f4d7932503
lib/sensor_calibration: decrease gyro cal change threshold
2024-10-15 21:27:42 -04:00
dbba9adb14
lib/rc/ghst: Added differentiation between GHST and CRSF ( #23805 )
2024-10-11 16:17:54 -04:00
8b032d58d8
actuators/vertiq_io: module.yaml switched bit: values to 0-30 instead of starting at 32
2024-10-11 13:41:29 -04:00
01888a3085
mavlink: fix SET_MESSAGE_INTERVAL parsing ( #23796 )
...
This fixes the SITL tests that fail in CI because we catch NAN as non
zero after cast to int. To fix this I've added the check whether they
are finite at all.
The checks for param5 and param6 would be a bit trickier because they
can be int or float, so I have omitted them for now.
2024-10-11 09:03:22 +13:00
34f65682ad
Commander: remove -local- from failsafe string to make it simpler to understand
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com >
2024-10-10 10:28:59 +02:00
9cb12d8e8e
HealthAndArmingChecks: improve messaging for position estimate failure
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com >
2024-10-10 10:28:59 +02:00
da8827883f
Use target camera in image capture start/stop messages ( #23115 )
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* Use target camera in image capture start/stop messages
* Add support for MAV_CMD_SET_CAMERA_SOURCE
* Add target ID for NAV_CMD_SET_CAMERA_MODE
* Run make format
2024-10-09 21:10:08 +13:00
66b9e60a49
MAV_CMD_SET_MESSAGE_INTERVAL reject non-zero values for unused params ( #23643 )
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* MAV_CMD_SET_MESSAGE_INTERVAL reject non-zero values for unused params
* Remove data rate
* Replace rounding with addition of 0.5/0.5f
2024-10-09 21:08:49 +13:00
4a08ebafbc
failsafe: prevent immediate low battery failsafe for existing low battery state
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This happens when BAT_CRIT_THR allows arming with a critical battery level. With this change it still fails the checks but only warns instead of doing the failsafe action because that would immediately land the vehicle before it has taken off.
2024-10-08 18:49:23 +02:00
7941310afd
batteryCheck: allow COM_ARM_BAT_MIN to be set lower than BAT_CRIT_THR
...
Which still allows to arm the vehicle even if it already has a critical battery level.
2024-10-08 18:49:23 +02:00
a5b17f14b0
batteryCheck: refactor to consistent parameter variable naming
2024-10-08 18:49:23 +02:00
daf604b361
mavlink_mission: handle concurrent mission count messages
2024-10-08 15:34:51 +02:00
7ec4c1419c
mavlink_mission: only accept a mission request list on an ongoing transfer, when it is the same partner
2024-10-08 15:34:51 +02:00
b51ad07ed0
mavlink_mission: do not send the mission count if a new mission is detected since a receiver can now check this by changing mission ids in the MISSION_CURRENT stream
2024-10-08 15:34:51 +02:00
1c62dda057
mavlink_mission: make sure send mission item error ack is send to the right sysid/compid
2024-10-08 15:34:51 +02:00
b1d52e20c6
mavlink_mission: guard incoming misison item to be from the current transfer partner
2024-10-08 15:34:51 +02:00
ee19691d95
fix mission sysid for mission_ack
2024-10-08 15:34:51 +02:00
0d31226b1c
AirspeedSelector: enable sensor checks right after catapult launch
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Airspeed sensor failures are crucial to catch early during catapult/hand launches,
as otherwise the large airspeed error can lead to the vehicle diving. Thus the
_in_takeoff_situation flag, which tells the validator when to enable the checks,
is already set to false when !landed and launched.
For runway takeoffs the logic in unchanged.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com >
2024-10-08 13:16:17 +02:00
936eb89edb
logger: fixed watchdog not logging, increased cycle trigger ( #23769 )
2024-10-08 09:53:55 +02:00
fd04ece6d4
geo: remove dependency on drv_hrt time driver
2024-10-07 14:24:18 +02:00
f971c0e617
ekf2: reduce bad acc probation time 10s->3s
2024-10-07 10:37:33 +02:00
9ddac762e3
ekf2: stricter GNSS vel rejected innovation override
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- in the special case of bad vertical acceleration detected
(bad_acc_vertical) only allow overriding rejected GNSS 3D velocity
if horizontal innovations are accepted
2024-10-07 10:36:09 +02:00
9238656a33
ekf2: configurable velocity state constraint (EKF2_VEL_LIM)
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- replace hardcoded 1000 m/s velocity state constraint with new EKF2_VEL_LIM parameter (default 100 m/s)
- new velocity limit also used for GPS checks and external vision velocity
2024-10-07 10:35:48 +02:00
4215e20120
modules/time_persistor: new time persistor module to save time to persistent storage ( #23760 )
2024-10-04 15:44:49 -04:00
7d0e93b779
ekf2: always publish global position when origin has been set
2024-10-04 11:41:20 -04:00
ad28c5893b
flight_mode_manager: invalidate dist to bottom/ground on terrain reset
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- this allows the terrain hold to simply reset on the next valid update
rather than trying to adjust the setpoints
2024-10-04 11:28:03 -04:00
34ee097f02
ekf2: tighten terrain validity requirements
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- require valid fusion from a range finder or optical flow before
considering terrain valid again
2024-10-04 10:31:20 +02:00
5b85859bfe
Update submodule libevents to latest Wed Oct 2 12:39:22 UTC 2024
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- libevents in PX4/Firmware (c4ab09d088798a97b80f2cb834b2345e26d485ea): https://github.com/mavlink/libevents/commit/9474657606d13301d426e044450c4f84de2221be
- libevents current upstream: https://github.com/mavlink/libevents/commit/7c1720749dfe555ec2e71d5f9f753e6ac1244e1c
- Changes: https://github.com/mavlink/libevents/compare/9474657606d13301d426e044450c4f84de2221be...7c1720749dfe555ec2e71d5f9f753e6ac1244e1c
7c17207 2024-08-21 Beat Küng - remove nlohmann json submodule and add header directly instead
ce60064 2024-08-16 Jonas Vautherin - Fix cmake_minimum_required
2024-10-02 15:09:53 -04:00
51702efe94
boards: update all NuttX defconfigs
2024-10-02 15:08:38 -04:00
98e2aaf5f0
Update submodule iq-module-communication-cpp to latest Wed Oct 2 12:39:13 UTC 2024
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- iq-module-communication-cpp in PX4/Firmware (6c9c62f70c4c1b8e5b9703efc96919856465e65e): https://github.com/PX4/iq-module-communication-cpp/commit/a9b700d50bdd06a837c74750ac3c4760937333df
- iq-module-communication-cpp current upstream: https://github.com/PX4/iq-module-communication-cpp/commit/c488af4e8807de80739aa48efd2ea51614dd8195
- Changes: https://github.com/PX4/iq-module-communication-cpp/compare/a9b700d50bdd06a837c74750ac3c4760937333df...c488af4e8807de80739aa48efd2ea51614dd8195
c488af4 2024-08-13 Ben Quan - Merged in development (pull request #22 )
0e9f7cd 2024-08-06 Fred Kummer - Merged in feature/add-led-support (pull request #21 )
acf5be0 2024-08-05 Fred Kummer - Fix indent
c5ef8d9 2024-08-05 Fred Kummer - Fix green blue order
64d0654 2024-08-05 Fred Kummer - Fix indentation
833cef7 2024-08-05 Fred Kummer - Add led support headers
2024-10-02 15:08:20 -04:00
6119b08ef4
mpc: reset integrators when controllers are not used
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Starting with a non-zero integrator could appear as a strong disturbance
when engaging position mode.
2024-10-02 10:47:25 -04:00
dbf51da99e
ekf2: rework amsl to ellipsoid altitude conversion
2024-10-01 10:40:18 -04:00
5bfa6b3359
ekf2: remove redundant ned_origin_initialised flag
2024-10-01 10:37:20 -04:00
fe40ccd193
EKF2: publish wind after external wind init ( #23747 )
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* publish wind after external wind init
* move ext-wind-init to estimator-interface
* Update src/modules/ekf2/EKF/estimator_interface.h
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com >
* Update src/modules/ekf2/EKF/estimator_interface.h
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com >
---------
Co-authored-by: Mathieu Bresciani <brescianimathieu@gmail.com >
2024-10-01 14:33:30 +02:00
8aec2d7c9f
GPS: add velocity fields to Unicore
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It looks like vertical velocity as well as velocity accuracy are not
available using NMEA, so we extract all velocities from the Unicore
ACRICA message instead.
2024-10-01 13:47:06 +13:00
4e359f9552
set file descriptor to -1 after close() ( #23751 )
2024-09-30 13:22:46 -06:00
602042dd5c
failure detector use per index esc current
2024-09-30 10:11:34 +02:00
332b7bec27
commander: ignore REQUEST_CAMERA_INFORMATION
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- add answer command logging
2024-09-27 10:33:37 -07:00
8fdf0931e5
Commander framework: only warn and do not re-start RTL if already in RTL
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com >
2024-09-27 14:25:27 +02:00
224aef142c
Retry logic in uxrce_dds_client startup ( #23723 )
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* Added retries if uxrce_dds_client fails during setup
* Break timesync endless loop in case of agent reset
* ORB unsubscribe, to avoid too many open fails with multiple reconnects & format
* Added review feedback
2024-09-26 17:43:49 +02:00
0e65679c9e
Mecanum rover: add dedicated module for mecanum rovers ( #23708 )
2024-09-25 09:35:41 +02:00
06dfc4b782
drivers/actuators: new vertiq_io driver ( #22892 )
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* brought in the Vertiq Cpp API as a submodule. updated the serial rx handling so that we can parse out IQUART data packets
---------
Co-authored-by: Luca Scheuer <scheuer.luca@gmail.com >
2024-09-24 11:44:35 -04:00
5ffe9c6de4
drivers/gnss/septentrio: disable default assignment of GPS1
2024-09-24 11:24:34 -04:00
35efe44a6b
ekf2: fusion always succeeds, do not return boolean
2024-09-24 10:48:14 -04:00
23f343aa3a
ekf2-rng: consider height covariance for terrain reset to range
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Range does not provide a direct terrain observation but a measurement
relative to the height state. Correlation between height and terrain
must be set properly.
2024-09-24 10:18:25 -04:00
d269ddfb49
sensors/vehicle_air_data: fix air data publication rate ( #23717 )
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Co-authored-by: Nicolas Martin <n.martin@elistair.com >
2024-09-24 09:49:47 -04:00
454ded1b25
EKF2: ev-vel refactoring ( #23577 )
2024-09-24 14:09:11 +02:00
21a2350eca
version: Change this IF statement to a SWITCH statement
2024-09-24 10:27:12 +02:00
f60bb2c6bc
rtl_direct: skip loiter altitude items for multicopter without RTL land delay ( #23689 )
...
This was already done before the refactor and was assumed to not be necessary.
The problem is that these mission items result in a strang looking vertical slow down directly followed
by an acceleration during the landing phase.
2024-09-23 18:33:03 +02:00
8afd267509
move more ekf function implementations to cpp
2024-09-23 12:18:41 -04:00
Daniel Agar