Firstly, the conception of hypersonic flight and its flight characteristics are introduced in the article. Secondly, a control method based on the structured singular value theory is proposed, and the necessity of this method whether can be applied to design the hypersonic vehicle controller is discussed. And then taking a model for example, the robust controller of hypersonic vehicle is designed. At last, the control effect of this controller is proved better through the simulation result. It also turned out that the controller has excellent command track performance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Control Method of Hypersonic Vehicle Based on the Structured Singular Value Theory



    Erschienen in:

    Erscheinungsdatum :

    2011-10-24


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Singular Value and Structured Singular Value Bounds in Parameter Space

    Bajcinca, N. / Muhler, M. | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2002

    Freier Zugriff

    Computation of the real structured singular value

    CHANG, B.-C. / EKDAL, O. / YEH, H.H. et al. | AIAA | 1989


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

    Wang, Peng ;Liu, Lu Hua ;Wu, Jie | Trans Tech Publications | 2012


    Missile Flight Control with Dynamic Inversion and Structured Singular Value Synthesis

    D'Souza, C. / McFarland, M. / AIAA | British Library Conference Proceedings | 1994