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Multicopter mixer - Rewrite unnecessarily complicated conditions
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@ -209,10 +209,10 @@ MultirotorMixer::mix(float *outputs, unsigned space)
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// which may result in motor saturation after thrust boost is applied
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// TODO: revise the saturation/boosting strategy
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if (min_out < 0.0f && max_out < 1.0f && -min_out <= 1.0f - max_out) {
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if (min_out < 0.0f && max_out < 1.0f && max_out - min_out <= 1.0f) {
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boost = -min_out;
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} else if (max_out > 1.0f && min_out > 0.0f && min_out >= max_out - 1.0f) {
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} else if (max_out > 1.0f && min_out > 0.0f && max_out - min_out <= 1.0f) {
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float max_thrust_diff = thrust - thrust_decrease_factor * thrust;
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if (max_thrust_diff >= max_out - 1.0f) {
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@ -223,12 +223,12 @@ MultirotorMixer::mix(float *outputs, unsigned space)
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roll_pitch_scale = (1 - (thrust + boost)) / (max_out - thrust);
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}
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} else if (min_out < 0.0f && max_out < 1.0f && -min_out > 1.0f - max_out) {
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} else if (min_out < 0.0f && max_out < 1.0f && max_out - min_out > 1.0f) {
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float max_thrust_diff = thrust * thrust_increase_factor - thrust;
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boost = math::constrain(-min_out - (1.0f - max_out) / 2.0f, 0.0f, max_thrust_diff);
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roll_pitch_scale = (thrust + boost) / (thrust - min_out);
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} else if (max_out > 1.0f && min_out > 0.0f && min_out < max_out - 1.0f) {
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} else if (max_out > 1.0f && min_out > 0.0f && max_out - min_out > 1.0f) {
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float max_thrust_diff = thrust - thrust_decrease_factor * thrust;
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boost = math::constrain(-(max_out - 1.0f - min_out) / 2.0f, -max_thrust_diff, 0.0f);
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roll_pitch_scale = (1 - (thrust + boost)) / (max_out - thrust);
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