The results are presented of a study of the dynamics of a spinning Skylab space station. The stability of motion of several simplified models with flexible appendages was investigated. A digital simulation model that more accurately portrays the complex Skylab vehicle is described, and simulation results are compared with analytically derived results. (Author)


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    Titel :

    Stabilizing a Spinning Skylab


    Beteiligte:
    S. M. Seltzer (Autor:in) / J. S. Patel (Autor:in) / D. W. Justice (Autor:in) / G. Schweitzer (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Stabilizing a spinning Skylab.

    Seltzer, S. M. / Justice, D. W. / Schweitzer, G. et al. | NTRS | 1972


    Stabilizing a spinning Skylab

    Seltzer, S. M. / Patel, J. S. / Justice, D. W. et al. | NTRS | 1972


    Attitude Control of a Spinning Skylab

    S. M. SELTZER / GERHARD SCHWEITZER AND BERNARD ASNER | AIAA | 1973


    Attitude control of a spinning Skylab.

    Seltzer, S. M. / Schweitzer, G. / Asner, B., Jr. | NTRS | 1972


    Attitude control of a spinning Skylab

    SELTZER, S. / SCHWEITZER, G. / ASNER, JR., B. | AIAA | 1972