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AC_AttitudeControl: add comment
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@ -552,6 +552,7 @@ void AC_AttitudeControl::update_rate_bf_targets()
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_rate_bf_target.z = _p_angle_yaw.kP() * _angle_bf_error.z;
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_rate_bf_target.z = _p_angle_yaw.kP() * _angle_bf_error.z;
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}
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}
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// include roll and pitch rate required to account for precession of the desired attitude about the body frame yaw axes
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_rate_bf_target.x += _angle_bf_error.y * _ahrs.get_gyro().z;
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_rate_bf_target.x += _angle_bf_error.y * _ahrs.get_gyro().z;
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_rate_bf_target.y += -_angle_bf_error.x * _ahrs.get_gyro().z;
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_rate_bf_target.y += -_angle_bf_error.x * _ahrs.get_gyro().z;
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}
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}
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