Two sources:
1. global to local conversion was sometimes giving issues, so do everything in global
2. on startup the RTL didn't check if the home position was valid before processing it
- parameter updates can be quite expensive because they trigger nearly all modules to reload all of their parameters immediately
- limit modules from updating faster than once per second
Do not use LOITER_TO_ALT for rotary wing mode as it would then always climb to
at least MIS_LTRMIN_ALT, even if current clib altitude is below
(e.g. RTL immediately after take off)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- especially when there are strong winds it's better to just go straight
to the landing point instead of trying to follow the planned path
Signed-off-by: RomanBapst <bapstroman@gmail.com>
- if vtol and in rotary wing mode then don't execute the mission landing
because it's designed to be flow as a fixed wing
- if vtol and in rotary wing mode and mission land is available then fly directly
to landing point and don't go home!
Signed-off-by: RomanBapst <bapstroman@gmail.com>
- this fixes a race condition which happens when an RTL is triggered
during the final approach of a mission landing. In that case the mission inactive
method is never called.
Signed-off-by: RomanBapst <bapstroman@gmail.com>
- previously the decision of being on a landing pattern was taken by just
looking at the current mission index. However, even if the current mission
index indicates a landing pattern the vehicle could be at an arbitrary location, far
from being established on the pattern.
Signed-off-by: RomanBapst <bapstroman@gmail.com>
NAV_CMD_LOITER_TO_ALT
- this allows vtol to track the loiter circle during the transition instead
of trying to fly to the landing position
Signed-off-by: RomanBapst <bapstroman@gmail.com>
- this caused the navigator to use the next waypoint (after the vtol takeoff item)
to be used as target during the transition. If the altitude of that waypoint
was much higher than the takeoff altitude then there were FOH effects
after the transition which caused the vehicle to first descend before
climbing again.
Signed-off-by: RomanBapst <bapstroman@gmail.com>