This paper presents an application of adaptive control techniques to the design of skid-to-turn missile autopilot. The involved simplified adaptive controller is developed by combining gain scheduling approach with the eigenstructure assignment control design. A linear interpolation method is proposed to generate linear parameter-varying controller from a finite set of linear time-invariant controllers. Results of simulations are reported to demonstrate the performance, stability, and robustness of the considered autopilot.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique


    Beteiligte:


    Erscheinungsdatum :

    2006-03-01


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Missile autopilot design using quasi-LPV polynomial eigenstructure assignment

    White, B.A. / Bruyere, L. / Tsourdos, A. | IEEE | 2007



    Nonlinear, hybrid bank-to-turn/skid-to-turn missile autopilot design

    Stansbery, Donald / Cloutier, James | AIAA | 2001


    Gain Scheduled Missile Autopilot Design Using a Control Signal Interpolation Technique

    Lawrence, D. / Kelly, J. / Evers, J. et al. | British Library Conference Proceedings | 1998