The first tethered satellite system, scheduled for launch in May 1991, is reviewed. The system dynamics, dynamics control, and dynamics simulations are discussed. Particular attention is given to in-plane and out-of-plane librations; tether oscillation modes; orbiter and sub-satellite dynamics; deployer control system; the sub-satellite attitude measurement and control system; the Aeritalia Dynamics Model; the Martin-Marietta and NASA-MSFC Dynamics Model; and simulation results.


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    Titel :

    Tethered satellite system dynamics and control


    Beteiligte:
    Musetti, B. (Autor:in) / Cibrario, B. (Autor:in) / Bussolino, L. (Autor:in) / Bodley, C. S. (Autor:in) / Flanders, H. A. (Autor:in) / Mowery, D. K. (Autor:in) / Tomlin, D. D. (Autor:in)

    Kongress:

    International Conference on the Dynamics of Flexible Structures in Space ; 1990 ; Cranfield


    Erscheinungsdatum :

    01.01.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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