forked from Archive/PX4-Autopilot
protect from zero division
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6b2ad2e258
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@ -315,8 +315,12 @@ MultirotorMixer::mix(float *outputs, unsigned space, uint16_t *status_reg)
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// scale yaw if it violates limits. inform about yaw limit reached
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if (out < 0.0f) {
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yaw = -((roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) *
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if (fabsf(_rotors[i].yaw_scale) <= FLT_EPSILON) {
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yaw = 0.0f;
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} else {
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yaw = -((roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) *
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roll_pitch_scale + thrust + boost) / _rotors[i].yaw_scale;
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}
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if (status_reg != NULL) {
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(*status_reg) |= PX4IO_P_STATUS_MIXER_YAW_LIMIT;
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@ -326,8 +330,12 @@ MultirotorMixer::mix(float *outputs, unsigned space, uint16_t *status_reg)
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// allow to reduce thrust to get some yaw response
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float thrust_reduction = fminf(0.15f, out - 1.0f);
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thrust -= thrust_reduction;
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yaw = (1.0f - ((roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) *
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roll_pitch_scale + thrust + boost)) / _rotors[i].yaw_scale;
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if (fabsf(_rotors[i].yaw_scale) <= FLT_EPSILON) {
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yaw = 0.0f;
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} else {
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yaw = (1.0f - ((roll * _rotors[i].roll_scale + pitch * _rotors[i].pitch_scale) *
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roll_pitch_scale + thrust + boost)) / _rotors[i].yaw_scale;
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}
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if (status_reg != NULL) {
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(*status_reg) |= PX4IO_P_STATUS_MIXER_YAW_LIMIT;
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