This paper addresses the autonomous landing control of FanWing. FanWing has good slow flight capability that shares certain fundamental features of both a fixed-wing aircraft and a rotary aircraft results in short take-off and landing (STOL) capability and no stall with a large angle of attack. FanWing is an aircraft configuration that uses a simple cross-flow fan mounted in the wing to provide distributed propulsion and augmented wing lift at very low flying speeds, leading to the high coupling of the attitude control and the altitude control. A control solution based on the pitch angle rate is proposed to obtain the pitch attitude stability control. And the combination control of the elevator and the fan wing is proposed to actualize the stability control of the longitudinal attitude and height control.


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    Titel :

    Automatic longitudinal landing control of FanWing


    Beteiligte:
    Meng, Lin (Autor:in) / Gao, Yang (Autor:in) / Zhang, Jiachao (Autor:in) / Jiao, Liangbao (Autor:in)

    Kongress:

    2nd International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2022) ; 2022 ; Guilin,China


    Erschienen in:

    Proc. SPIE ; 12244 ; 1224433


    Erscheinungsdatum :

    25.04.2022





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch