This paper describes the design of a nonlinear controller for an air- breathing hypersonic vehicle. To overcome the analytical intractability of this model, a nominal control-oriented model is used to derive the control law. The nominal model has unstable zero dynamics with respect to the output to be controlled, namely flight path angle and velocity, and presents intricate couplings between the engine dynamics and flight dynamics. The flexible effects have not been included in the analysis yet. Adaptive control techniques and robust control techniques are applied to achieve tracking of velocity and altitude trajectories. Simulation results are provided to show that the derived control law allows to achieves excellent tracking performance on the nominal model.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Nonlinear Robust/Adaptive Controller Design for an Air-Breathing Hypersonic Vehicle Model (Preprint)


    Beteiligte:
    L. Fiorentini (Autor:in) / A. Serrani (Autor:in) / M. A. Bolender (Autor:in) / D. B. Doman (Autor:in)

    Erscheinungsdatum :

    2006


    Format / Umfang :

    19 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Nonlinear Robust/Adaptive Controller Design for an Air-Breathing Hypersonic Vehicle Model

    Fiorentini, Lisa / Serrani, Andrea / Bolender, Michael et al. | AIAA | 2007


    Nonlinear Robust/Adaptive Controller Design for an Air-Breathing Hypersonic Vehicle Model AIAA Paper

    Fiorentini, L. / Serrani, A. / Bolender, M. et al. | British Library Conference Proceedings | 2007



    Robust Adaptive Multiple Model Controller Design for an Airbreathing Hypersonic Vehicle Model

    Kuipers, M. / Ioannou, P. / Fidan, B. et al. | British Library Conference Proceedings | 2008


    Robust Adaptive Multiple Model Controller Design for an Airbreathing Hypersonic Vehicle Model

    Kuipers, Matthew / Ioannou, Petros / Fidan, Baris et al. | AIAA | 2008