Abstract
According to the basic principles of fixed-wing aircraft and multi-rotor design, combined with power requirement of the tilt tri-rotor UAV three flight modes, gives the tilt tri-rotor UAV power system model to solve the tilt tri-rotor UAV electric UAV power system matching problem, and to apply the theory completed a tilt tri-rotor UAV production, flight test was carried out to verify the theory. The experimental results analysis, tilt-rotor aircraft power system model in this paper can meet the general tilt rotor UAV power system design requirements. This achievement can provide theoretical references such UAV power system design.
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