0be38ef424
set yaw to NAN
2025-02-21 12:12:28 -09:00
347d4e0c1b
fix implicit conversion
2025-02-13 12:35:37 -09:00
de997f93c2
navigator: loiter: allow without global position
2025-02-13 12:20:11 -09:00
98cba19f50
esc_battery: report temperature
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Co-authored-by: Jacob Dahl <37091262+dakejahl@users.noreply.github.com >
2025-02-11 21:17:53 -05:00
975ec30c9c
uxrce_dds_client: add DDS message versioning
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This adds "_v" + string(T::MESSAGE_VERSION) to the ROS topic if the message
contains a MESSAGE_VERSION field (and the version is non-zero).
2025-02-11 13:19:25 +01:00
136f9f48fc
FW Position controller: transform RWTO_PSP to rad when used ( #24312 )
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Signed-off-by: Silvan <silvan@auterion.com >
2025-02-11 12:12:11 +01:00
2b75d2e738
run fog check independently from stuck check
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-02-11 09:08:25 +01:00
8cedef2dc4
further cleanup
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-02-11 09:08:25 +01:00
2c4d38e303
fixed mistake
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-02-11 09:08:25 +01:00
806500fc4a
further improve logic
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-02-11 09:08:25 +01:00
73ade6d05c
range finder: remove potential deadlock
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-02-11 09:08:25 +01:00
35da86c85a
improve unit tests for range fog detection
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-02-11 09:08:25 +01:00
55f51d7e7e
ackermann: refactor code architecture
2025-02-10 15:54:24 +01:00
ce64263ce7
publish validated airspeed topic ( #24302 )
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* publish validated airspeed topic
* fix typo
2025-02-07 14:44:48 +01:00
69d95a6664
sf45: separate sensor yaw variable into FRD and sensor frames for clarity.
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Obstacle map is created in sensor frame, but scaling for vehicle orientation is done in vehicle FRD frame.
2025-02-07 13:28:17 +01:00
093b379b6b
sf45/collision-prevention: replace repeated code with ObstacleMath library functions.
2025-02-07 13:28:17 +01:00
e7e76e2e21
Spacecraft build and bare control allocator ( #24221 )
2025-02-06 23:54:24 -05:00
de1ade8eb8
sensors/vehicle_air_data: only trigger the sensor fallback when the baro_fault flag switches from 0 -> 1
2025-02-06 23:47:32 -05:00
8d296a50f9
FlightTask: properly initialize EKF reset counters
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This fixes a race condition when switching from a flight mode that is
not a flight task (e.g.: stabilized). In this case, the reset counters
were initialized to 0 and deltas were applied to the first setpoints if
the EKF had any of its reset counters different from 0.
2025-02-05 13:21:32 -05:00
bd2a009217
commander: remove MC nav test
2025-02-05 11:58:04 -05:00
9e5cfa330a
Commander: Quick calibration supports mag too
2025-02-04 21:58:03 -05:00
48c0992a7d
sf45: refactor how sensor orientation (yaw_cfg) correction is applied to incoming sensor data.
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yaw_cfg is now read into the obstacle_distance message as the angle_offset. The offset is computed once at init and applied to each measurement.
2025-02-03 17:17:35 +01:00
31bff3e5bb
sf45: change handle_missed_bins() function logic.
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To simplify logic for wrap-around cases and cases in which bins outside the FOV may be filled. Bin indices are offset such that the 0th bin is the first bin within the sensor FOV. This way we can always fill bins from smallest to largest index.
2025-02-03 17:17:35 +01:00
cb332e047d
obstacle-math: add standard obstacle map functions.
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These functions help simplify repeated calculations accross driver and collision prevention files that are computing bins, angles and sensor offsets in obstacle maps.
2025-02-03 17:17:35 +01:00
f7dadd9b89
Remove inclusion of rotors in library to enable test ( #24286 )
2025-02-03 15:51:55 +01:00
a9214b3aa3
gimbal: don't spoof gimbal device ( #24271 )
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The current approach was wrong because the gimbal protocol now
handles the case properly where the autopilot is in charge of a
non-MAVLink gimbal.
This means that we don't need to send message "as if we were a gimbal
device" and instead set thet gimbal_device_id to 1 (up to 6) to indicate
we are in charge or a non-MAVLink gimbal.
2025-01-31 12:59:41 +13:00
4c2e69b2e6
estimatorCheck: only warn about GPS in modes that require a position but fail all modes if GPS required by configuration
2025-01-30 18:45:10 +01:00
f142363575
HealthAndArmingChecks: allow to warn in certain modes and fail arming checks in other modes
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Previously it was only possible to warn in all modes and fail none or fail and warn in certain modes.
2025-01-30 18:45:10 +01:00
3b828e157a
MC att: clarify prioritization algorithm
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Especially rename "mix" which is just the delta yaw angle
2025-01-30 11:28:26 +01:00
ddf591c4f5
Navigator: use FLT_EPSILON instead of 0.0001f for >0 float comparison
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Signed-off-by: Silvan <silvan@auterion.com >
2025-01-29 15:42:51 +01:00
2f2e56c097
Navigator: replace custom NAV_EPSILON_POSITION with FLT_EPSILON
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Signed-off-by: Silvan <silvan@auterion.com >
2025-01-29 15:42:51 +01:00
7e47605871
batteryCheck: separate event messages for low, critical and emergency battery states
2025-01-29 15:32:47 +01:00
41c4933e10
add standard vtol airframe
2025-01-29 11:15:00 +01:00
a0a2bdaea5
commander: COM_MODE_ARM_CHK parameter to allow mode registration while armed ( #24249 )
2025-01-28 14:33:15 +01:00
4df65c133e
add cs_baro_fault to switch to fallback baro if available ( #24260 )
2025-01-28 10:37:16 +01:00
5bca71791a
SIH: clean up control surface configuration ( #24205 )
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* fix sign error in appropriate place
In PR https://github.com/PX4/PX4-Autopilot/pull/24175 I changed the
control surface deflection signs in generate_fw_aerodynamics to make the
1103 airframe work correctly. However, this breaks the 1101 airframe,
introducing sing errors there.
So, here the change in generate_fw_aerodynamics is reverted to the state
before PR #24175 . Instead, the signs are set correctly by using
the HIL_ACT_REV bitfield in the respective airframe config files.
* match control surface parameters to SIH model
2025-01-27 16:52:29 +01:00
165f644580
control_allocator: fix typo and use [0,1] instead of [0%, 100%] in slew rate description
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Co-authored-by: Hamish Willee <hamishwillee@gmail.com >
2025-01-27 08:43:11 +01:00
c1cab2d4e0
control_allocator: add unit for slew rate and reword description
2025-01-27 08:43:11 +01:00
c76e74338b
ekf-replay: fix airspeed replay
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If available, the EKF uses airspeed_validated, not airspeed
2025-01-26 23:05:39 -05:00
c3ba39f931
dshot: remove dshot 1200
2025-01-23 23:50:50 -05:00
07e7c64e60
drivers/power_monitor/ina238: retry if read fails
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* ina238: retry if read fails
* ina238: increase retries and only publish not connected if register check fails
* ina238: use I2C resets
2025-01-22 15:32:26 -05:00
045c8d9831
Mission feasibility checks: make adding new check less error prone ( #24241 )
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* make adding new feasibility checks less prone to errors
Signed-off-by: RomanBapst <bapstroman@gmail.com >
* Update src/modules/navigator/MissionFeasibility/FeasibilityChecker.hpp
Co-authored-by: Silvan Fuhrer <silvan@auterion.com >
---------
Signed-off-by: RomanBapst <bapstroman@gmail.com >
Co-authored-by: Silvan Fuhrer <silvan@auterion.com >
2025-01-22 16:56:31 +01:00
57fdda597b
vtol_takeoff: store altitude on takeoff and don't use home position altitude
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as vehicle does not need to be close to home position
Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-01-22 14:03:18 +03:00
ee150a15b4
Optical Flow: add unit testes for only using downward distance sensor ( #23266 )
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* Test for Optical Flow checks correct camera position
* Formatting fixed
* Update src/modules/sensors/vehicle_optical_flow/test/CMakeLists.txt
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com >
* Update src/modules/sensors/vehicle_optical_flow/test/VehicleOpticalFlowTest.cpp
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com >
* Update src/modules/sensors/vehicle_optical_flow/test/VehicleOpticalFlowTest.cpp
Co-authored-by: Silvan Fuhrer <silvan@auterion.com >
* For test GIVEN/WHEN/THEN added
---------
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com >
Co-authored-by: Silvan Fuhrer <silvan@auterion.com >
2025-01-22 11:58:07 +01:00
caaae6ed51
ekf2: allow sideslip fusion to always start with airspeed fusion
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This allow sideslip fusion to start during VTOL front transition or even
on a multirotor with a vertical stabilizer and an airspeed sensor for example.
2025-01-22 09:33:16 +01:00
1900d2c98f
uavcan: fix hw_errors from mutex lock, hide ESC/Servo status if no function set ( #23888 )
2025-01-22 12:48:05 +13:00
a3215419d7
gz: remove model spawn offset ( #24165 )
2025-01-22 12:47:25 +13:00
918eca8de4
gz: increase timeout for service request ( #24164 )
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* gz: increase timeout for service request
* change error messages to warnings, specify retrying
* fix typo
2025-01-21 22:14:38 +01:00
f36b45b2ff
VehicleOpticalFlow: use 32bit integer for dt
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-01-21 16:48:33 +03:00
25e76883b7
Integrator: use 32bit integer to store dt to avoid overflow
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Signed-off-by: RomanBapst <bapstroman@gmail.com >
2025-01-21 16:48:33 +03:00
Jacob Dahl