Reduces flash usage by ~16KB.
- compress formats at build-time into a single string with all formats
- then at runtime iteratively decompress using
https://github.com/atomicobject/heatshrink
- if not in air the accel noise is doubled
- if landed don't init unless GPS velocity is non-negligible
- when inactive continue seeding with EKF gyro bias
- reset yaw estimator if GPS fusion is stopped
Has options *None where the check is disabled, and *Warning, where only a warning is
published (which replaces the high wind warning from the COM_WIND_WARN limit).
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
* started tiltrotor port
* added advanced plane and changed some parameters on the tiltrotor
* added advanced plane
* removed tiltrotor for clean push
* removed standard vtol old model file
* removing the standard vtol changes from this PR, since it is not part of the advanced plane
* removed advanced plane meshes as they are already found in the rc_cessna
* updating and improving airframe parameters
* updated mesh paths
Signed-off-by: frederik <frederik@auterion.com>
---------
Signed-off-by: frederik <frederik@auterion.com>
Co-authored-by: frederik <frederik@auterion.com>
There is no reason to keep an uncertainty on the origin as it is then
already contained in the local position estimate when GNSS data is fused
in the filter.
The command is sent by a dedicated mavlink command and forwarded to the fixed wing position controller.
The pattern is defined by the radius of the major axis, the radius of the minor axis and the orientation. The pattern is then defined by:
The upper part of the pattern consist of a clockwise circle with radius defined by the minor axis. The center of the circle is defined by the major axis minus the minor axis away from the pattern center.
The lower part of the pattern consist of a counter-clockwise circle with the same definitions as above.
In between, the circles are connected with straight lines in a cross configuration. The lines are always tangetial to the circles.
The orientation rotates the major axis around the NED down axis.
The loitering logic is defined inside its own class used by the fixed wing position control module. It defines which segment (one of the circles or lines) is active and uses the path controller (npfg or l1-control) to determine the desired roll angle.
A feedback mavlink message is send with the executed pattern parameters.
