A terminal sliding mode controller is designed for a generic air-breathing hypersonic vehicles (AHVs). The model of AHVs is nonlinear, and includes uncertain parameters and intricate coupling between the engine and flight dynamics. An affine form of the longitudinal model is obtained by input/output linearization, and then a controller is designed by using terminal sliding mode method. The terminal sliding mode can make the system stabilize in finite time. Simulation results are provided to show the availability of the designed controller by excellent altitude and velocity tracking performance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Terminal sliding mode control design for air-breathing hypersonic vehicles


    Beteiligte:
    Xiaoxiang Hu, (Autor:in) / Changxing Ding, (Autor:in) / Ligang Wu, (Autor:in) / Changhua Hu, (Autor:in) / Hongyi Li, (Autor:in) / Yulin Si, (Autor:in) / Zeguo Wang, (Autor:in)


    Erscheinungsdatum :

    01.06.2010


    Format / Umfang :

    790313 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Adaptive Backstepping Sliding Mode Control of Air-Breathing Hypersonic Vehicles

    Shuo Wang / Ju Jiang / Chaojun Yu | DOAJ | 2020

    Freier Zugriff

    Adaptive Terminal Sliding Mode Control for Flexible Air-Breathing Hypersonic Vehicle

    Qin, Decong / Chen, Haibing / Lin, Wei et al. | AIAA | 2021


    Disturbance compensated terminal sliding mode control for hypersonic vehicles

    Xianfa, Z. / Xiaohu, W. / Jing, Z. et al. | British Library Online Contents | 2012