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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Modular Design Attitude Control System


    Contributors:

    Publication date :

    1982


    Size :

    137 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Modular Design Attitude Control System

    F. D. Chichester | NTIS | 1983


    Modular design attitude control system

    Chichester, F. D. | NTRS | 1982


    Modular design attitude control system

    Chichester, F. D. | NTRS | 1983