because we need to have SITL simulation as realistic as possible
compared to a real flight with default settings such that we
either fix the problems or adjust the defaults already in SITL testing.
- avoids the need for ekf2_timestamp publications by q and lpe
- adds logger to the lockstep cycle and makes it poll on ekf2_timestamps
or vehicle_attitude. This avoids dropped samples (required for replay).
- IMU integration move from drivers (PX4Accelerometer/PX4Gyroscope) to sensors/vehicle_imu
- sensors: voted_sensors_update now consumes vehicle_imu
- delete sensor_accel_integrated, sensor_gyro_integrated
- merge sensor_accel_status/sensor_gyro_status into vehicle_imu_status
- sensors status output minor improvements (ordering, whitespace, show selected sensor device id and instance)
Before #14212 the velocity control gains used in the multicopter
position controller were defined as a scale between velocity error in
one axis (or it's integral and derivative respectively) and the unit
thrust vector. The problem with this is that the normalization of the
unit thrust vector changes per vehicle or even vehicle configuration
as 0 and 100% thrust get a different physical response. That's why
the gains are now defined as scale between velocity error
(integral/derivative) and the output acceleration in m/s².
- skip avionics rail voltage check when USB connected
- skip forced reboot on USB disconnect if circuit breaker set
- avionics voltage preflight check don't silently fail if system_power unavailble
- explicitly set supply check circuit breaker (CBRK_SUPPLY_CHK)
This adds a sitl target and aiframe configs for the r1_rover, which is a differential rover example for SITL rover. The model is based on the aion robotics r1 rover
-decrease L1 period for tighter mission tracking in fw mode
- increase backtransition duration, we can now do this is we have active
deceleration control
Signed-off-by: RomanBapst <bapstroman@gmail.com>
The implementation before this change had two timeouts, a hard-coded
timeout of 0.5 seconds as well as a by param configurable timeout with
certain failsafe actions set.
This change aims to fix two problems:
1. The hard-coded offboard timeout can be triggered easily with sped up
lockstep simulation. Since i t is hard-coded it can't be adapted to
the speed factor.
2. The offboard signal can time out but no action will be taken just
yet. This means we end up in an in-between stage where no warning or
failsafe action has happened yet, even though certain flags are set
to a timeout state.
This patch aims to fix this by unifying the two timeouts to the existing
configurable param. The convoluted double timeout logic is replaced by a
simple hysteresis.
For anyone that has previously not changed the default timeout param (0),
the param will now be changed to 0.5 seconds which reflects the
previously hardcoded time. For anyone with a specific timeout
configured, the behaviour should remain the same.
Also, going forward, timeouts lower than 0.5 seconds should be possible.
Sometimes in CI for VTOL we saw disarms before the spoolup and ramp were
over and the takeoff would actually happen. By raising the auto-disarm
time we should be able to work around this and get CI less flaky.
* add support for unmanned underwater vehicles:
* airframe uuv_generic + uuv_hippocammpus including mav_type = 12 for submarines
* mixer for UUVs with X-shaped thruster setup similar to quadcopter
* add module uuv_att_control for underwater robot attitude control
* add rc.uuv_defaults/apps for autostarting e.g. ekf2 and uuv_att_control app
This reverts commit be35c4857b.
This would only work for integer math, so for simulation speed-up. For
speeds slower than realtime we need floating point.
