Application of modular control techniques to the attitude control of a prototype flexible spacecraft and a prototype flexible space platform was further developed by determining numerical values for the physical parameters of a four body approximation of the MSFC/hybrid deployable truss incorporated in the space platform model, generating sensitivity coefficients for the model of the flexible spacecraft, evaluating the changes in the digital computer simulation of the flexible spacecraft resulting from the addition of another rigid body to the model and comparing attitude control effectiveness with actuators on more than one rigid body of the model with that for the case in which the actuators were restricted to one body.


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    Title :

    Modular Design Attitude Control System


    Contributors:

    Publication date :

    1983


    Size :

    65 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Modular design attitude control system

    Chichester, F. D. | NTRS | 1983


    Modular design attitude control system

    Chichester, F. D. | NTRS | 1982


    Modular Design Attitude Control System

    F. D. Chichester | NTIS | 1982