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Copter: minor rename of ACRO circular limits variable
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@ -48,10 +48,10 @@ static void get_pilot_desired_angle_rates(int16_t roll_in, int16_t pitch_in, int
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Vector3f rate_ef_level, rate_bf_level, rate_bf_request;
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// apply circular limit to pitch and roll inputs
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float total_out = pythagorous2((float)pitch_in, (float)roll_in);
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float total_in = pythagorous2((float)pitch_in, (float)roll_in);
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if (total_out > ROLL_PITCH_INPUT_MAX) {
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float ratio = (float)ROLL_PITCH_INPUT_MAX / total_out;
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if (total_in > ROLL_PITCH_INPUT_MAX) {
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float ratio = (float)ROLL_PITCH_INPUT_MAX / total_in;
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roll_in *= ratio;
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pitch_in *= ratio;
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}
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