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.


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    Title :

    Novel control method for high aspect-ratio flying wing solar-powered airplane


    Contributors:
    SUN KANGWEN (author) / WANG RUOQIN (author) / SUN MINGXU (author) / SUN MOU (author)

    Publication date :

    2015-04-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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