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Satellites, Attitude stability, Flexible spacecraftEdition | Availability |
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The attitude stability of a flexible rod satellite placed at an equilateral Lagrangian point in the restricted three-body problem
1980, Dept. of Aerospace Science and Engineering
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Book Details
Edition Notes
Thesis (M.A.Sc.) - University of Toronto, 1980.
Includes bibliographical references.
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January 18, 2010 | Edited by WorkBot | add subjects and covers |
December 11, 2009 | Created by WorkBot | add works page |