A hybrid multilevel linear quadratic regulator (ML-LQR) approach was developed and applied to the attitude control of models of the rotational dynamics of a prototype flexible spacecraft and of a typical space platform. Three axis rigid body flexible suspension models were developed for both the spacecraft and the space platform utilizing augmented body methods. Models of the spacecraft with hybrid ML-LQR attitude control and with LQR attitude control were simulated and their response with the two different types of control were compared.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Modular design attitude control system


    Beteiligte:

    Erscheinungsdatum :

    1982-03-08


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Modular Design Attitude Control System

    F. D. Chichester | NTIS | 1983


    Modular Design Attitude Control System

    F. D. Chichester | NTIS | 1982


    Modular design attitude control system

    Chichester, F. D. | NTRS | 1983