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AC_AttControl: remove resolved To-Do 

This To-Do is resolved by heli flight modes calling the
relax_bf_rate_controller method
This commit is contained in:
Randy Mackay 2014-06-06 13:00:17 +09:00
parent 7f734f38d6
commit a662f87ffb
1 changed files with 0 additions and 4 deletions
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4
libraries/AC_AttitudeControl/AC_AttitudeControl.cpp
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@ -423,8 +423,6 @@ void AC_AttitudeControl::update_ef_roll_angle_and_error(float roll_rate_ef, Vect
angle_ef_error.x = wrap_180_cd(_angle_ef_target.x - _ahrs.roll_sensor);
angle_ef_error.x = constrain_float(angle_ef_error.x, -AC_ATTITUDE_RATE_STAB_ROLL_OVERSHOOT_ANGLE_MAX, AC_ATTITUDE_RATE_STAB_ROLL_OVERSHOOT_ANGLE_MAX);
// To-Do: handle check for traditional heli's motors.motor_runup_complete
// update roll angle target to be within max angle overshoot of our roll angle
_angle_ef_target.x = angle_ef_error.x + _ahrs.roll_sensor;
@ -441,8 +439,6 @@ void AC_AttitudeControl::update_ef_pitch_angle_and_error(float pitch_rate_ef, Ve
angle_ef_error.y = wrap_180_cd(_angle_ef_target.y - _ahrs.pitch_sensor);
angle_ef_error.y = constrain_float(angle_ef_error.y, -AC_ATTITUDE_RATE_STAB_PITCH_OVERSHOOT_ANGLE_MAX, AC_ATTITUDE_RATE_STAB_PITCH_OVERSHOOT_ANGLE_MAX);
// To-Do: handle check for traditional heli's motors.motor_runup_complete
// update pitch angle target to be within max angle overshoot of our pitch angle
_angle_ef_target.y = angle_ef_error.y + _ahrs.pitch_sensor;