The invention belongs to the technical field of aircrafts, and particularly relates to a novel jet-propelled vertical take-off and landing aircraft and a nonlinear control method thereof. The aircraft comprises an aircraft fuselage, aircraft racks, an aircraft control system, a micro turbojet engine, an aircraft thrust vector system and an aircraft power supply system, the aircraft fuselage is fixedly connected with the aircraft racks, and the four aircraft racks are arranged at the four corners of the aircraft fuselage; the four micro turbojet engines are respectively fixed at the tail end of the aircraft frame, and the aircraft control system is arranged on the aircraft body and is connected with the aircraft thrust vector system and the aircraft power supply system through an external circuit and an oil path.

    本发明属于飞行器技术领域,更具体地,涉及一种新型喷气式垂直起降飞行器及其非线性控制方法。该飞行器包括飞行器机身、飞行器机架、飞行器控制系统、微型涡喷发动机、飞行器推力矢量系统和飞行器动力供应系统,飞行器机身与飞行器机架固定连接,四个飞行器机架设置在飞行器机身的四个角,四个微型涡喷发动机分别固定在飞行器机架的末端,飞行器控制系统设置在飞行器机身上,并通过外部电路和油路与飞行器推力矢量系统和飞行器动力供应系统连接。


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    Titel :

    Novel jet-propelled vertical take-off and landing aircraft and nonlinear control method thereof


    Weitere Titelangaben:

    新型喷气式垂直起降飞行器及其非线性控制方法


    Beteiligte:
    DUAN FENG (Autor:in) / YIN YANKAI (Autor:in) / KANG FEI (Autor:in) / HE MAOCHANG (Autor:in)

    Erscheinungsdatum :

    2022-09-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT