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The prediction of satellite orbits

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Dynamics of Satellites / Dynamique des Satellites

Part of the book series: IUTAM Symposia ((IUTAM))

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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Maurice Roy

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© 1963 Springer-Verlag Berlin Heidelberg

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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

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-48132-1

  • Online ISBN: 978-3-642-48130-7

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