ardupilot/libraries/AC_AttitudeControl
Tom Pittenger 3adf8c3e51 AC_AttitudeControl: comment odd math in get_att_target_euler_cd
degree(100) = 1 float multiplicaiton
vector3f * degree(100.0f)  = 4 float multiplications
degree(vector3f) * 100.0f  = 6 float multiplications and needs new degree(vector3f) function
degree(vector3f * 100.0f)  = 6 float multiplications and needs new degree(vector3f) function

These all come to the same conclusion but the one that is faster appears to be a bug but is mathematically correct.
2016-09-27 17:04:53 -07:00
..
AC_AttitudeControl_Heli.cpp AC_AttitudeControl: enhanced quaternion attitude controller 2016-06-24 17:17:11 +09:00
AC_AttitudeControl_Heli.h AC_AttitudeControl: enhanced quaternion attitude controller 2016-06-24 17:17:11 +09:00
AC_AttitudeControl_Multi.cpp AC_AttControl: add parameter check of throttle mix 2016-09-02 09:27:15 +09:00
AC_AttitudeControl_Multi.h AC_AttControl: add parameter check of throttle mix 2016-09-02 09:27:15 +09:00
AC_AttitudeControl.cpp AC_AttControl: reduce max_rate_step based on hover throttle 2016-08-12 22:29:53 +09:00
AC_AttitudeControl.h AC_AttitudeControl: comment odd math in get_att_target_euler_cd 2016-09-27 17:04:53 -07:00
AC_PosControl.cpp AC_PosControl: check Z-axis accel imax can always overpower hover throttle 2016-09-05 14:19:43 +09:00
AC_PosControl.h AC_PosControl: add get_horizontal_error 2016-07-12 18:40:25 +09:00
ControlMonitor.cpp AC_AttitudeControl: added accessors for P and D RMS controller values 2016-06-10 17:48:31 +10:00