The dynamics of the model used for the design and simulation of a flexible aerospace vehicle differs from the actual system due to dynamic perturbations. The changes in parameters of the vehicle during the flight duration could lead to failure in the control system if ignored during the initial stage of the controller design. The ability of a designed control system to maintain it performance and stability characteristics under the effect of all types of influences is a major concern for controller-design engineers. This paper presents the robust controller design and simulation for a flexible sounding rocket.


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    Titel :

    Application of robust synthesis methodology for sounding rocket attitude stabilization


    Beteiligte:
    Brodsky, S. A. (Autor:in) / Aro, H. O. (Autor:in)


    Erscheinungsdatum :

    01.06.2011


    Format / Umfang :

    778583 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Application of Adaptive Control - Sounding Rocket Attitude

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    Shrewsberry, D. J. | NTRS | 1973



    NASA Sounding Rocket Program Attitude Control Systems (AAS 08-073)

    Eberspeaker, P.J. / American Astronautical Society | British Library Conference Proceedings | 2008