This fixes the case where a new gimbal input gets lost in the output
throttling.
This is required because an input is potentially set only once and
then not computed again. In the failure case, control_data is set
to nullptr in subsequent calls and therefore not used for the output
calculation ever.
Adds MNT_DO_STAB for whether to stabilize by default.
Adds MNT_RANGE_{PITCH,ROLL,YAW} for the output range of each output channel in AUX mode (instead of hardcoded 360 degrees).
Adds MNT_OFF_{PITCH,ROLL,YAW} for adjusting the zero point of each output channel.
control_data needs to be able to be set to nullptr in case if the input
is already active. Otherwise the output will think there's always new
requests and reset it's state.
It is not convenient having to change a parameter to change a gimbal
from RC input to mavlink input mode or back. This refactor changes the
behaviour to use whatever is available, RC or mavlink commands.
Once a mavlink command is followed, control can be taken back using RC,
however, this requires a clear stick change.
This splits vmount into inputs and outputs modules with a small API in
between. It allows for greater flexibility, as any input method can be
combined with any output method. At the same time it is easy to add a new
input or output module.
MavLink spec implementation
implemented vehicle_roi topic
rename old gimbal to rc_gimbal
little changes
corrected RC Gimbal group
Starting ROI implementation in commander
implementation done, needs to be tested
uhm..
add todo
Change to float32 for x,y and z
remove mission topic again, not needed
change roi coordinates to lat, lon and alt
adjust to float64
starting mount implementation
correcting small mistakes, compiles now
add todos
further progress
implementing parameters
adjust default parameters
started implementation of mavlink
fix typo
change to lat, lon and alt
fix typo :D
change to double (to represent float64)
add global_position_
add mount topic
commander mount implementation done
cleanup
almost finished
little fix
codestyle fixes
leave pitch at 0 degrees
added pitch calculation
codestyle changes
Undo vehicle_mount, react to updated parameters, parsing of CMD_DO_MOUNT_* in mount.cpp
start implementing mode override
forgot a semikolon.
add debug
Finish implementation of mount override and manual control.
fix codestyle
correct cleanup
rename to vmount
works now
fix rebase error
fix polling
refactoring and custom airframe for gimbal
couple changes
remove warnx
almost done
finally
What is going on?
change back to actuator_controls_2
working
bump parameter version number and some clarification
fix submodules