The invention provides a novel control method for a high aspect-ratio flying wing solar-powered airplane. Through a steering engine, the tension line direction of a vector motor is controlled, the rotating speed of the motor is controlled and the deflection of a control surface is adjusted, so that the flying state of the airplane is controlled; and complicated control system and sensing system are simplified, so as to achieve the function of controlling the airplane. According to the control method, stable control on the high aspect-ratio flying wing solar-powered airplane can be finished; the control system can be simplified; the structure weight can be reduced; the working load of the airplane is improved; and the control reliability of the airplane is increased.
Novel control method for high aspect-ratio flying wing solar-powered airplane
2015-04-29
Patent
Electronic Resource
English
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