Attitude Stability of a Spinning Satellite in an Elliptic Orbit
- 1 June 1966
- journal article
- Published by ASME International in Journal of Applied Mechanics
- Vol. 33 (2) , 402-405
- https://doi.org/10.1115/1.3625056
Abstract
Floque´t theory is used to develop a procedure for testing the stability of a spinning, symmetric satellite whose mass center moves on an elliptic orbit while the symmetry axis remains normal to the orbit plane.Keywords
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