This work is concerned with an application of gain-scheduling control method to design of skid-to-turn (STT) missile autopilot. Presented simple non-linear adaptive controller is developed by combining linear parameter-varying (LPV) gain scheduling approach with eigenvalue assignment control technique. Subsequently, linear interpolation is applied to generate non-linear parameter varying controller from a finite number of linear time-invariant (LTI) controllers. Results of simulations are reported to demonstrate performance, stability as well as robustness of introduced scheme.


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    Titel :

    Design of gain-scheduled autopilot for a highly-agile missile


    Beteiligte:
    Mehrabian, A.R. (Autor:in) / Roshanian, J. (Autor:in)


    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    3432729 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch