A laboratory-based testbed that will be used to explore various issues and concepts in spacecraft dynamics and control is described. The testbed is based on a triaxial air bearing to allow experiments involving large-angle, three-axis motion. The sensing, actuation, and processor hardware being developed for the testbed is highlighted.


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    Title :

    Development of air spindle and triaxial air bearing testbeds for spacecraft dynamics and control experiments


    Contributors:

    Published in:

    Publication date :

    2001


    Size :

    6 Seiten, 16 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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