When the spacecraft has a low spin rate and precise pointing requirements, the wobble angle must be damped in a time period equivalent to a very few wobble cycles. The design, analysis, and test of a passive pendulum wobble damper are described.


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    Title :

    A passive pendulum wobble damper for a low spin rate Jupiter flyby spacecraft


    Contributors:


    Publication date :

    1972-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :