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@ -274,7 +274,7 @@ void AP_MotorsSingle::output_armed_stabilizing()
@@ -274,7 +274,7 @@ void AP_MotorsSingle::output_armed_stabilizing()
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} |
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// limit thrust out for calculation of actuator gains
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float thrust_out_actuator = MAX(throttle_thrust_hover*0.5,_thrust_out); |
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float thrust_out_actuator = MAX(_throttle_hover*0.5,_thrust_out); |
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// force of a lifting surface is approximately equal to the angle of attack times the airflow velocity squared
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// static thrust is proportional to the airflow velocity squared
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