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21 Commits

Author SHA1 Message Date
Balduin
93c0d19712 preflight check: enable mode via command 2025-02-20 14:37:42 +01:00
Balduin
276a7a2ab2 ActuatorEffectivenessTiltrotorVTOL: move comment 2025-02-20 11:44:35 +01:00
Balduin
6613272a70 Commander: remove unneeded function
The preflight check can be enabled by switching to nav_state
vehicle_status_s::NAVIGATION_STATE_CS_PREFLIGHT_CHECK using
VEHICLE_CMD_SET_NAV_STATE. Thus we can ditch this function and forgo
adding an extra vehicle command.
2025-02-20 10:10:52 +01:00
Balduin
6e6df2e47e preflight check: format 2025-02-20 09:12:15 +01:00
Balduin
9654ac6b20 ActuatorEffectivenessTiltrotorVTOL: refactor
put everything related to tiltrotor extra controls into own function to
clean up updateSetpoint
2025-02-20 09:11:35 +01:00
Balduin
009c300216 preflight check: replace argument with setter
this allows us to have *only* the setter in the base class
(ActuatorEffectiveness) with an empty implementation. Derived classes
can implement another implementation, or stay completely unchanged
w.r.t. previously. This may finally be the desired clean-ish OOP-ish
solution to this.
2025-02-20 08:50:50 +01:00
Balduin
10bcc52f13 preflight check: only change nav_mode once 2025-02-19 16:30:01 +01:00
Balduin
dea58db757 preflight check: only conduct if pre-armed 2025-02-19 16:30:01 +01:00
Balduin
6e5f3a6099 preflight check: only conduct if not armed 2025-02-18 16:59:08 +01:00
Balduin
c28d015d9c preflight check: replace uOrb msg with argument
Previously, the approach to modify collective tilt control was to send
the corresponding tiltrotor_extra_control uOrb message from
ControlAllocator, which then influences
ActuatorEffectivenessTiltrotorVTOL with minimal changes.

This was a bit hacky and introduced potentially conflicting uOrb
messages. So, with this new approach we pass the same information via
argument.

Specifically, the class ActuatorEffectiveness now declares
updateSetpoint with an extra argument, preflight_check_running. It is
only used in ActuatorEffectivenessTiltrotorVTOL, but has to be included
as a "dummy" in all other classes inheriting from ActuatorEffectiveness.

The argument can be used to bypass the collective tilt/thrust setpoints,
instead replacing them with values from public class member variables
which can be set from outside just before calling updateSetpoints.

Also, slight refactor in ControlAllocator by splitting up the functions
related to the preflight check into smaller parts
2025-02-18 15:57:56 +01:00
Balduin
96fc4a0673 preflight check: modify actuator_sp if running
this adds a new flag to ActuatorEffectivenessTiltrotorVTOL:
_preflight_check_running. We set it from ControlAllocator, and if true
we always add collective tilt to the actuator setpoint.
2025-02-18 13:03:45 +01:00
Balduin
122643af25 preflight check: fix range 2025-02-18 13:03:38 +01:00
Balduin
71afdb5680 preflight check: restore old nav_state only once
previously it would always change _user_mode_intention to
_prev_nav_state forever. now we change it only if we are in preflight
check mode to not interfere with anything else later.
2025-02-18 11:08:12 +01:00
Balduin
0253f9798e preflight check: send tilt control always
even if we are not currently testing the tilt axis. then we send zero
tilt rather than nothing.
2025-02-18 11:08:06 +01:00
Balduin
ad42a5b2f9 preflight check: more self explanatory code 2025-02-17 17:46:39 +01:00
Balduin
761810884e preflight check: always send tiltrotor controls 2025-02-17 17:24:21 +01:00
Balduin
2a779663f6 preflight check: tilt collective actuation
we "intercept" the tiltrotor_extra_controls message, which is read again
right after in ActuatorEffectivenessTiltrotorVTOL::updateSetpoint.
2025-02-17 11:40:41 +01:00
Balduin
7816fd14b7 preflight check: restore prev nav state 2025-02-14 13:37:31 +01:00
Balduin
64d18f0a64 preflight check: first working version
modifies torque setpoints directly via the matrix c.
2025-02-14 12:17:10 +01:00
Balduin
a3cca099a8 preflight check: set vehicle_control_mode flags
not sure if all of these are needed, but with all of them the allocator
runs, and with only flag_control_allocation_enabled it does not.
2025-02-14 10:59:42 +01:00
Balduin
01a65bfcf6 preflight check: base business logic
- currently triggered via param COM_DO_CS_CHECK. ultimately this will
   be replaced by a mavlink cmd
 - new VehicleStatus.nav_state, NAVIGATION_STATE_CS_PREFLIGHT_CHECK.
   this is how commander tells ControlAllocator to conduct the check
 - (todo) within ControlAllocator we overwrite torque setpoints to do
   the check. additionally we can also control servos directly from
   there, in a different mode if that is needed.
2025-02-14 09:45:53 +01:00
414 changed files with 9038 additions and 13599 deletions

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@ -96,6 +96,6 @@ jobs:
platforms: |
linux/amd64
provenance: mode=max
push: ${{ github.event_name != 'pull_request' }}
push: true
cache-from: type=s3,blobs_prefix=cache/${{ github.repository }}/,manifests_prefix=cache/${{ github.repository }}/,region=${{ env.RUNS_ON_AWS_REGION }},bucket=${{ env.RUNS_ON_S3_BUCKET_CACHE }}
cache-to: type=s3,blobs_prefix=cache/${{ github.repository }}/,manifests_prefix=cache/${{ github.repository }}/,region=${{ env.RUNS_ON_AWS_REGION }},bucket=${{ env.RUNS_ON_S3_BUCKET_CACHE }},mode=max

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@ -1,10 +1,5 @@
name: FLASH usage analysis
permissions:
contents: read
pull-requests: write
issues: write
on:
push:
branches:

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@ -1,52 +0,0 @@
name: ROS Translation Node Tests
on:
push:
branches:
- 'main'
pull_request:
branches:
- '*'
defaults:
run:
shell: bash
jobs:
build_and_test:
name: Build and test
runs-on: [runs-on,runner=8cpu-linux-x64,image=ubuntu24-full-x64,"run-id=${{ github.run_id }}",spot=false]
strategy:
fail-fast: false
matrix:
config:
- {ros_version: "humble", ubuntu: "jammy"}
- {ros_version: "jazzy", ubuntu: "noble"}
container:
image: rostooling/setup-ros-docker:ubuntu-${{ matrix.config.ubuntu }}-latest
steps:
- name: Setup ROS 2 (${{ matrix.config.ros_version }})
uses: ros-tooling/setup-ros@v0.7
with:
required-ros-distributions: ${{ matrix.config.ros_version }}
- name: Checkout repository
uses: actions/checkout@v4
with:
fetch-depth: 0
# Workaround for https://github.com/actions/runner/issues/2033
- name: ownership workaround
run: git config --system --add safe.directory '*'
- name: Check .msg file versioning
if: github.event_name == 'pull_request'
run: |
./Tools/ci/check_msg_versioning.sh ${{ github.event.pull_request.base.sha }} ${{github.event.pull_request.head.sha}}
- name: Build and test
run: |
ros_ws=/ros_ws
mkdir -p $ros_ws/src
./Tools/copy_to_ros_ws.sh $ros_ws
cd $ros_ws
source /opt/ros/${{ matrix.config.ros_version }}/setup.sh
colcon build --cmake-args -DCMAKE_BUILD_TYPE=Release --symlink-install --event-handlers=console_cohesion+
source ./install/setup.sh
./build/translation_node/translation_node_unit_tests

2
.gitmodules vendored
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@ -75,7 +75,7 @@
[submodule "Tools/simulation/gz"]
path = Tools/simulation/gz
url = https://github.com/PX4/PX4-gazebo-models.git
branch = moving_platform_world
branch = main
[submodule "boards/modalai/voxl2/libfc-sensor-api"]
path = boards/modalai/voxl2/libfc-sensor-api
url = https://gitlab.com/voxl-public/voxl-sdk/core-libs/libfc-sensor-api.git

4
Jenkinsfile vendored
View File

@ -235,9 +235,9 @@ pipeline {
sh('rm -f px4_msgs/srv/*.srv')
sh('rm -f px4_msgs/srv/versioned/*.srv')
sh('cp msg/*.msg px4_msgs/msg/')
sh('cp msg/versioned/*.msg px4_msgs/msg/ || true')
sh('mkdir -p px4_msgs/msg/versioned && cp msg/versioned/*.msg px4_msgs/msg/versioned/')
sh('cp srv/*.srv px4_msgs/srv/')
sh('cp srv/versioned/*.srv px4_msgs/srv/ || true')
sh('mkdir -p px4_msgs/srv/versioned && cp srv/versioned/*.srv px4_msgs/srv/versioned/')
sh('cd px4_msgs; git status; git add .; git commit -a -m "Update message definitions `date`" || true')
sh('cd px4_msgs; git push origin main || true')
sh('rm -rf px4_msgs')

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@ -1,42 +0,0 @@
Maintainers
===========
See [the documentation on Maintainers](https://docs.px4.io/main/en/contribute/maintainers.html) to learn about the role of the maintainers and the process to become one.
**Active Maintainers**
| Name | Sector | GitHub | Chat | email
|-------------------------|--------|--------|------|----------------
| Lorenz Meier | Founder | [LorenzMeier][LorenzMeier] | | <lorenz@px4.io>
| Daniel Agar | Architecture | [dagar][dagar] | daniel_agar | <daniel@agar.ca>
| Beat Küng | Architecture | [bkueng][bkueng] | beatkueng | <beat-kueng@gmx.net>
| Ramón Roche | CI / Testing | [mrpollo][mrpollo] | rroche | <rroche@linuxfoundation.org>
| Mathieu Bresciani | State Estimation | [bresch][bresch] | mbresch |
| Paul Riseborough | State Estimation | [priseborough][priseborough] | |
| David Sidrane | RTOS / NuttX | [davids5][davids5] | david_s5 | <David.Sidrane@Nscdg.com>
| Jayoung Lim | Simulation | [Jaeyoung-Lim][Jaeyoung-Lim] | jaeyounglim. | <jalim@ethz.ch>
| Beniamino Pozzan | ROS 2 | [beniaminopozzan][beniaminopozzan] | beniaminopozzan | <beniamino.pozzan@gmail.com>
| Matthias Grob | Multirotor | [MaEtUgR][MaEtUgR] | maetugr |
| Silvan Fuhrer | Fixed-Wing / VTOL | [sfuhrer][sfuhrer] | sfuhrer |
| Christian Friedrich | Rover | [chfriedrich98][chfriedrich98] | christian982564 |
| Pedro Roque | Spacecraft | [Pedro-Roque][Pedro-Roque] | .pedroroque | <padr@kth.se>
**Documentation Maintainers**
| Name | GitHub | Chat | email
|------|--------|------|----------------------
| Hamish Willee | [hamishwillee][hamishwillee] | hamishwillee |
**Release Managers**
| Name | GitHub | Chat | email
|------|--------|------|----------------------
| Ramón Roche | [mrpollo][mrpollo] | rroche | <rroche@linuxfoundation.org>
| Daniel Agar | [dagar][dagar] | daniel_agar | <daniel@agar.ca>
**Retired Maintainers**
| Name | GitHub | Chat | email
|------|--------|------|----------------------
| | | |

View File

@ -404,7 +404,7 @@ check_newlines:
# Testing
# --------------------------------------------------------------------
.PHONY: tests tests_coverage tests_mission tests_mission_coverage tests_offboard
.PHONY: tests tests_coverage tests_mission tests_mission_coverage tests_offboard tests_avoidance
.PHONY: rostest python_coverage
tests:
@ -457,6 +457,10 @@ tests_offboard: rostest
@"$(SRC_DIR)"/test/rostest_px4_run.sh mavros_posix_tests_offboard_posctl.test
@"$(SRC_DIR)"/test/rostest_px4_run.sh mavros_posix_tests_offboard_rpyrt_ctl.test
tests_avoidance: rostest
@"$(SRC_DIR)"/test/rostest_avoidance_run.sh mavros_posix_test_avoidance.test
@"$(SRC_DIR)"/test/rostest_avoidance_run.sh mavros_posix_test_safe_landing.test
python_coverage:
@mkdir -p "$(SRC_DIR)"/build/python_coverage
@cd "$(SRC_DIR)"/build/python_coverage && cmake "$(SRC_DIR)" $(CMAKE_ARGS) -G"$(PX4_CMAKE_GENERATOR)" -DCONFIG=px4_sitl_default -DPYTHON_COVERAGE=ON

View File

@ -44,9 +44,30 @@ The PX4 Dev Team syncs up on a [weekly dev call](https://docs.px4.io/main/en/con
## Maintenance Team
See the latest list of maintainers on [MAINTAINERS](MAINTAINERS.md) file at the root of the project.
Note: This is the source of truth for the active maintainers of PX4 ecosystem.
For the latest stats on contributors please see the latest stats for the Dronecode ecosystem in our project dashboard under [LFX Insights](https://insights.lfx.linuxfoundation.org/foundation/dronecode). For information on how to update your profile and affiliations please see the following support link on how to [Complete Your LFX Profile](https://docs.linuxfoundation.org/lfx/my-profile/complete-your-lfx-profile). Dronecode publishes a yearly snapshot of contributions and achievements on its [website under the Reports section](https://dronecode.org).
| Sector | Maintainer |
|---|---|
| Founder | [Lorenz Meier](https://github.com/LorenzMeier) |
| Architecture | [Daniel Agar](https://github.com/dagar) / [Beat Küng](https://github.com/bkueng)|
| State Estimation | [Mathieu Bresciani](https://github.com/bresch) / [Paul Riseborough](https://github.com/priseborough) |
| OS/NuttX | [David Sidrane](https://github.com/davids5) |
| Drivers | [Daniel Agar](https://github.com/dagar) |
| Simulation | [Jaeyoung Lim](https://github.com/Jaeyoung-Lim) |
| ROS2 | [Beniamino Pozzan](https://github.com/beniaminopozzan) |
| Community QnA Call | [Ramon Roche](https://github.com/mrpollo) |
| [Documentation](https://docs.px4.io/main/en/) | [Hamish Willee](https://github.com/hamishwillee) |
| Vehicle Type | Maintainer |
|---|---|
| Multirotor | [Matthias Grob](https://github.com/MaEtUgR) |
| Fixed Wing | [Thomas Stastny](https://github.com/tstastny) |
| Hybrid VTOL | [Silvan Fuhrer](https://github.com/sfuhrer) |
| Rover | [Christian Friedrich](https://github.com/chfriedrich98) |
| Boat | x |
See also [maintainers list](https://px4.io/community/maintainers/) (px4.io) and the [contributors list](https://github.com/PX4/PX4-Autopilot/graphs/contributors) (Github). However it may be not up to date.
## Supported Hardware

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@ -1,68 +0,0 @@
#!/bin/sh
# Un comment and use set +e to ignore and set -e to enable 'exit on error control'
set +e
# Un comment the line below to help debug scripts by printing a trace of the script commands
#set -x
# PX4FMU startup script.
#
# NOTE: environment variable references:
# If the dollar sign ('$') is followed by a left bracket ('{') then the
# variable name is terminated with the right bracket character ('}').
# Otherwise, the variable name goes to the end of the argument.
#
#
# NOTE: COMMENT LINES ARE REMOVED BEFORE STORED IN ROMFS.
#
#------------------------------------------------------------------------------
set R /
#
# Print full system version.
#
ver all
#
# Set the parameter file the board supports params on
# MTD device.
#
if mft query -q -k MTD -s MTD_PARAMETERS -v /fs/mtd_params
then
set PARAM_FILE /fs/mtd_params
fi
#
# Load parameters.
#
# if the board has a storage for (factory) calibration data
if mft query -q -k MTD -s MTD_CALDATA -v /fs/mtd_caldata
then
param load /fs/mtd_caldata
fi
#
# Load parameters.
#
param select $PARAM_FILE
if ! param load
then
param reset_all
fi
#
# Try to mount the microSD card.
#
mount -t vfat /dev/mmcsd0 /fs/microsd
if [ $? = 0 ]
then
echo "SD card mounted at /fs/microsd"
else
echo "No SD card found"
fi
unset R
echo ""
echo "!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!"
echo "!!!!!! This is the PERFORMANCE TESTING firmware! WARNs and ERRORs are expected! !!!!!"
echo "!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!"
echo ""

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@ -0,0 +1,32 @@
#!/bin/sh
#
# @name 3DR Iris Quadrotor SITL (Obstacle Avoidance)
#
# @type Quadrotor Wide
#
. ${R}etc/init.d/rc.mc_defaults
param set-default CA_AIRFRAME 0
param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 0.1515
param set-default CA_ROTOR0_PY 0.245
param set-default CA_ROTOR0_KM 0.05
param set-default CA_ROTOR1_PX -0.1515
param set-default CA_ROTOR1_PY -0.1875
param set-default CA_ROTOR1_KM 0.05
param set-default CA_ROTOR2_PX 0.1515
param set-default CA_ROTOR2_PY -0.245
param set-default CA_ROTOR2_KM -0.05
param set-default CA_ROTOR3_PX -0.1515
param set-default CA_ROTOR3_PY 0.1875
param set-default CA_ROTOR3_KM -0.05
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
param set-default PWM_MAIN_FUNC3 103
param set-default PWM_MAIN_FUNC4 104
param set-default COM_OBS_AVOID 1

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@ -0,0 +1,2 @@
# shellcheck disable=SC2154
mavlink start -x -u 14558 -r 4000000 -m onboard -o 14541 -p # add mavlink stream for SDK

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@ -19,6 +19,7 @@ param set-default SENS_EN_BAROSIM 0
param set-default SENS_EN_MAGSIM 1
# Commander Parameters
param set-default COM_OBS_AVOID 0
param set-default COM_DISARM_LAND 0.5
# EKF2 parameters

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@ -11,39 +11,29 @@ PX4_SIM_MODEL=${PX4_SIM_MODEL:=r1_rover}
param set-default SIM_GZ_EN 1 # Gazebo bridge
param set-default NAV_ACC_RAD 0.5
# Differential Parameters
# Rover parameters
param set-default RD_WHEEL_TRACK 0.3
param set-default RD_MAX_ACCEL 5
param set-default RD_MAX_DECEL 10
param set-default RD_MAX_JERK 30
param set-default RD_MAX_THR_YAW_R 1.5
param set-default RD_YAW_RATE_P 0.25
param set-default RD_YAW_RATE_I 0.01
param set-default RD_YAW_P 5
param set-default RD_YAW_I 0.1
param set-default RD_MAX_SPEED 2
param set-default RD_MAX_THR_SPD 2.15
param set-default RD_SPEED_P 0.1
param set-default RD_SPEED_I 0.01
param set-default RD_MAX_YAW_RATE 180
param set-default RD_TRANS_DRV_TRN 0.349066
param set-default RD_TRANS_TRN_DRV 0.174533
param set-default RD_MAX_YAW_ACCEL 1000
# Rover Control Parameters
param set-default RO_ACCEL_LIM 5
param set-default RO_DECEL_LIM 10
param set-default RO_JERK_LIM 30
param set-default RO_MAX_THR_SPEED 2.1
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0.01
param set-default RO_YAW_RATE_P 0.25
param set-default RO_YAW_RATE_LIM 180
param set-default RO_YAW_ACCEL_LIM 120
param set-default RO_YAW_DECEL_LIM 1000
# Rover Attitude Control Parameters
param set-default RO_YAW_P 5
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 2
param set-default RO_SPEED_I 0.5
param set-default RO_SPEED_P 1
# Pure Pursuit parameters
# Pure pursuit parameters
param set-default PP_LOOKAHD_MAX 30
param set-default PP_LOOKAHD_MIN 2
param set-default PP_LOOKAHD_GAIN 1
param set-default PP_LOOKAHD_MAX 10
param set-default PP_LOOKAHD_MIN 1
# Simulated sensors
param set-default SENS_EN_GPSSIM 1

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@ -11,33 +11,23 @@ PX4_SIM_MODEL=${PX4_SIM_MODEL:=rover_ackermann}
param set-default SIM_GZ_EN 1 # Gazebo bridge
# Rover parameters
param set-default NAV_ACC_RAD 0.5
# Ackermann Parameters
param set-default RA_WHEEL_BASE 0.321
param set-default RA_ACC_RAD_GAIN 2
param set-default RA_ACC_RAD_MAX 3
param set-default RA_LAT_ACCEL_I 0.01
param set-default RA_LAT_ACCEL_P 0.1
param set-default RA_MAX_ACCEL 3
param set-default RA_MAX_DECEL 6
param set-default RA_MAX_JERK 15
param set-default RA_MAX_LAT_ACCEL 4
param set-default RA_MAX_SPEED 3
param set-default RA_MAX_STR_ANG 0.5236
param set-default RA_STR_RATE_LIM 360
# Rover Control Parameters
param set-default RO_ACCEL_LIM 3
param set-default RO_DECEL_LIM 6
param set-default RO_JERK_LIM 15
param set-default RO_MAX_THR_SPEED 3.1
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0.1
param set-default RO_YAW_RATE_P 1
param set-default RO_YAW_RATE_LIM 180
# Rover Attitude Control Parameters
param set-default RO_YAW_P 3
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 3
param set-default RO_SPEED_I 0.1
param set-default RO_SPEED_P 1
param set-default RA_MAX_STR_RATE 360
param set-default RA_MAX_THR_SPEED 3.1
param set-default RA_SPEED_I 0.01
param set-default RA_SPEED_P 0.1
param set-default RA_WHEEL_BASE 0.321
# Pure Pursuit parameters
param set-default PP_LOOKAHD_GAIN 1

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@ -39,6 +39,8 @@ px4_add_romfs_files(
1012_gazebo-classic_iris_rplidar
1013_gazebo-classic_iris_vision
1013_gazebo-classic_iris_vision.post
1014_gazebo-classic_iris_obs_avoid
1014_gazebo-classic_iris_obs_avoid.post
1015_gazebo-classic_iris_depth_camera
1016_gazebo-classic_iris_downward_depth_camera
1017_gazebo-classic_iris_opt_flow_mockup

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@ -337,11 +337,6 @@ then
payload_deliverer start
fi
if param compare -s ICE_EN 1
then
internal_combustion_engine_control start
fi
#user defined mavlink streams for instances can be in PATH
. px4-rc.mavlink

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@ -12,6 +12,7 @@
. ${R}etc/init.d/rc.mc_defaults
# Commander Parameters
param set-default COM_OBS_AVOID 1
param set-default COM_DISARM_LAND 0.5
# EKF2 parameters

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@ -12,6 +12,7 @@
. ${R}etc/init.d/rc.mc_defaults
# Commander Parameters
param set-default COM_OBS_AVOID 1
param set-default COM_DISARM_LAND 0.5
# EKF2 parameters

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@ -21,37 +21,26 @@ param set-default RBCLW_FUNC1 101
param set-default RBCLW_FUNC2 102
param set-default RBCLW_REV 1 # reverse right wheels
param set-default NAV_ACC_RAD 0.5
# Differential Parameters
# Rover parameters
param set-default RD_WHEEL_TRACK 0.3
param set-default RD_MAX_ACCEL 3
param set-default RD_MAX_DECEL 4
param set-default RD_MAX_JERK 5
param set-default RD_MAX_SPEED 1.6
param set-default RD_MAX_THR_SPD 1.9
param set-default RD_MAX_THR_YAW_R 0.7
param set-default RD_MAX_YAW_ACCEL 600
param set-default RD_MAX_YAW_RATE 250
param set-default RD_SPEED_P 0.1
param set-default RD_SPEED_I 0.01
param set-default RD_TRANS_DRV_TRN 0.785398
param set-default RD_TRANS_TRN_DRV 0.139626
param set-default RD_YAW_P 5
param set-default RD_YAW_I 0.1
param set-default RD_YAW_RATE_P 0.1
param set-default RD_YAW_RATE_I 0.01
# Rover Control Parameters
param set-default RO_ACCEL_LIM 3
param set-default RO_DECEL_LIM 4
param set-default RO_JERK_LIM 5
param set-default RO_MAX_THR_SPEED 1.9
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0.01
param set-default RO_YAW_RATE_P 0.1
param set-default RO_YAW_RATE_LIM 250
param set-default RO_YAW_ACCEL_LIM 600
param set-default RO_YAW_DECEL_LIM 600
# Rover Attitude Control Parameters
param set-default RO_YAW_P 5
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 1.6
param set-default RO_SPEED_I 0.01
param set-default RO_SPEED_P 0.1
# Pure Pursuit parameters
param set-default PP_LOOKAHD_GAIN 1
# Pure pursuit parameters
param set-default PP_LOOKAHD_MAX 10
param set-default PP_LOOKAHD_MIN 1
param set-default PP_LOOKAHD_GAIN 1

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@ -14,33 +14,24 @@
. ${R}etc/init.d/rc.rover_ackermann_defaults
param set-default BAT1_N_CELLS 3
param set-default NAV_ACC_RAD 0.5
# Ackermann Parameters
param set-default RA_WHEEL_BASE 0.321
# Rover parameters
param set-default NAV_ACC_RAD 0.5
param set-default RA_ACC_RAD_GAIN 2
param set-default RA_ACC_RAD_MAX 3
param set-default RA_LAT_ACCEL_I 0.01
param set-default RA_LAT_ACCEL_P 0.1
param set-default RA_MAX_ACCEL 1.5
param set-default RA_MAX_DECEL 10
param set-default RA_MAX_JERK 20
param set-default RA_MAX_LAT_ACCEL 3
param set-default RA_MAX_SPEED 2.5
param set-default RA_MAX_STR_ANG 0.5236
param set-default RA_STR_RATE_LIM 270
# Rover Control Parameters
param set-default RO_ACCEL_LIM 1.5
param set-default RO_DECEL_LIM 10
param set-default RO_JERK_LIM 20
param set-default RO_MAX_THR_SPEED 2.8
# Rover Rate Control Parameters
param set-default RO_YAW_RATE_I 0
param set-default RO_YAW_RATE_P 0
param set-default RO_YAW_RATE_LIM 0
# Rover Attitude Control Parameters
param set-default RO_YAW_P 0
# Rover Position Control Parameters
param set-default RO_SPEED_LIM 2.5
param set-default RO_SPEED_I 0.01
param set-default RO_SPEED_P 0.1
param set-default RA_MAX_STR_RATE 270
param set-default RA_MAX_THR_SPEED 2.8
param set-default RA_SPEED_I 0.01
param set-default RA_SPEED_P 0.1
param set-default RA_WHEEL_BASE 0.321
# Pure pursuit parameters
param set-default PP_LOOKAHD_GAIN 1

View File

@ -16,7 +16,6 @@ control_allocator start
fw_rate_control start
fw_att_control start
fw_pos_control start
fw_lat_lon_control start
airspeed_selector start
#

View File

@ -28,7 +28,6 @@ fi
fw_rate_control start vtol
fw_att_control start vtol
fw_pos_control start vtol
fw_lat_lon_control start vtol
fw_autotune_attitude_control start vtol
# Start Land Detector

View File

@ -555,11 +555,6 @@ else
payload_deliverer start
fi
if param compare -s ICE_EN 1
then
internal_combustion_engine_control start
fi
#
# Optional board supplied extras: rc.board_extras
#

View File

@ -136,6 +136,9 @@ class TestHardwareMethods(unittest.TestCase):
def test_atomic_bitset(self):
self.assertTrue(do_test(self.TEST_DEVICE, self.TEST_BAUDRATE, "atomic_bitset"))
def test_bezier(self):
self.assertTrue(do_test(self.TEST_DEVICE, self.TEST_BAUDRATE, "bezier"))
def test_bitset(self):
self.assertTrue(do_test(self.TEST_DEVICE, self.TEST_BAUDRATE, "bitset"))

View File

@ -8,12 +8,10 @@ if [ $# -gt 0 ]; then
fi
exec find boards msg src platforms test \
-path msg/translation_node -prune -o \
-path platforms/nuttx/NuttX -prune -o \
-path platforms/qurt/dspal -prune -o \
-path src/drivers/ins/vectornav/libvnc -prune -o \
-path src/drivers/uavcan/libdronecan -prune -o \
-path src/drivers/uavcan/libuavcan -prune -o \
-path src/drivers/uavcan/uavcan_drivers/kinetis/driver/include/uavcan_kinetis -prune -o \
-path src/drivers/cyphal/libcanard -prune -o \
-path src/lib/crypto/monocypher -prune -o \

View File

@ -1,76 +0,0 @@
#! /bin/bash
# Copy a git diff between two commits if msg versioning is added
DIR=$( cd "$( dirname "${BASH_SOURCE[0]}" )" && pwd )
PX4_SRC_DIR="$DIR/.."
BASE_COMMIT="$1"
HEAD_COMMIT="$2"
if [ -z "${BASE_COMMIT}" ] || [ -z "${HEAD_COMMIT}" ]
then
echo "Usage: $0 <base_commit> <head_commit>"
exit 1
fi
failed=0
# Iterate git diff files between BASE_COMMIT and HEAD_COMMIT
modified_files="$(git --no-pager diff --no-color --name-only --diff-filter=M "${BASE_COMMIT}"..."${HEAD_COMMIT}")"
all_files="$( git --no-pager diff --no-color --name-only "${BASE_COMMIT}"..."${HEAD_COMMIT}")"
for file in ${modified_files}
do
if [[ "$file" == msg/versioned/*.msg ]]; then
echo "Modified msg file: ${file}"
# A modified versioned .msg file requires:
# - Incrementing the version
# - An old .msg version exists
# - A translation header exists and is included
# Ignore changes to comments or constants
content_a=$(git show "${BASE_COMMIT}:${file}" | grep -o '^[^#]*' | grep -v =)
content_b=$(git show "${HEAD_COMMIT}:${file}" | grep -o '^[^#]*' | grep -v =)
if [ "${content_a}" == "${content_b}" ]; then
echo "No version update required for ${file}"
continue
fi
diff=$(git --no-pager diff --no-color --diff-filter=M "${BASE_COMMIT}"..."${HEAD_COMMIT}" -- "${file}")
old_version=$(echo "${diff}" | sed -n 's/^-uint32 MESSAGE_VERSION = \([0-9]*\).*/\1/p')
new_version=$(echo "${diff}" | sed -n 's/^+uint32 MESSAGE_VERSION = \([0-9]*\).*/\1/p')
# Check that the version is incremented
if [ -z "${new_version}" ] || [ -z "${old_version}" ]; then
echo "ERROR: Missing version update for ${file}"
failed=1
else
if [ $((new_version-old_version)) -ne 1 ]; then
echo "ERROR: Version not incremented by +1 for ${file}"
failed=1
fi
fi
# Check that an old version exists
filename=$(basename -- "$file")
filename="${filename%.*}"
old_version_file="px4_msgs_old/msg/${filename}V${old_version}.msg"
if [[ "${all_files}" != *"${old_version_file}"* ]]; then
echo "ERROR: Old message version does not exist for ${file} (missing ${old_version_file})"
failed=1
fi
# Check that a translation header got added by checking for a modification to all_translations.h
# If it is changed, we assume a new header got added too, so we don't explicitly check for that
if [[ "${modified_files}" != *"translations/all_translations.h"* ]]; then
echo "ERROR: missing modification to translations/all_translations.h"
failed=1
fi
fi
done
if [ ${failed} -ne 0 ]; then
echo ""
echo "ERROR: missing message versioning due to changed .msg file(s) (see above)"
echo "Check the documentation under https://docs.px4.io/main/en/ros2/px4_ros2_msg_translation_node.html for how to add a new version"
exit 1
fi

View File

@ -69,7 +69,7 @@ def process_target(px4board_file, target_name):
group = None
if px4board_file.endswith("default.px4board") or \
px4board_file.endswith("performance-test.px4board") or \
px4board_file.endswith("recovery.px4board") or \
px4board_file.endswith("bootloader.px4board"):
kconf.load_config(px4board_file, replace=True)
else: # Merge config with default.px4board

View File

@ -1,33 +0,0 @@
#! /bin/bash
# Copy msgs and the message translation node into a ROS workspace directory
DIR=$( cd "$( dirname "${BASH_SOURCE[0]}" )" && pwd )
PX4_SRC_DIR="$DIR/.."
WS_DIR="$1"
if [ ! -e "${WS_DIR}" ]
then
echo "Usage: $0 <ros_ws_dir>"
exit 1
fi
WS_DIR="$WS_DIR"/src
if [ ! -e "${WS_DIR}" ]
then
echo "'src' directory not found inside ROS workspace (${WS_DIR})"
exit 1
fi
cp -ar "${PX4_SRC_DIR}"/msg/translation_node "${WS_DIR}"
cp -ar "${PX4_SRC_DIR}"/msg/px4_msgs_old "${WS_DIR}"
PX4_MSGS_DIR="${WS_DIR}"/px4_msgs
if [ ! -e "${PX4_MSGS_DIR}" ]
then
git clone https://github.com/PX4/px4_msgs.git "${PX4_MSGS_DIR}"
rm -rf "${PX4_MSGS_DIR}"/msg/*.msg
rm -rf "${PX4_MSGS_DIR}"/msg/versioned/*.msg
rm -rf "${PX4_MSGS_DIR}"/srv/*.srv
fi
cp -ar "${PX4_SRC_DIR}"/msg/*.msg "${PX4_MSGS_DIR}"/msg
cp -ar "${PX4_SRC_DIR}"/msg/versioned/*.msg "${PX4_MSGS_DIR}"/msg
cp -ar "${PX4_SRC_DIR}"/srv/*.srv "${PX4_MSGS_DIR}"/srv

View File

@ -47,7 +47,6 @@ CCACHE_DIR=${HOME}/.ccache
mkdir -p "${CCACHE_DIR}"
docker run -it --rm -w "${SRC_DIR}" \
--user="$(id -u):$(id -g)" \
--env=AWS_ACCESS_KEY_ID \
--env=AWS_SECRET_ACCESS_KEY \
--env=BRANCH_NAME \
@ -55,6 +54,7 @@ docker run -it --rm -w "${SRC_DIR}" \
--env=CI \
--env=CODECOV_TOKEN \
--env=COVERALLS_REPO_TOKEN \
--env=LOCAL_USER_ID="$(id -u)" \
--env=PX4_ASAN \
--env=PX4_MSAN \
--env=PX4_TSAN \

View File

@ -74,7 +74,6 @@ exception_list_sitl = [
'SYSTEMCMDS_I2CDETECT', # Not supported in SITL
'SYSTEMCMDS_DMESG', # Not supported in SITL
'SYSTEMCMDS_USB_CONNECTED', # Not supported in SITL
'SYSTEMCMDS_MFT_CFG', # Not supported in SITL
'MODULES_SPACECRAFT', # Clashes with Control Allocation (mom's spaghetti code)
]

View File

@ -708,7 +708,7 @@ class uploader:
# https://github.com/PX4/Firmware/blob/master/src/drivers/boards/common/stm32/board_mcu_version.c#L125-L144
if self.fw_maxsize > fw.property('image_maxsize') and not force:
print(f"WARNING: Board can accept larger flash images ({self.fw_maxsize} bytes) than board config ({fw.property('image_maxsize')} bytes)")
raise RuntimeError(f"Board can accept larger flash images ({self.fw_maxsize} bytes) than board config ({fw.property('image_maxsize')} bytes). Please use the correct board configuration to avoid lacking critical functionality.")
else:
# If we're still on bootloader v4 on a Pixhawk, we don't know if we
# have the silicon errata and therefore need to flash px4_fmu-v2

View File

@ -1,5 +1,6 @@
#!/bin/bash
echo "[docker-entrypoint.sh] Starting entrypoint"
# Start virtual X server in the background
# - DISPLAY default is :99, set in dockerfile
# - Users can override with `-e DISPLAY=` in `docker run` command to avoid
@ -16,4 +17,17 @@ if [ -n "${ROS_DISTRO}" ]; then
source "/opt/ros/$ROS_DISTRO/setup.bash"
fi
exec "$@"
echo "[docker-entrypoint.sh] Working Directory: ${pwd}"
# Use the LOCAL_USER_ID if passed in at runtime
if [ -n "${LOCAL_USER_ID}" ]; then
echo "[docker-entrypoint.sh] Starting with: $LOCAL_USER_ID:user"
# modify existing user's id
usermod -u $LOCAL_USER_ID user
# run as user
# exec gosu user "$@"
exec "$@"
else
exec "$@"
fi

View File

@ -116,7 +116,6 @@ if [[ $INSTALL_NUTTX == "true" ]]; then
binutils-dev \
bison \
build-essential \
curl \
flex \
g++-multilib \
gcc-arm-none-eabi \

@ -1 +1 @@
Subproject commit 40deb719e3429098d808589dfa600b82d03439ea
Subproject commit db4af69088cccef4549cf3a5c195d5cd97d6b36a

View File

@ -42,7 +42,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -107,13 +107,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -47,7 +47,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -4,7 +4,7 @@
#------------------------------------------------------------------------------
param set-default CBRK_IO_SAFETY 0
param set-default MBE_ENABLE 0
param set-default MBE_ENABLE 1
param set-default SENS_IMU_CLPNOTI 0
safety_button start

View File

@ -7,7 +7,7 @@ param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_SUB_MBD 1
param set-default CANNODE_SUB_RTCM 1
param set-default GPS_1_GNSS 63
param set-default MBE_ENABLE 0
param set-default MBE_ENABLE 1
param set-default SENS_IMU_CLPNOTI 0
safety_button start

View File

@ -3,7 +3,6 @@
# board specific defaults
#------------------------------------------------------------------------------
param set-default MBE_ENABLE 0
param set-default SENS_IMU_CLPNOTI 0
pwm_out start

View File

@ -48,7 +48,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -150,13 +150,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -35,7 +35,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -145,13 +145,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -32,7 +32,7 @@ CONFIG_BOARD_LOOPSPERMSEC=95150
CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_CDCACM=y
CONFIG_CDCACM_IFLOWCONTROL=y
CONFIG_CDCACM_PRODUCTID=0x003A
CONFIG_CDCACM_PRODUCTID=0x0039
CONFIG_CDCACM_PRODUCTSTR="ARK BL Pi6X.x"
CONFIG_CDCACM_RXBUFSIZE=600
CONFIG_CDCACM_TXBUFSIZE=12000

View File

@ -76,7 +76,7 @@ CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_BUILTIN=y
CONFIG_CDCACM=y
CONFIG_CDCACM_IFLOWCONTROL=y
CONFIG_CDCACM_PRODUCTID=0x003A
CONFIG_CDCACM_PRODUCTID=0x0039
CONFIG_CDCACM_PRODUCTSTR="ARK Pi6X.x"
CONFIG_CDCACM_RXBUFSIZE=600
CONFIG_CDCACM_TXBUFSIZE=12000

View File

@ -141,13 +141,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -6,7 +6,7 @@
param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_SUB_MBD 1
param set-default CANNODE_SUB_RTCM 1
param set-default MBE_ENABLE 0
param set-default MBE_ENABLE 1
param set-default SENS_IMU_CLPNOTI 0
safety_button start

View File

@ -6,7 +6,7 @@
param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_SUB_MBD 1
param set-default CANNODE_SUB_RTCM 1
param set-default MBE_ENABLE 0
param set-default MBE_ENABLE 1
param set-default SENS_IMU_CLPNOTI 0
tone_alarm start

View File

@ -43,7 +43,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -94,13 +94,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -31,7 +31,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -43,7 +43,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -142,13 +142,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(io_timer_channel_get_gpio_output(i));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -51,7 +51,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -113,13 +113,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -51,7 +51,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -113,13 +113,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -49,7 +49,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -104,13 +104,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -50,7 +50,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -104,13 +104,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -47,7 +47,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -102,13 +102,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -33,7 +33,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -39,7 +39,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -100,13 +100,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -42,7 +42,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -100,13 +100,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -45,7 +45,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -144,13 +144,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -124,13 +124,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -46,7 +46,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -129,13 +129,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -46,7 +46,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -127,13 +127,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -46,7 +46,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -127,13 +127,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -51,7 +51,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -143,13 +143,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -31,7 +31,6 @@ CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y

View File

@ -94,13 +94,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -34,7 +34,6 @@ CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y

View File

@ -98,13 +98,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -33,7 +33,6 @@ CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y

View File

@ -94,13 +94,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -40,7 +40,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y

View File

@ -98,13 +98,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -41,7 +41,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y

View File

@ -98,13 +98,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -39,7 +39,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y

View File

@ -98,13 +98,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -50,7 +50,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -141,13 +141,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -41,7 +41,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -139,13 +139,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -13,7 +13,6 @@ CONFIG_DRIVERS_MAGNETOMETER_QMC5883L=y
CONFIG_DRIVERS_POWER_MONITOR_VOXLPM=y
CONFIG_DRIVERS_QSHELL_QURT=y
CONFIG_DRIVERS_RC_CRSF_RC=y
CONFIG_DRIVERS_VOXL2_IO=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_EKF2=y

View File

@ -47,7 +47,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

View File

@ -107,13 +107,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(io_timer_channel_get_as_pwm_input(i)));
}
/*
* On resets invoked from system (not boot) ensure we establish a low
* output state on PWM pins to disarm the ESC and prevent the reset from potentially
* spinning up the motors.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}

View File

@ -45,7 +45,6 @@ CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_LATERAL_LONGITUDINAL_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y

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