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.


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    Title :

    Stabilizing a spinning Skylab


    Contributors:

    Publication date :

    1972-01-03


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Stabilizing a Spinning Skylab

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


    Stabilizing a spinning Skylab.

    Seltzer, S. M. / Justice, D. W. / Schweitzer, G. 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