* PositionSetpoint: remove yaw_valid field
* Navigator: set yaw setpoint to NAN for Takeoff
Don't set a yaw setpoint for takeoff, as Navigator doesn't handle the yaw reset.
The yaw setpoint generation is handled by FlightTaskAuto.
* PositionSetpoint.msg: remove disable_weather_vane and instead only use the yaw field
Strictly follow the concept that if the position_setpoint.yaw is set, then
follow it the controller, and otherwise let the controller set it as it
thinks it's best.
* Navigator: remove logic that sets yaw to be accepted in TAKEOFF
No longer needed as during Takeoff we anyway don't set a yaw setpoint.
* PositionSetpoint.msg: remove yawspeed_valid
* PositionSetpoint.msg: remove yawspeed
* Navigator: set yaw setpoint to NAN instead of current
In set_takeoff and set_land_item, as well as for VTOL transition.
The flight tasks then set the yaw corresponding to the current yaw.
* Navigator: change get_yaw_acceptance into a bool
* PositionSetpoint.msg: improve comment for yaw
* MissionBlock: remove unnecessary code from set_vtol_transition_item
* Navigator: clean up calculate_breaking_stop(), set yaw to NAN
* Navigator: set yaw to NAN in variouls places where not specifc setpoint is desired
* Navigator: set yaw to NAN in reset_position_setpoint()
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Matthias Grob <maetugr@gmail.com>
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.
- update all msgs to be directly compatible with ROS2
- microdds_client improvements
- timesync
- reduced code size
- add to most default builds if we can afford it
- lots of other little changes
- purge fastrtps (I tried to save this multiple times, but kept hitting roadblocks)
Silvan Fuhrer
Konrad
Daniel Agar