Abstract
This paper is based on the restricted problem of three bodies with the unusual feature that the lightest particle is replaced by a rigid body.
The attitude stability of the body is considered when its centre of mass is located at one of the equilibrium points. The stable attitude is determined when the satellite is stationary relative to the primaries. It is found that for some bodies there are two such attitudes, and these are determined.
Similar content being viewed by others
References
De Bra, D. B. and Delp, R. H.: 1961,J. Astronaut. Sci. 8, 14.
Kane, T. R. and Marsh, E. L.: 1971,Celes. Mech. 4, 78.
Kane, T. R., Marsh, E. L., and Wilson, W. G.: 1963,J. Astronaut. Sci. 9, 108.
Robinson, W. J.: 1973a,Celes. Mech. 8, 323.
Robinson, W. J.: 1973b, in B. D. Tapley and V. Szebehely (eds.),Recent Advances in Dynamical Astronomy, D. Reidel Publ. Co., Dordrecht, pp. 457–460.
Szebehely, V.: 1967, Theory of Orbits, Academic Press, New York and London.
Szebehely, V. and Williams, C. A.: 1964,Astron. J. 69, 460.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Robinson, W.J. Attitude stability of a rigid body placed at an equilibrium point in the restricted problem of three bodies. Celestial Mechanics 10, 17–33 (1974). https://doi.org/10.1007/BF01261876
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01261876