* 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
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.
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>
- in the special case of bad vertical acceleration detected
(bad_acc_vertical) only allow overriding rejected GNSS 3D velocity
if horizontal innovations are accepted
- 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
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.
* 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
* brought in the Vertiq Cpp API as a submodule. updated the serial rx handling so that we can parse out IQUART data packets
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Co-authored-by: Luca Scheuer <scheuer.luca@gmail.com>
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.
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.
* fixes to restart the state machine if sensor does not init correctly
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
* fixes
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
* increase fail count
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
* remove extra flush, switch from warn to debug, add enum states for sensor bring-up
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
* remove dead code, decrease restart fail count metric, break out of loop with consec errors if over the fail count and not init
Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
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Signed-off-by: dirksavage88 <dirksavage88@gmail.com>
* Added AUAV absolute pressure sensing
* Moved func to abstract base class
* Probe and params
* Fixed arg parsing and added auto start
* refactorings
* Added sample perf
* Fixed CI findings
* Simplified rc.sensors condition
Hamish Willee