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https://github.com/ArduPilot/ardupilot
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AC_AttitudeControl: revert AP_Math class change
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@ -434,7 +434,7 @@ void AC_AttitudeControl::frame_conversion_ef_to_bf(const Vector3f& ef_vector, Ve
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bool AC_AttitudeControl::frame_conversion_bf_to_ef(const Vector3f& bf_vector, Vector3f& ef_vector)
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{
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// avoid divide by zero
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if (AP_Math::is_zero(_ahrs.cos_pitch())) {
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if (is_zero(_ahrs.cos_pitch())) {
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return false;
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}
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// convert earth frame angle or rates to body frame
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@ -672,14 +672,14 @@ void AC_AttitudeControl::accel_limiting(bool enable_limits)
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{
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if (enable_limits) {
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// if enabling limits, reload from eeprom or set to defaults
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if (AP_Math::is_zero(_accel_roll_max)) {
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if (is_zero(_accel_roll_max)) {
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_accel_roll_max.load();
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}
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// if enabling limits, reload from eeprom or set to defaults
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if (AP_Math::is_zero(_accel_pitch_max)) {
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if (is_zero(_accel_pitch_max)) {
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_accel_pitch_max.load();
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}
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if (AP_Math::is_zero(_accel_yaw_max)) {
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if (is_zero(_accel_yaw_max)) {
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_accel_yaw_max.load();
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}
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} else {
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@ -742,7 +742,7 @@ float AC_AttitudeControl::get_boosted_throttle(float throttle_in)
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// sqrt_controller - response based on the sqrt of the error instead of the more common linear response
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float AC_AttitudeControl::sqrt_controller(float error, float p, float second_ord_lim)
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{
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if (AP_Math::is_zero(second_ord_lim) || AP_Math::is_zero(p)) {
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if (is_zero(second_ord_lim) || is_zero(p)) {
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return error*p;
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}
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@ -505,7 +505,7 @@ void AC_PosControl::get_stopping_point_xy(Vector3f &stopping_point) const
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float vel_total = pythagorous2(curr_vel.x, curr_vel.y);
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// avoid divide by zero by using current position if the velocity is below 10cm/s, kP is very low or acceleration is zero
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if (kP <= 0.0f || _accel_cms <= 0.0f || AP_Math::is_zero(vel_total)) {
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if (kP <= 0.0f || _accel_cms <= 0.0f || is_zero(vel_total)) {
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stopping_point.x = curr_pos.x;
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stopping_point.y = curr_pos.y;
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return;
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