Liapunov Stability of Spinning Satellites with Long Flexible Appendages

Details Liapunov Stability of Spinning Satellites with Long Flexible Appendages Liapunov Stability of Spinning Satellites with Long Flexible Appendages

Dec 1971

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1971cemec...4..295h&link_type=abstract

Celestial Mechanics, Volume 4, Issue 3-4, pp. 295-308

Physics

1

Scientific paper

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.

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