Abstract
In this paper we develop a perturbation method and apply it to the prediction of orbits of earth satellites that are disturbed by various external forces. The theory of resonances and stable orbit configurations, possible when sunlight pressure is important, are also analyzed. Finally, we describe experiments to determine the magnitude of perturbing forces such as charge drag.
Operated with support from the U.S. Air Force.
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References
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We wish to thank L. G. Jacchia for a discussion on this point.
Colombo, G.: Smith. Astrophys. Obs., is investigating the possibility of using such techniques.
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Shapiro, I.I. (1963). The prediction of satellite orbits. In: Roy, M. (eds) Dynamics of Satellites / Dynamique des Satellites. IUTAM Symposia. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-48130-7_24
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DOI: https://doi.org/10.1007/978-3-642-48130-7_24
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