At hypersonic speed, strong nonlinear couplings will bring enormous challenges to the attitude control of a hypersonic flight vehicle. To reduce the negative impacts of the couplings, a hierarchical coordinated controller is proposed for a generic hypersonic vehicle in this paper. By using a statistical sampling method, a series of coupling analyses between any two different attitude variables groups are studied firstly, and the matrices that describe the coupling degrees are provided. Based on the coupling degree matrices, two coordinated controllers are designed for the attitude angles and angular rates, respectively. The simulation results indicate that the proposed controller can effectively coordinate the coupling impacts, and achieve smooth attitude tracking.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Coordinated attitude control of hypersonic flight vehicles based on the coupling analysis


    Beteiligte:
    Zhen, Wubin (Autor:in) / Wang, Yuhui (Autor:in) / Wu, Qingxian (Autor:in) / Shao, Peng (Autor:in)


    Erscheinungsdatum :

    2018-04-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Finite-Time Attitude Tracking Control for Hypersonic Flight Vehicles with Actuator Saturation

    Teng Cao / Huajun Gong / Huiyunuo Xiao et al. | DOAJ | 2022

    Freier Zugriff

    MHD flight control for hypersonic vehicles

    Robinson, Wesley / Gerwin, Richard | AIAA | 2001



    MHD Flight Control System for Hypersonic Vehicles

    Robinson, W. / Gerwin, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2001