This is done to test the recovery function of the estimator in case
of divergence or sudden extreme hover thrust change.
Also specify seed of random generator
with measurement noise auto-tuning
The purpose of this estimator is to improve land detection and vertical
velocity feedforward
Recovery strategy:
This is required when the setpoint suddenly changes in air or that the
EKF is diverging. A lowpassed test ratio is used as a trigger for the recovery logic
Also, a lowpassed residual is used to estimate the steady-state value
and remove it when estimating the accel noise to avoid increasing the
accel noise when the redisual is caused by an offset.
- it does nothing useful
- increases boot time by 2 seconds on pixhawk 4 due to a poll timeout:
IST8310 on I2C bus 3 at 0x0e (bus: 100 KHz, max: 400 KHz)
WARN [ist8310] ERROR: TIMEOUT 2
* 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
* Add param for software flow ctl on 3DR radios
* Dont reset telemetry type on radio timeout
* Treat 3DR radio as generic link type
* Rename 3DR to SiK radio
new versions of logger does not allow to log multiple instances of a topic when using 'logger_topics.txt'
This commit restores the default behavior (log all instances of a topic) and ad the option to specify an instance to log
This allows us to print an error message instead of a weird Java failure
further down the road.
Better yet would be if this would take down everything, so a user does
not have to scroll up to read the message.
These assignments were temporary for correct logging of the input
setpoint which now properly also comes out of the controller again.
This is reverting the hotfix from:
dee8d200d8bb42cd964065f9a6506e3c4a901f10
Removing the skip_controller and interfaceMapping
concept and replacing it with a single method checking
if the position control update was successful and
return the result in the PositionControl.update().
This restores original horizontal thrust setpoint execution
that I intentionally broke three commits ago. It's necessary
for correct stick to tilt mapping of FlightTaskManualAltitude.
This commit temporarily breaks direct horizontal thrust setpoint execution
which is used by FlightTaskManualAltitude. This is necessary to allow for
PositionControl cleanup namely calculating the whole velocity PID in one
Vector3f formula.
Having this in a separate commit is useful since it reduces indentation
of a bigger code block.
