- generate PWM_MAIN 1-14
- generate PWM_AUX 1-8
- generate PWM_EXTRA 1-8
- px4io and pwm_out directly read configuration parameters
- only available and active physical outputs are actually shown for configuration
- overall saves flash despite adding many new parameters
- control allocation module with multirotor, VTOL standard, and tiltrotor support
- angular_velocity_controller
- See https://github.com/PX4/PX4-Autopilot/pull/13351 for details
Co-authored-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Roman Bapst <bapstroman@gmail.com>
- commander preflightcheck use estimator_sensor_bias message instead of EKF state index magic number
- ekf2 publish estimated bias limits in estimator_sensor_bias
- preflightcheck only error if bias estimate exceeds half of configured limit (delete COM_ARM_EKF_AB and COM_ARM_EKF_GB parameters)
- in practice this is mostly useful for identifying incorrect rotations
which we mostly have in 45 degree increments
- handling a vehicle on the ground can easily disturb one mag by more than 30 degrees, so this is often distracting noise
- the values of the parameters GND_MAX_ANG and GND_WHEEL_BASE are outdated. They belonged to another Rover setup.
- in the mixer file rover_diff_and_servo.main.mix the steering was controlled by roll, but in PX4 rover steering is controlled by yaw. And this was the reason why the attitude control did not work correctly
- the DF Robot GPX:Asurada rover has actual a steering angle of 60 degrees. And and wheel base of 0.17m. Parameter values in the airframe file are changed to this values
Before #14212 the velocity control gains used in the multicopter
position controller were defined as a scale between velocity error in
one axis (or it's integral and derivative respectively) and the unit
thrust vector. The problem with this is that the normalization of the
unit thrust vector changes per vehicle or even vehicle configuration
as 0 and 100% thrust get a different physical response. That's why
the gains are now defined as scale between velocity error
(integral/derivative) and the output acceleration in m/s².
Jaeyoung-Lim
Beat Küng
Lorenz Meier
JacobCrabill
xdwgood
JaeyoungLim
Daniel Agar
Roman Dvořák
Jakub Kákona
TheLegendaryJedi
Julien Lecoeur
Silvan Fuhrer
Hamish Willee
Thies Lennart Alff
David Sidrane
Matthias Grob
Katrin Moritz
Daniel Leonard Robinson
Katrin
Stone White
斯东Stone