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  • 1
    Electronic Resource
    Electronic Resource
    Liapunov stability of spinning satellites with long flexible appendages (1971)
    Springer
    Celestial mechanics and dynamical astronomy 4 (1971), S. 295-308 
    Details
    ISSN: 1572-9478
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics
    Notes: Abstract The equations of motion are derived for the case of a spinning satellite which has a central rigid body, and long flexible appendages which are nominally in the spin plane. The ‘major-axis theorem’ is found to be necessary, but not sufficient for this case, and appropriate sufficiency criteria are derived from a Liapunov function. The results are presented in a form amenable to satellite design.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF01231392
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