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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
306 changed files with 6992 additions and 10356 deletions
+1 -1
View File
@@ -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=${{ env.RUNS_ON_S3_BUCKET_CACHE }},mode=max
@@ -1,52 +0,0 @@
name: ROS Translation Node Tests
on:
push:
branches:
- 'main'
pull_request:
branches:
- '*'
defaults:
run:
shell: bash
jobs:
build_and_test:
name: Build and test
runs-on: [runs-on,runner=8cpu-linux-x64,image=ubuntu24-full-x64,"run-id=${{ 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
Vendored
+2 -2
View File
@@ -235,9 +235,9 @@ pipeline {
sh('rm -f px4_msgs/srv/*.srv')
sh('rm -f px4_msgs/srv/versioned/*.srv')
sh('cp msg/*.msg px4_msgs/msg/')
sh('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')
-42
View File
@@ -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
|------|--------|------|----------------------
| | | |
+5 -1
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
+23 -2
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
@@ -0,0 +1,32 @@
#!/bin/sh
#
# @name 3DR Iris Quadrotor SITL (Obstacle Avoidance)
#
# @type Quadrotor Wide
#
. ${R}etc/init.d/rc.mc_defaults
param set-default CA_AIRFRAME 0
param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 0.1515
param set-default CA_ROTOR0_PY 0.245
param set-default CA_ROTOR0_KM 0.05
param set-default CA_ROTOR1_PX -0.1515
param set-default CA_ROTOR1_PY -0.1875
param set-default CA_ROTOR1_KM 0.05
param set-default CA_ROTOR2_PX 0.1515
param set-default CA_ROTOR2_PY -0.245
param set-default CA_ROTOR2_KM -0.05
param set-default CA_ROTOR3_PX -0.1515
param set-default CA_ROTOR3_PY 0.1875
param set-default CA_ROTOR3_KM -0.05
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
param set-default PWM_MAIN_FUNC3 103
param set-default PWM_MAIN_FUNC4 104
param set-default COM_OBS_AVOID 1
@@ -0,0 +1,2 @@
# shellcheck disable=SC2154
mavlink start -x -u 14558 -r 4000000 -m onboard -o 14541 -p # add mavlink stream for SDK
@@ -19,6 +19,7 @@ param set-default SENS_EN_BAROSIM 0
param set-default SENS_EN_MAGSIM 1
# Commander Parameters
param set-default COM_OBS_AVOID 0
param set-default COM_DISARM_LAND 0.5
# EKF2 parameters
@@ -11,39 +11,29 @@ PX4_SIM_MODEL=${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
@@ -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
@@ -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
-5
View File
@@ -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
@@ -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
@@ -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
@@ -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
@@ -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
-5
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
#
+3
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"))
@@ -8,12 +8,10 @@ if [ $# -gt 0 ]; then
fi
exec find boards msg src platforms test \
-path msg/translation_node -prune -o \
-path platforms/nuttx/NuttX -prune -o \
-path platforms/qurt/dspal -prune -o \
-path src/drivers/ins/vectornav/libvnc -prune -o \
-path src/drivers/uavcan/libdronecan -prune -o \
-path src/drivers/uavcan/libuavcan -prune -o \
-path src/drivers/uavcan/uavcan_drivers/kinetis/driver/include/uavcan_kinetis -prune -o \
-path src/drivers/cyphal/libcanard -prune -o \
-path src/lib/crypto/monocypher -prune -o \
-76
View File
@@ -1,76 +0,0 @@
#! /bin/bash
# Copy a git diff between two commits if msg versioning is added
DIR=$( 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 [ ${failed} -ne 0 ]; then
echo ""
echo "ERROR: missing message versioning due to changed .msg file(s) (see above)"
echo "Check the documentation under https://docs.px4.io/main/en/ros2/px4_ros2_msg_translation_node.html for how to add a new version"
exit 1
fi
-33
View File
@@ -1,33 +0,0 @@
#! /bin/bash
# Copy msgs and the message translation node into a ROS workspace directory
DIR=$( 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
+1 -1
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="$(id -u)" \
--env=PX4_ASAN \
--env=PX4_MSAN \
--env=PX4_TSAN \
+1 -1
View File
@@ -708,7 +708,7 @@ class uploader:
# https://github.com/PX4/Firmware/blob/master/src/drivers/boards/common/stm32/board_mcu_version.c#L125-L144
if self.fw_maxsize > fw.property('image_maxsize') and not force:
print(f"WARNING: Board can accept larger flash images ({self.fw_maxsize} bytes) than board config ({fw.property('image_maxsize')} bytes)")
raise RuntimeError(f"Board can accept larger flash images ({self.fw_maxsize} bytes) than board config ({fw.property('image_maxsize')} bytes). Please use the correct board configuration to avoid lacking critical functionality.")
else:
# If we're still on bootloader v4 on a Pixhawk, we don't know if we
# have the silicon errata and therefore need to flash px4_fmu-v2
+15 -1
View File
@@ -1,5 +1,6 @@
#!/bin/bash
echo "[docker-entrypoint.sh] Starting entrypoint"
# Start virtual X server in the background
# - DISPLAY default is :99, set in dockerfile
# - Users can override with `-e DISPLAY=` in `docker run` command to avoid
@@ -16,4 +17,17 @@ if [ -n "${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
-1
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 -6
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);
}
}
+1 -1
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
@@ -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
@@ -3,7 +3,6 @@
# board specific defaults
#------------------------------------------------------------------------------
param set-default MBE_ENABLE 0
param set-default SENS_IMU_CLPNOTI 0
pwm_out start
+1 -6
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);
}
}
+1 -6
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);
}
}
@@ -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
+1 -1
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
+1 -6
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);
}
}
@@ -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
+1 -1
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
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
@@ -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
+1 -6
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);
}
}
+1 -6
View File
@@ -132,13 +132,8 @@ __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);
}
}
+1 -6
View File
@@ -132,13 +132,8 @@ __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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+5 -5
View File
@@ -106,13 +106,13 @@ __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.
/**
* On resets invoked from system (not boot) insure we establish a low
* output state (discharge the pins) on PWM pins before they become inputs.
*/
if (status >= 0) {
up_mdelay(100);
up_mdelay(6);
}
}
+1 -6
View File
@@ -120,13 +120,8 @@ 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);
}
}
+1 -6
View File
@@ -120,13 +120,8 @@ 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);
}
}
+1 -6
View File
@@ -134,13 +134,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(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);
}
}
+1 -6
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);
}
}
+1 -6
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);
}
}
+1 -6
View File
@@ -137,13 +137,8 @@ __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);
}
}
+1 -6
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);
}
}
+1 -6
View File
@@ -145,13 +145,8 @@ __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);
}
}
+1 -6
View File
@@ -153,13 +153,8 @@ __EXPORT void board_on_reset(int status)
px4_arch_configgpio(PX4_MAKE_GPIO_INPUT(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);
}
}
+1 -3
View File
@@ -11,9 +11,7 @@ CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=n
CONFIG_MODULES_MC_POS_CONTROL=n
CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_MODULES_ROVER_ACKERMANN=n
CONFIG_MODULES_ROVER_DIFFERENTIAL=n
CONFIG_MODULES_ROVER_MECANUM=n
CONFIG_MODULES_DIFFERENTIAL_DRIVE=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
CONFIG_MODULES_CONTROL_ALLOCATOR=n
CONFIG_MODULES_SPACECRAFT=y
+1 -6
View File
@@ -136,13 +136,8 @@ __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);
}
}
@@ -142,13 +142,8 @@ __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);
}
}
+1 -6
View File
@@ -125,13 +125,8 @@ __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);
}
}
+1 -6
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);
}
}
+1 -6
View File
@@ -144,13 +144,8 @@ __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);
}
}
@@ -0,0 +1,88 @@
{
"fileType": "Plan",
"geoFence": {
"circles": [
],
"polygons": [
],
"version": 2
},
"groundStation": "QGroundControl",
"mission": {
"cruiseSpeed": 15,
"firmwareType": 12,
"hoverSpeed": 5,
"items": [
{
"AMSLAltAboveTerrain": null,
"Altitude": 4,
"AltitudeMode": 0,
"autoContinue": true,
"command": 22,
"doJumpId": 1,
"frame": 3,
"params": [
0,
0,
0,
null,
47.3977432,
8.5456085,
4
],
"type": "SimpleItem"
},
{
"AMSLAltAboveTerrain": null,
"Altitude": 4,
"AltitudeMode": 0,
"autoContinue": true,
"command": 16,
"doJumpId": 2,
"frame": 3,
"params": [
0,
0,
0,
null,
47.3977432,
8.5458765,
4
],
"type": "SimpleItem"
},
{
"AMSLAltAboveTerrain": null,
"Altitude": -1,
"AltitudeMode": 0,
"autoContinue": true,
"command": 21,
"doJumpId": 3,
"frame": 3,
"params": [
0,
0,
0,
null,
47.3977432,
8.5458812,
-1
],
"type": "SimpleItem"
}
],
"plannedHomePosition": [
47.3977419,
8.5458854,
487.923
],
"vehicleType": 2,
"version": 2
},
"rallyPoints": {
"points": [
],
"version": 2
},
"version": 1
}
+2
View File
@@ -5,4 +5,6 @@ float32 indicated_airspeed_m_s # indicated airspeed in m/s
float32 true_airspeed_m_s # true filtered airspeed in m/s
float32 air_temperature_celsius # air temperature in degrees Celsius, -1000 if unknown
float32 confidence # confidence value from 0 to 1 for this sensor
+8
View File
@@ -0,0 +1,8 @@
uint64 timestamp # time since system start (microseconds)
uint8 len # length of data
uint32 MAX_BUFLEN = 128
uint8[128] data # data
# TOPICS voxl2_io_data
+11 -8
View File
@@ -48,6 +48,7 @@ set(msg_files
AirspeedValidated.msg
AirspeedWind.msg
AutotuneAttitudeControlStatus.msg
Buffer128.msg
ButtonEvent.msg
CameraCapture.msg
CameraStatus.msg
@@ -113,7 +114,6 @@ set(msg_files
HeaterStatus.msg
HoverThrustEstimate.msg
InputRc.msg
InternalCombustionEngineControl.msg
InternalCombustionEngineStatus.msg
IridiumsbdStatus.msg
IrlockReport.msg
@@ -171,13 +171,12 @@ set(msg_files
RateCtrlStatus.msg
RcChannels.msg
RcParameterMap.msg
RoverAttitudeSetpoint.msg
RoverAttitudeStatus.msg
RoverVelocityStatus.msg
RoverRateSetpoint.msg
RoverRateStatus.msg
RoverSteeringSetpoint.msg
RoverThrottleSetpoint.msg
RoverAckermannGuidanceStatus.msg
RoverAckermannSetpoint.msg
RoverAckermannStatus.msg
RoverDifferentialGuidanceStatus.msg
RoverDifferentialSetpoint.msg
RoverDifferentialStatus.msg
RoverMecanumGuidanceStatus.msg
RoverMecanumSetpoint.msg
RoverMecanumStatus.msg
@@ -211,6 +210,8 @@ set(msg_files
TelemetryStatus.msg
TiltrotorExtraControls.msg
TimesyncStatus.msg
TrajectoryBezier.msg
TrajectoryWaypoint.msg
TransponderReport.msg
TuneControl.msg
UavcanParameterRequest.msg
@@ -230,6 +231,8 @@ set(msg_files
VehicleRoi.msg
VehicleThrustSetpoint.msg
VehicleTorqueSetpoint.msg
VehicleTrajectoryBezier.msg
VehicleTrajectoryWaypoint.msg
VelocityLimits.msg
WheelEncoders.msg
Wind.msg
-2
View File
@@ -20,5 +20,3 @@ float32[4] q
float32 angular_velocity_x
float32 angular_velocity_y
float32 angular_velocity_z
uint8 ORB_QUEUE_LENGTH = 2
-8
View File
@@ -1,8 +0,0 @@
uint64 timestamp # time since system start (microseconds)
bool ignition_on # activate/deactivate ignition (Spark Plug)
float32 throttle_control # [0,1] - Motor should idle with 0. Includes slew rate if enabled.
float32 choke_control # [0,1] - 1 fully closes the air inlet.
float32 starter_engine_control # [0,1] - control value for electric starter motor.
uint8 user_request # user intent for the ICE being on/off
+2
View File
@@ -7,4 +7,6 @@ float32 target_bearing # Bearing angle from aircraft to current target [rad]
float32 xtrack_error # Signed track error [m]
float32 wp_dist # Distance to active (next) waypoint [m]
float32 acceptance_radius # Current horizontal acceptance radius [m]
float32 yaw_acceptance # Yaw acceptance error[rad]
float32 altitude_acceptance # Current vertical acceptance error [m]
uint8 type # Current (applied) position setpoint type (see PositionSetpoint.msg)
+6
View File
@@ -0,0 +1,6 @@
uint64 timestamp # time since system start (microseconds)
float32 lookahead_distance # [m] Lookahead distance of pure the pursuit controller
float32 heading_error # [deg] Heading error of the pure pursuit controller
# TOPICS rover_ackermann_guidance_status
+9
View File
@@ -0,0 +1,9 @@
uint64 timestamp # time since system start (microseconds)
float32 forward_speed_setpoint # [m/s] Desired speed in body x direction. Positiv: forwards, Negativ: backwards
float32 forward_speed_setpoint_normalized # [-1, 1] Desired normalized speed in body x direction. Positiv: forwards, Negativ: backwards
float32 steering_setpoint # [rad] Desired steering angle
float32 steering_setpoint_normalized # [-1, 1] Desired normalized steering angle
float32 lateral_acceleration_setpoint # [m/s^2] Desired acceleration in body y direction. Positiv: right, Negativ: left.
# TOPICS rover_ackermann_setpoint
+11
View File
@@ -0,0 +1,11 @@
uint64 timestamp # time since system start (microseconds)
float32 measured_forward_speed # [m/s] Measured speed in body x direction. Forwards: positiv, Backwards: negativ
float32 adjusted_forward_speed_setpoint # [m/s] Speed setpoint after applying slew rate
float32 steering_setpoint_normalized # [-1, 1] Normalized steering setpoint
float32 adjusted_steering_setpoint_normalized # [-1, 1] Normalized steering setpoint after applying slew rate
float32 measured_lateral_acceleration # [m/s^2] Measured acceleration in body y direction. Positiv: right, Negativ: left.
float32 pid_throttle_integral # Integral of the PID for the closed loop speed controller
float32 pid_lat_accel_integral # Integral of the PID for the closed loop lateral acceleration controller
# TOPICS rover_ackermann_status
-5
View File
@@ -1,5 +0,0 @@
uint64 timestamp # time since system start (microseconds)
float32 yaw_setpoint # [rad] Expressed in NED frame
# TOPICS rover_attitude_setpoint
-6
View File
@@ -1,6 +0,0 @@
uint64 timestamp # time since system start (microseconds)
float32 measured_yaw # [rad/s] Measured yaw rate
float32 adjusted_yaw_setpoint # [rad/s] Yaw setpoint that is being tracked (Applied slew rates)
# TOPICS rover_attitude_status
+7
View File
@@ -0,0 +1,7 @@
uint64 timestamp # time since system start (microseconds)
float32 lookahead_distance # [m] Lookahead distance of pure the pursuit controller
float32 heading_error_deg # [deg] Heading error of the pure pursuit controller
uint8 state_machine # Driving state of the rover [0: SPOT_TURNING, 1: DRIVING, 2: GOAL_REACHED]
# TOPICS rover_differential_guidance_status
+9
View File
@@ -0,0 +1,9 @@
uint64 timestamp # time since system start (microseconds)
float32 forward_speed_setpoint # [m/s] Desired forward speed for the rover
float32 forward_speed_setpoint_normalized # [-1, 1] Normalized forward speed for the rover
float32 yaw_rate_setpoint # [rad/s] Desired yaw rate for the rover (Overriden by yaw controller if yaw_setpoint is used)
float32 speed_diff_setpoint_normalized # [-1, 1] Normalized speed difference between the left and right wheels
float32 yaw_setpoint # [rad] Desired yaw (heading) for the rover
# TOPICS rover_differential_setpoint
+14
View File
@@ -0,0 +1,14 @@
uint64 timestamp # time since system start (microseconds)
float32 measured_forward_speed # [m/s] Measured speed in body x direction. Forwards: positiv, Backwards: negativ
float32 adjusted_forward_speed_setpoint # [m/s] Speed setpoint after applying slew rate
float32 measured_yaw # [rad] Measured yaw
float32 adjusted_yaw_setpoint # [rad] Yaw setpoint after applying slew rate
float32 clyaw_yaw_rate_setpoint # [rad/s] Yaw rate setpoint output by the closed loop yaw controller
float32 measured_yaw_rate # [rad/s] Measured yaw rate
float32 adjusted_yaw_rate_setpoint # [rad/s] Yaw rate setpoint from the closed loop yaw controller
float32 pid_yaw_integral # Integral of the PID for the closed loop yaw controller
float32 pid_yaw_rate_integral # Integral of the PID for the closed loop yaw rate controller
float32 pid_throttle_integral # Integral of the PID for the closed loop speed controller
# TOPICS rover_differential_status
-5
View File
@@ -1,5 +0,0 @@
uint64 timestamp # time since system start (microseconds)
float32 yaw_rate_setpoint # [rad/s] Expressed in NED frame
# TOPICS rover_rate_setpoint

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