Topics are presented in the field of flexible spacecraft configurations. Dynamic models are reviewed for spinning and non-spinning satellites. The attitude stability of flexible satellites is discussed. Applications are described of modern control theory and the design of control systems for these configurations is outlined. Test and flight verifications are reported, and some special dynamics problems are dealt with.


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    Title :

    Dynamics and Control of Non-Rigid Space Vehicles


    Publication date :

    1976


    Size :

    338 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English