIN = 0x00000000, LENGTH = 64K
FLASH (rx) : ORIGIN = 0x08020000, LENGTH = 1920K
DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH = 64K
DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH = 64K
AXI_SRAM (rwx) : ORIGIN = 0x24000000, LENGTH = 512K /* D1 domain AXI bus */
@@ -186,7 +187,12 @@ SECTIONS
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > AXI_SRAM AT > FLASH
/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
. = ALIGN(16);
FILL(0xffff)
. += 16;
} > AXI_SRAM AT > FLASH = 0xffff
.bss : {
_sbss = ABSOLUTE(.);
@@ -0,0 +1,245 @@
#
# This file is autogenerated: PLEASE DO NOT EDIT IT.
#
# You can use "make menuconfig" to make any modifications to the installed .config file.
# You can then do "make savedefconfig" to generate a new defconfig file that includes your
# modifications.
#
# CONFIG_DISABLE_ENVIRON is not set
# CONFIG_DISABLE_PSEUDOFS_OPERATIONS is not set
# CONFIG_MMCSD_HAVE_CARDDETECT is not set
# CONFIG_MMCSD_HAVE_WRITEPROTECT is not set
# CONFIG_MMCSD_MMCSUPPORT is not set
# CONFIG_MMCSD_SPI is not set
# CONFIG_NSH_DISABLEBG is not set
# CONFIG_NSH_DISABLESCRIPT is not set
# CONFIG_NSH_DISABLE_DF is not set
# CONFIG_NSH_DISABLE_EXEC is not set
# CONFIG_NSH_DISABLE_EXIT is not set
# CONFIG_NSH_DISABLE_GET is not set
# CONFIG_NSH_DISABLE_ITEF is not set
# CONFIG_NSH_DISABLE_LOOPS is not set
# CONFIG_NSH_DISABLE_MKFATFS is not set
# CONFIG_NSH_DISABLE_SEMICOLON is not set
# CONFIG_NSH_DISABLE_TIME is not set
CONFIG_ARCH="arm"
CONFIG_ARCH_BOARD_CUSTOM=y
CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/cuav/x7pro/nuttx-config"
CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
CONFIG_ARCH_CHIP="stm32h7"
CONFIG_ARCH_CHIP_STM32H743XI=y
CONFIG_ARCH_CHIP_STM32H7=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARCH_STACKDUMP=y
CONFIG_ARMV7M_BASEPRI_WAR=y
CONFIG_ARMV7M_DCACHE=y
CONFIG_ARMV7M_DTCM=y
CONFIG_ARMV7M_ICACHE=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_ARM_MPU_EARLY_RESET=y
CONFIG_BOARDCTL_RESET=y
CONFIG_BOARD_CRASHDUMP=y
CONFIG_BOARD_LOOPSPERMSEC=95150
CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_BUILTIN=y
CONFIG_C99_BOOL8=y
CONFIG_CDCACM=y
CONFIG_CDCACM_IFLOWCONTROL=y
CONFIG_CDCACM_PRODUCTID=0x004c
CONFIG_CDCACM_PRODUCTSTR="PX4 CUAV X7Pro"
CONFIG_CDCACM_RXBUFSIZE=600
CONFIG_CDCACM_TXBUFSIZE=12000
CONFIG_CDCACM_VENDORID=0x3163
CONFIG_CDCACM_VENDORSTR="CUAV"
CONFIG_DEBUG_FULLOPT=y
CONFIG_DEBUG_HARDFAULT_ALERT=y
CONFIG_DEBUG_SYMBOLS=y
CONFIG_DEFAULT_SMALL=y
CONFIG_DEV_FIFO_SIZE=0
CONFIG_DEV_PIPE_MAXSIZE=1024
CONFIG_DEV_PIPE_SIZE=70
CONFIG_DISABLE_MQUEUE=y
CONFIG_EXAMPLES_CALIB_UDELAY=y
CONFIG_EXPERIMENTAL=y
CONFIG_FAT_DMAMEMORY=y
CONFIG_FAT_LCNAMES=y
CONFIG_FAT_LFN=y
CONFIG_FAT_LFN_ALIAS_HASH=y
CONFIG_FDCLONE_STDIO=y
CONFIG_FS_BINFS=y
CONFIG_FS_CROMFS=y
CONFIG_FS_FAT=y
CONFIG_FS_FATTIME=y
CONFIG_FS_PROCFS=y
CONFIG_FS_PROCFS_INCLUDE_PROGMEM=y
CONFIG_FS_PROCFS_MAX_TASKS=64
CONFIG_FS_PROCFS_REGISTER=y
CONFIG_FS_ROMFS=y
CONFIG_GRAN=y
CONFIG_GRAN_INTR=y
CONFIG_HAVE_CXX=y
CONFIG_HAVE_CXXINITIALIZE=y
CONFIG_I2C=y
CONFIG_I2C_RESET=y
CONFIG_IDLETHREAD_STACKSIZE=750
CONFIG_LIBC_LONG_LONG=y
CONFIG_LIBC_STRERROR=y
CONFIG_MEMSET_64BIT=y
CONFIG_MEMSET_OPTSPEED=y
CONFIG_MMCSD=y
CONFIG_MMCSD_SDIO=y
CONFIG_MMCSD_SDIOWAIT_WRCOMPLETE=y
CONFIG_MM_REGIONS=4
CONFIG_MTD=y
CONFIG_MTD_BYTE_WRITE=y
CONFIG_MTD_PARTITION=y
CONFIG_MTD_PROGMEM=y
CONFIG_MTD_RAMTRON=y
CONFIG_NAME_MAX=40
CONFIG_NSH_ARCHINIT=y
CONFIG_NSH_ARGCAT=y
CONFIG_NSH_BUILTIN_APPS=y
CONFIG_NSH_CMDPARMS=y
CONFIG_NSH_CROMFSETC=y
CONFIG_NSH_DISABLE_IFCONFIG=y
CONFIG_NSH_DISABLE_IFUPDOWN=y
CONFIG_NSH_DISABLE_TELNETD=y
CONFIG_NSH_LINELEN=128
CONFIG_NSH_MAXARGUMENTS=15
CONFIG_NSH_NESTDEPTH=8
CONFIG_NSH_QUOTE=y
CONFIG_NSH_ROMFSETC=y
CONFIG_NSH_ROMFSSECTSIZE=128
CONFIG_NSH_STRERROR=y
CONFIG_NSH_VARS=y
CONFIG_OTG_ID_GPIO_DISABLE=y
CONFIG_PIPES=y
CONFIG_PREALLOC_TIMERS=50
CONFIG_PRIORITY_INHERITANCE=y
CONFIG_PTHREAD_MUTEX_ROBUST=y
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_RAMTRON_SETSPEED=y
CONFIG_RAM_SIZE=245760
CONFIG_RAM_START=0x20010000
CONFIG_RAW_BINARY=y
CONFIG_READLINE_CMD_HISTORY=y
CONFIG_READLINE_TABCOMPLETION=y
CONFIG_RTC_DATETIME=y
CONFIG_SCHED_ATEXIT=y
CONFIG_SCHED_HPWORK=y
CONFIG_SCHED_HPWORKPRIORITY=249
CONFIG_SCHED_HPWORKSTACKSIZE=1280
CONFIG_SCHED_INSTRUMENTATION=y
CONFIG_SCHED_INSTRUMENTATION_EXTERNAL=y
CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
CONFIG_SIG_SIGUSR1_ACTION=y
CONFIG_SIG_SIGUSR2_ACTION=y
CONFIG_SIG_SIGWORK=4
CONFIG_STACK_COLORATION=y
CONFIG_START_DAY=30
CONFIG_START_MONTH=11
CONFIG_STDIO_BUFFER_SIZE=256
CONFIG_STM32H7_ADC1=y
CONFIG_STM32H7_ADC3=y
CONFIG_STM32H7_BBSRAM=y
CONFIG_STM32H7_BBSRAM_FILES=5
CONFIG_STM32H7_BDMA=y
CONFIG_STM32H7_BKPSRAM=y
CONFIG_STM32H7_DMA1=y
CONFIG_STM32H7_DMA2=y
CONFIG_STM32H7_DMACAPABLE=y
CONFIG_STM32H7_FLOWCONTROL_BROKEN=y
CONFIG_STM32H7_I2C1=y
CONFIG_STM32H7_I2C2=y
CONFIG_STM32H7_I2C3=y
CONFIG_STM32H7_I2C4=y
CONFIG_STM32H7_I2C_DYNTIMEO=y
CONFIG_STM32H7_I2C_DYNTIMEO_STARTSTOP=10
CONFIG_STM32H7_OTGFS=y
CONFIG_STM32H7_PROGMEM=y
CONFIG_STM32H7_RTC=y
CONFIG_STM32H7_RTC_HSECLOCK=y
CONFIG_STM32H7_RTC_MAGIC_REG=1
CONFIG_STM32H7_SAVE_CRASHDUMP=y
CONFIG_STM32H7_SDMMC1=y
CONFIG_STM32H7_SERIALBRK_BSDCOMPAT=y
CONFIG_STM32H7_SERIAL_DISABLE_REORDERING=y
CONFIG_STM32H7_SPI1=y
CONFIG_STM32H7_SPI1_DMA=y
CONFIG_STM32H7_SPI1_DMA_BUFFER=1024
CONFIG_STM32H7_SPI2=y
CONFIG_STM32H7_SPI4=y
CONFIG_STM32H7_SPI4_DMA=y
CONFIG_STM32H7_SPI4_DMA_BUFFER=1024
CONFIG_STM32H7_SPI5=y
CONFIG_STM32H7_SPI6=y
CONFIG_STM32H7_SPI6_DMA=y
CONFIG_STM32H7_SPI6_DMA_BUFFER=1024
CONFIG_STM32H7_SPI_DMA=y
CONFIG_STM32H7_TIM12=y
CONFIG_STM32H7_TIM15=y
CONFIG_STM32H7_TIM1=y
CONFIG_STM32H7_TIM3=y
CONFIG_STM32H7_TIM4=y
CONFIG_STM32H7_TIM5=y
CONFIG_STM32H7_TIM8=y
CONFIG_STM32H7_UART4=y
CONFIG_STM32H7_UART7=y
CONFIG_STM32H7_UART8=y
CONFIG_STM32H7_USART1=y
CONFIG_STM32H7_USART2=y
CONFIG_STM32H7_USART6=y
CONFIG_STM32H7_USART_BREAKS=y
CONFIG_STM32H7_USART_INVERT=y
CONFIG_STM32H7_USART_SINGLEWIRE=y
CONFIG_STM32H7_USART_SWAP=y
CONFIG_SYSTEM_CDCACM=y
CONFIG_SYSTEM_NSH=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_TESTING_OSTEST=y
CONFIG_TESTING_OSTEST_FPUTESTDISABLE=y
CONFIG_TESTING_OSTEST_STACKSIZE=10240
CONFIG_TTY_SIGINT=y
CONFIG_TTY_SIGTSTP=y
CONFIG_UART4_BAUD=57600
CONFIG_UART4_RXBUFSIZE=600
CONFIG_UART4_TXBUFSIZE=1500
CONFIG_UART7_BAUD=57600
CONFIG_UART7_RXBUFSIZE=600
CONFIG_UART7_SERIAL_CONSOLE=y
CONFIG_UART7_TXBUFSIZE=1500
CONFIG_UART8_BAUD=57600
CONFIG_UART8_RXBUFSIZE=600
CONFIG_UART8_TXBUFSIZE=1500
CONFIG_USART1_BAUD=57600
CONFIG_USART1_RXBUFSIZE=600
CONFIG_USART1_TXBUFSIZE=1500
CONFIG_USART2_BAUD=57600
CONFIG_USART2_IFLOWCONTROL=y
CONFIG_USART2_OFLOWCONTROL=y
CONFIG_USART2_RXBUFSIZE=600
CONFIG_USART2_TXBUFSIZE=1500
CONFIG_USART6_BAUD=57600
CONFIG_USART6_IFLOWCONTROL=y
CONFIG_USART6_OFLOWCONTROL=y
CONFIG_USART6_RXBUFSIZE=600
CONFIG_USART6_TXBUFSIZE=1500
CONFIG_USBDEV=y
CONFIG_USBDEV_BUSPOWERED=y
CONFIG_USBDEV_MAXPOWER=500
CONFIG_USEC_PER_TICK=1000
CONFIG_USERMAIN_STACKSIZE=2944
CONFIG_USER_ENTRYPOINT="nsh_main"
CONFIG_WATCHDOG=y
+6 -8
View File
@@ -7,7 +7,7 @@ CONFIG_BOARD_SERIAL_TEL1="/dev/ttyS0"
CONFIG_BOARD_SERIAL_TEL2="/dev/ttyS1"
CONFIG_DRIVERS_ADC_ADS1115=y
CONFIG_DRIVERS_ADC_BOARD_ADC=y
CONFIG_COMMON_BAROMETERS=y
CONFIG_DRIVERS_BAROMETER_MS5611=y
CONFIG_DRIVERS_BATT_SMBUS=y
CONFIG_DRIVERS_CAMERA_CAPTURE=y
CONFIG_DRIVERS_CAMERA_TRIGGER=y
@@ -24,14 +24,13 @@ CONFIG_COMMON_LIGHT=y
CONFIG_COMMON_MAGNETOMETER=y
CONFIG_COMMON_OPTICAL_FLOW=y
CONFIG_DRIVERS_OSD=y
CONFIG_DRIVERS_PCA9685=y
CONFIG_DRIVERS_PCA9685_PWM_OUT=y
CONFIG_DRIVERS_POWER_MONITOR_INA226=y
CONFIG_DRIVERS_PWM_INPUT=y
CONFIG_DRIVERS_PWM_OUT=y
CONFIG_DRIVERS_PWM_OUT_SIM=y
CONFIG_DRIVERS_PX4IO=y
CONFIG_DRIVERS_ROBOCLAW=y
#CONFIG_DRIVERS_ROBOCLAW=y
CONFIG_DRIVERS_RPM=y
CONFIG_DRIVERS_SMART_BATTERY_BATMON=y
CONFIG_COMMON_TELEMETRY=y
@@ -42,6 +41,7 @@ CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
CONFIG_MODULES_BATTERY_STATUS=y
CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
@@ -50,6 +50,7 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL_L1=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y
CONFIG_MODULES_LAND_DETECTOR=y
@@ -65,17 +66,15 @@ CONFIG_MODULES_MC_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=y
CONFIG_MODULES_MC_POS_CONTROL=y
CONFIG_MODULES_MC_RATE_CONTROL=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_NAVIGATOR=y
CONFIG_MODULES_RC_UPDATE=y
CONFIG_MODULES_ROVER_POS_CONTROL=y
CONFIG_MODULES_SENSORS=y
CONFIG_MODULES_SIH=y
CONFIG_MODULES_TEMPERATURE_COMPENSATION=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_VTOL_ATT_CONTROL=y
CONFIG_SYSTEMCMDS_BL_UPDATE=y
CONFIG_SYSTEMCMDS_ACTUATOR_TEST=y
CONFIG_SYSTEMCMDS_BL_UPDATE=y
CONFIG_SYSTEMCMDS_DMESG=y
CONFIG_SYSTEMCMDS_DUMPFILE=y
CONFIG_SYSTEMCMDS_GPIO=y
@@ -93,7 +92,6 @@ CONFIG_SYSTEMCMDS_PWM=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_REFLECT=y
CONFIG_SYSTEMCMDS_SD_BENCH=y
CONFIG_SYSTEMCMDS_SD_STRESS=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
@@ -102,4 +100,4 @@ CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_USB_CONNECTED=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
CONFIG_EXAMPLES_FAKE_GPS=y
CONFIG_DRIVERS_TRANSPONDER_SAGETECH_MXS=y
@@ -140,8 +140,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -187,7 +187,12 @@ SECTIONS
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > AXI_SRAM AT > FLASH
/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
. = ALIGN(16);
FILL(0xffff)
. += 16;
} > AXI_SRAM AT > FLASH = 0xffff
.bss : {
_sbss = ABSOLUTE(.);
@@ -60,6 +60,7 @@ CONFIG_DEFAULT_SMALL=y
CONFIG_DEV_FIFO_SIZE=0
CONFIG_DEV_PIPE_MAXSIZE=1024
CONFIG_DEV_PIPE_SIZE=70
CONFIG_DISABLE_MQUEUE=y
CONFIG_EXAMPLES_CALIB_UDELAY=y
CONFIG_EXPERIMENTAL=y
CONFIG_FAT_DMAMEMORY=y
@@ -138,8 +139,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -197,6 +197,9 @@ CONFIG_STM32H7_USART_SWAP=y
CONFIG_SYSTEM_CDCACM=y
CONFIG_SYSTEM_NSH=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_TESTING_OSTEST=y
CONFIG_TESTING_OSTEST_FPUTESTDISABLE=y
CONFIG_TESTING_OSTEST_STACKSIZE=10240
CONFIG_TTY_SIGINT=y
CONFIG_TTY_SIGTSTP=y
CONFIG_UART4_BAUD=57600
+1 -1
View File
@@ -5,7 +5,6 @@ CONFIG_DRIVERS_PCA9685=n
CONFIG_DRIVERS_PCA9685_PWM_OUT=n
CONFIG_DRIVERS_RPM=n
CONFIG_DRIVERS_UAVCAN=n
CONFIG_EXAMPLES_FAKE_GPS=n
CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=n
CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=n
CONFIG_MODULES_ROVER_POS_CONTROL=n
@@ -13,3 +12,4 @@ CONFIG_MODULES_TEMPERATURE_COMPENSATION=n
CONFIG_BOARD_TESTING=y
CONFIG_DRIVERS_TEST_PPM=y
CONFIG_SYSTEMCMDS_MICROBENCH=y
CONFIG_SYSTEMCMDS_SD_STRESS=y
@@ -141,8 +141,7 @@ CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_MODE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -120,8 +120,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -158,7 +157,7 @@ CONFIG_STM32_SERIALBRK_BSDCOMPAT=y
CONFIG_STM32_SERIAL_DISABLE_REORDERING=y
CONFIG_STM32_SPI1=y
CONFIG_STM32_SPI1_DMA=y
CONFIG_STM32_SPI1_DMA_BUFFER=1024
CONFIG_STM32_SPI1_DMA_BUFFER=512
CONFIG_STM32_SPI2=y
CONFIG_STM32_SPI2_DMA=y
CONFIG_STM32_SPI3=y
@@ -176,8 +175,8 @@ CONFIG_SYSTEM_CDCACM=y
CONFIG_SYSTEM_NSH=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_UART4_BAUD=57600
CONFIG_UART4_RXBUFSIZE=300
CONFIG_UART4_TXBUFSIZE=900
CONFIG_UART4_RXBUFSIZE=600
CONFIG_UART4_TXBUFSIZE=600
CONFIG_USART1_RXBUFSIZE=300
CONFIG_USART1_RXDMA=y
CONFIG_USART1_TXBUFSIZE=300
+10 -2
View File
@@ -1,16 +1,22 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m7"
CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_BAROMETER_BMP388=y
CONFIG_DRIVERS_BOOTLOADERS=y
CONFIG_DRIVERS_GPS=y
CONFIG_DRIVERS_IMU_ST=y
CONFIG_DRIVERS_LIGHTS_RGBLED_NCP5623C=y
CONFIG_DRIVERS_MAGNETOMETER_ISENTEK_IST8310=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_LOAD_MON=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
CONFIG_SYSTEMCMDS_LED_CONTROL=y
CONFIG_SYSTEMCMDS_MFT=y
CONFIG_SYSTEMCMDS_MTD=y
@@ -19,5 +25,7 @@ CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
@@ -122,8 +122,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -2,6 +2,7 @@ CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_ADC_BOARD_ADC=y
CONFIG_DRIVERS_BAROMETER_BMP388=y
@@ -12,6 +13,18 @@ CONFIG_DRIVERS_LIGHTS_RGBLED_NCP5623C=y
CONFIG_DRIVERS_MAGNETOMETER_BOSCH_BMM150=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
@@ -108,8 +108,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
@@ -140,8 +140,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -109,16 +109,17 @@
MEMORY
{
itcm (rwx) : ORIGIN = 0x00000000, LENGTH = 64K
flash (rx) : ORIGIN = 0x08020000, LENGTH = 1920K
dtcm1 (rwx) : ORIGIN = 0x20000000, LENGTH = 64K
dtcm2 (rwx) : ORIGIN = 0x20010000, LENGTH = 64K
sram (rwx) : ORIGIN = 0x24000000, LENGTH = 512K
sram1 (rwx) : ORIGIN = 0x30000000, LENGTH = 128K
sram2 (rwx) : ORIGIN = 0x30020000, LENGTH = 128K
sram3 (rwx) : ORIGIN = 0x30040000, LENGTH = 32K
sram4 (rwx) : ORIGIN = 0x38000000, LENGTH = 64K
bbram (rwx) : ORIGIN = 0x38800000, LENGTH = 4K
ITCM_RAM (rwx) : ORIGIN = 0x00000000, LENGTH = 64K
FLASH (rx) : ORIGIN = 0x08020000, LENGTH = 1920K
DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH = 64K
DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH = 64K
AXI_SRAM (rwx) : ORIGIN = 0x24000000, LENGTH = 512K /* D1 domain AXI bus */
SRAM1 (rwx) : ORIGIN = 0x30000000, LENGTH = 128K /* D2 domain AHB bus */
SRAM2 (rwx) : ORIGIN = 0x30020000, LENGTH = 128K /* D2 domain AHB bus */
SRAM3 (rwx) : ORIGIN = 0x30040000, LENGTH = 32K /* D2 domain AHB bus */
SRAM4 (rwx) : ORIGIN = 0x38000000, LENGTH = 64K /* D3 domain */
BKPRAM (rwx) : ORIGIN = 0x38800000, LENGTH = 4K
}
OUTPUT_ARCH(arm)
@@ -156,7 +157,7 @@ SECTIONS
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
} > FLASH
/*
* Init functions (static constructors and the like)
@@ -165,17 +166,17 @@ SECTIONS
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
} > FLASH
.ARM.extab : {
*(.ARM.extab*)
} > flash
} > FLASH
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
} > FLASH
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
@@ -186,7 +187,12 @@ SECTIONS
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
. = ALIGN(16);
FILL(0xffff)
. += 16;
} > AXI_SRAM AT > FLASH = 0xffff
.bss : {
_sbss = ABSOLUTE(.);
@@ -195,7 +201,7 @@ SECTIONS
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
} > AXI_SRAM
/* Emit the the D3 power domain section for locating BDMA data */
@@ -204,7 +210,7 @@ SECTIONS
*(.sram4)
. = ALIGN(4);
_sram4_heap_start = ABSOLUTE(.);
} > sram4
} > SRAM4
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
+2
View File
@@ -1,5 +1,6 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m7"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_EXTERNAL_METADATA=y
CONFIG_BOARD_SERIAL_GPS1="/dev/ttyS3"
@@ -31,6 +32,7 @@ CONFIG_MODULES_MC_RATE_CONTROL=y
CONFIG_MODULES_NAVIGATOR=y
CONFIG_MODULES_RC_UPDATE=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
CONFIG_SYSTEMCMDS_MIXER=y
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PWM=y
@@ -140,8 +140,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
+5 -4
View File
@@ -15,10 +15,10 @@ CONFIG_DRIVERS_DSHOT=y
CONFIG_DRIVERS_GPS=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM20689=y
CONFIG_DRIVERS_IMU_INVENSENSE_MPU6000=y
CONFIG_DRIVERS_OSD=y
CONFIG_COMMON_LIGHT=y
CONFIG_COMMON_MAGNETOMETER=y
CONFIG_COMMON_OPTICAL_FLOW=y
CONFIG_DRIVERS_OSD=y
CONFIG_DRIVERS_POWER_MONITOR_INA226=y
CONFIG_DRIVERS_PWM_OUT=y
CONFIG_DRIVERS_PWM_OUT_SIM=y
@@ -28,8 +28,8 @@ CONFIG_DRIVERS_RPM=y
CONFIG_DRIVERS_SMART_BATTERY_BATMON=y
CONFIG_COMMON_TELEMETRY=y
CONFIG_DRIVERS_TONE_ALARM=y
CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
CONFIG_MODULES_AIRSPEED_SELECTOR=y
CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
CONFIG_MODULES_BATTERY_STATUS=y
CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
@@ -42,6 +42,7 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL_L1=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y
CONFIG_MODULES_LAND_DETECTOR=y
@@ -60,12 +61,12 @@ CONFIG_MODULES_NAVIGATOR=y
CONFIG_MODULES_RC_UPDATE=y
CONFIG_MODULES_ROVER_POS_CONTROL=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
CONFIG_MODULES_SIH=y
CONFIG_MODULES_TEMPERATURE_COMPENSATION=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_VTOL_ATT_CONTROL=y
CONFIG_SYSTEMCMDS_BL_UPDATE=y
CONFIG_SYSTEMCMDS_ACTUATOR_TEST=y
CONFIG_SYSTEMCMDS_BL_UPDATE=y
CONFIG_SYSTEMCMDS_DMESG=y
CONFIG_SYSTEMCMDS_DUMPFILE=y
CONFIG_SYSTEMCMDS_GPIO=y
@@ -139,8 +139,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -109,16 +109,17 @@
MEMORY
{
itcm (rwx) : ORIGIN = 0x00000000, LENGTH = 64K
flash (rx) : ORIGIN = 0x08020000, LENGTH = 1792K /* params in last sector */
dtcm1 (rwx) : ORIGIN = 0x20000000, LENGTH = 64K
dtcm2 (rwx) : ORIGIN = 0x20010000, LENGTH = 64K
sram (rwx) : ORIGIN = 0x24000000, LENGTH = 512K
sram1 (rwx) : ORIGIN = 0x30000000, LENGTH = 128K
sram2 (rwx) : ORIGIN = 0x30020000, LENGTH = 128K
sram3 (rwx) : ORIGIN = 0x30040000, LENGTH = 32K
sram4 (rwx) : ORIGIN = 0x38000000, LENGTH = 64K
bbram (rwx) : ORIGIN = 0x38800000, LENGTH = 4K
ITCM_RAM (rwx) : ORIGIN = 0x00000000, LENGTH = 64K
FLASH (rx) : ORIGIN = 0x08020000, LENGTH = 1792K /* params in last sector */
DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH = 64K
DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH = 64K
AXI_SRAM (rwx) : ORIGIN = 0x24000000, LENGTH = 512K /* D1 domain AXI bus */
SRAM1 (rwx) : ORIGIN = 0x30000000, LENGTH = 128K /* D2 domain AHB bus */
SRAM2 (rwx) : ORIGIN = 0x30020000, LENGTH = 128K /* D2 domain AHB bus */
SRAM3 (rwx) : ORIGIN = 0x30040000, LENGTH = 32K /* D2 domain AHB bus */
SRAM4 (rwx) : ORIGIN = 0x38000000, LENGTH = 64K /* D3 domain */
BKPRAM (rwx) : ORIGIN = 0x38800000, LENGTH = 4K
}
OUTPUT_ARCH(arm)
@@ -156,7 +157,7 @@ SECTIONS
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
} > FLASH
/*
* Init functions (static constructors and the like)
@@ -165,17 +166,17 @@ SECTIONS
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
} > FLASH
.ARM.extab : {
*(.ARM.extab*)
} > flash
} > FLASH
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
} > FLASH
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
@@ -186,7 +187,12 @@ SECTIONS
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
. = ALIGN(16);
FILL(0xffff)
. += 16;
} > AXI_SRAM AT > FLASH = 0xffff
.bss : {
_sbss = ABSOLUTE(.);
@@ -195,7 +201,7 @@ SECTIONS
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
} > AXI_SRAM
/* Emit the the D3 power domain section for locating BDMA data */
@@ -204,7 +210,7 @@ SECTIONS
*(.sram4)
. = ALIGN(4);
_sram4_heap_start = ABSOLUTE(.);
} > sram4
} > SRAM4
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
Binary file not shown.
@@ -140,8 +140,7 @@ CONFIG_SCHED_WAITPID=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SDMMC1_SDIO_MODE=y
CONFIG_SDMMC1_SDIO_PULLUP=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
@@ -1,6 +1,8 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_BOARD_SERIAL_GPS1="/dev/ttyS2"
CONFIG_DRIVERS_BAROMETER_DPS310=y
@@ -10,13 +12,20 @@ CONFIG_DRIVERS_IMU_INVENSENSE_ICM20602=y
CONFIG_DRIVERS_MAGNETOMETER_RM3100=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
CONFIG_SYSTEMCMDS_I2CDETECT=y
CONFIG_SYSTEMCMDS_NSHTERM=y
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_SERIAL_PASSTHRU=y
CONFIG_SERIAL_PASSTHRU_UBLOX=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
@@ -126,8 +126,7 @@ CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SEM_PREALLOCHOLDERS=32
CONFIG_SERIAL_PASSTHRU_UBLOX=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
+3 -2
View File
@@ -9,14 +9,15 @@ CONFIG_DRIVERS_ADC_BOARD_ADC=y
CONFIG_DRIVERS_BAROMETER_DPS310=y
CONFIG_DRIVERS_CAMERA_CAPTURE=n
CONFIG_DRIVERS_CAMERA_TRIGGER=n
CONFIG_COMMON_DISTANCE_SENSOR=y
CONFIG_DRIVERS_DSHOT=y
CONFIG_DRIVERS_GPS=y
CONFIG_DRIVERS_IMU_INVENSENSE_MPU6000=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM20602=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM42605=y
CONFIG_DRIVERS_MAGNETOMETER_QMC5883L=y
CONFIG_COMMON_DISTANCE_SENSOR=n
CONFIG_COMMON_LIGHT=n
CONFIG_COMMON_MAGNETOMETER=y
CONFIG_COMMON_MAGNETOMETER=n
CONFIG_COMMON_OPTICAL_FLOW=y
CONFIG_DRIVERS_OSD=y
CONFIG_DRIVERS_PWM_OUT=y

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