This is a rework so that servos.cpp is responsible for setting the
throttle limits under more circumstances and always notifies TECS when
it does so.
Additionally, the TAKEOFF mode has been improved with a new parameters
TKOFF_MODE and TKOFF_THR_MIN that extend the throttle behaviour.
This variable updated unpredictably, and it was easy to introduce bugs.
It was not used in many places and is clearer to calculate the error
directly when needed.
* Set position target used to just be used in scripting, now it's used
by DDS in external control
Signed-off-by: Ryan Friedman <ryanfriedman5410+github@gmail.com>
this fixes a bug where if the terrain database cache does not have the
tile for the location of a rally point then RTL to the rally point
with TERRAIN_FOLLOW=1 will not track terrain
The underlying issue is that Location::loc.change_alt_frame() will
return false if the location is not in the terrain memory cache. We
can't just extrapolate as the rally point could be in a totally
different terrain area to the current location. So instead we set it
as terrain_following_pending and fix it as soon as the terrain cache
is filled.
fixes https://github.com/ArduPilot/ardupilot/issues/25157
this fixes a bug where a change of home altitude would cause a sudden
height demand change. This copes with 3 situations:
- flying with AMSL alt demand. Changing home altitude makes for no change
- flying with AGL alt demand. Changing home altitude requires update of next_WP_loc
- flying with home relative alt demand. Changing home altitude changes demand at end of current navigation leg
The code had a bug where if GPS fix was lost, the demanded airspeed would be set to the measured or estimated airspeed causing unpredictable variations in the demanded airspeed.
This patch prevents the minimum ground speed protection speed up from running if the ground speed undershoot cannot be calculated.
This patch extends the range of conditions over which the minimum ground speed functionality can be used by enabling the ground speed undershoot to be calculated when the navigation system is able to estimate velocity.
The check for the aircraft being lined up for a tangent exit has an early breakout condition if the next waypoint is too close to the loiter circle which can prevent the required ground course to waypoint ever being achieved. This check was using the WP_LOITER_RAD parameter value, not the actual radius being used which can be set differently by the mission plan. If a large value for WP_LOITER_RAD was set and being over-written by the mission plan with a smaller value compatible with the distance to the next waypoint, the aircraft would still exit early.
timtuxworth
Peter Barker
Iampete1
George Zogopoulos
Henry Wurzburg
Andrew Tridgell
Bob Long
Tom Pittenger
Ryan Friedman
Mykhailo Kuznietsov
Zach Flathers
Paul Riseborough