This paper presents the results 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:

    Conference:

    World Congress of the International Federation of Automatic Control ; 1972 ; Paris, France


    Publication date :

    1972-01-01


    Type of media :

    Miscellaneous


    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. / 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


    Passive stability of a spinning Skylab

    Seltzer, S. M. | NTRS | 1972


    Attitude control of a spinning Skylab.

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