Planar motion of satellite containing damping mechanism is considered; it is shown that for small dampers motion eventually becomes nearly identical with periodic solution of undamped case; if state of satellite can be expressed by point inside appropriate limiting manifold for undamped motion then, for small damping, subsequent motion should remain stable and approach limit cycle; thus limits of stability determined for undamped satellite may be regarded as approximately valid for lightly damped configuration. (29800)


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    Title :

    Planar motion of damped satellite


    Additional title:

    CASI Trans


    Contributors:
    Modi, V.J. (author)


    Publication date :

    1969


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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