A hierarchy-structured predictive control(HSPC) method is proposed according to the feature that hypersonic flight vehicle(HFV) model is highly nonlinear, fast-variability, coupling, and with parameters of great uncertainties. This method contains two parts, which are inner-loop nonlinear generable predictive control(NGPC) system and outer-loop NGPC system, respectively. These two NGPC systems are both designed by closed-form optimal generable predictive control(GPC) method. The HSPC system can ensure the longitudinal flight stability under the influence of uncertain parameters. Simulation studies demonstrate that the proposed control method is feasible for hypersonic flight vehicle.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Nonlinear Hierarchy-Structured Predictive Control System Design for Hypersonic Flight Vehicle



    Erschienen in:

    Erscheinungsdatum :

    2012-11-29


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Nonlinear Predictive Control with Sliding Mode for Hypersonic Vehicle

    Xiande Wu / Wenbin Bai / Yaen Xie et al. | DOAJ | 2023

    Freier Zugriff

    Flight Control Law Design with Hierarchy-Structured Dynamic Inversion Approach

    Kawaguchi, Jun-ichiro / Miyazawa, Yoshikazu / Ninomiya, Tetsujiro | AIAA | 2008


    Flight Control Design of Hypersonic Flight Experiment (HYFLEX) Vehicle

    Ishimoto, S. / Takizawa, M. / Suzuki, H. et al. | British Library Conference Proceedings | 1996