Before:
When the mixed throttle for the motor was exactly zero the ramp went
from the disarmed PWM value to the minimum PWM value.
When the throttle was even just slightly different from zero the ramp
made a jump up to the commanded throttle scaled between
disarmed PWM and maximum PWM, then ramped between
disarmed PWM and minimum PWM and at the end jumped up again to
the commanded throttle scaled between minimum PWM and maximum PWM.
After:
The ramp goes from disarmed PWM value to the the
commanded throttle scaled between minimum PWM and maximum PWM.
If the commanded throttle changes during the ramp then the scale and
hence also end value of the ramp changes.
- Instead we disable interrups on Nuttx where needed
- No lock is held during param export. Params can be changed
concurrently and we rely on the fact that another export will be
triggered in that case.
* RateControl: rename setGains to setPidGains to be more precise
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
* FW Rate controller: only allow to disable Yaw in Acro, not roll and pitch
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- if the height rate input into TECS is finite, use that one to
update a velocity reference generator
- if the velocity reference generator reports position locked or
height rate input is not finite, then run altidue reference generator
- run altitude controller only if altitue is controlled
if height_rate_setpoint is set, only use that one to update altitdue trajectory
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
* FWPositionController: add linear airspeed-to-trim-throttle mapping
Scale trim throttle in a linear way with airspeed.
Different gradients above/below trim airspeed.
The airspeed- and airs density-corrected trim throttle is required for an accurate
throttle prediction in TECS, while the default trim throttle is still needed
as well, as the throttle delta from height rate setpoint delta is linked to it.
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
to enable proper automatic output in gtest unit tests
that compare two `Matrix`, `Vector` or two `Dual` objects.
Credits to @jwidauer for showing me this trick.
- add unit tests for adsb conflict detection
- move adsb conflict detection to lib/adsb and adsb conflict class
- use containers/Array.hpp for buffer array
- expand fake_traffic
* [npfg]: Remove the guideToPoint function and replace with guideToPath
* [npfg]: remove unused navigateXXX functions
* [npfg]: Move navigateXXX Function into FWPoscontrol
* [FixedwingPositionControl]: Set default flaps and spoilers in attitude setpoint topic, and only change if necessary.
Matthias Grob