The invention provides a drone aircraft flight control system and method. The drone aircraft flight control system comprises a flight execution unit, a sensor unit and a flight control unit. By means of the relation existing among the wing area, the drone aircraft lift force and the flight rotating speed, the swing angle of a leading edge flap and a leading edge flap is controlled strictly, so that power consumption of an aircraft engine is reduced while enough drone aircraft lift force is ensured.


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    Titel :

    Drone aircraft flight control system and method


    Beteiligte:
    WANG YOUCHUANG (Autor:in) / SONG YUCHENG (Autor:in) / XIU HONGMING (Autor:in) / WANG GUOLONG (Autor:in) / ZHU PING (Autor:in) / LIAO HUALONG (Autor:in)

    Erscheinungsdatum :

    2015-11-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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