Control system is shown to be sized, in terms of required impulse capacity, by long term effects of gravity gradient and aerodynamic disturbances; reaction control propellant required to counteract disturbances is minimized by selection of attitude orientations which reduce external torques and by using momentum storage devices to counteract cyclic disturbances; examples of experimental mechanization with space station control system are described including earth surface tracking device, horizon spectrometry experiment and astronomical telescope.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flight control for manned orbital space station


    Additional title:

    SAE-NASA -- Proc


    Contributors:
    Hayes, W.S. (author) / Wensley, D.C. (author)

    Conference:

    Proceedings of the SAE-NASA -- Aerospace Vehicle Flight Control Conference ; 1965 Control



    Publication date :

    1965


    Size :

    32 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Flight Control for a Manned Orbital Space Station

    Wensley, D. C. / Hayes, W. S. | SAE Technical Papers | 1965


    Flight control for a manned orbital space station.

    Hayes, W. S. / Wensley, D. C. | NTRS | 1965


    A MULTIPURPOSE, MANNED, ORBITAL SPACE STATION

    Mathews, C. W. / Olling, E. H. | NTRS | 1963


    A MULTIPURPOSE, MANNED, ORBITAL SPACE STATION

    MATHEWS, C. / OLLING, E. | AIAA | 1963


    Results of the Second U.S. Manned Orbital Space Flight

    J. H. Boynton / E. M. Fields | NTIS | 1962