Attitude stability of a symmetric satellite at the equilibrium points in the restricted three-body problem-Reference-Cited by-同舟云学术

Attitude stability of a symmetric satellite at the equilibrium points in the restricted three-body problem

Published:1971-09 Issue:1 Volume:4 Page:78-90
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Kane T. R.,Marsh E. L.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modelling and Simulation,General Medicine

Link

http://link.springer.com/content/pdf/10.1007/BF01230323.pdf

Reference5 articles.

1. Kane, T. R., Marsh, E. L., and Wilson, W. G.: 1963, ?Letter to the Editor,?J. Astron. Sci. 9, 108?109.

2. Moulton, F. R.: 1914,An Introduction to Celestial Mechanics, Macmillan Co., New York, N. Y., pp. 277?320.

3. Plummer, Lt. C.: 1960,An Introductory Treatise on Dynamical Astronomy, Dover Publications, New York, N. Y., p. 294.

4. Smart, W. M.: 1953,Celestial Mechanics, Longmans, Green and Co. Ltd., London, pp. 343?377.

5. Thomson, W. T.: 1962, ?Spin Stabilization of Attitude Against Gravity Torque?,J. Astron. Sci. 9, 31?33.

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