Attitude stability of a spherical satell
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D.G. Maciros; A.J. Dennison
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Article
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1968
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Elsevier Science
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English
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The in-orbit-plane angular motion of a spherical satellite with a maSs eccentricity is studied, and both aerodynamic and gravitational torques along with large angle motions are considered. The equilibrium attitudes of the motion are investigated and the conditions for stability presented. The stabi