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Investigation of the Time of Ballistic Existence for Elliptic Orbits Evolving under the Influence of Gravitational Perturbations of External Bodies

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Abstract

A comparative analysis of the time of ballistic existence for different elliptic orbits evolving under the influence of gravitational perturbations of external bodies is performed. For this purpose, the solution of a satellite variant of the restricted circular double-averaged three-body problem obtained by M.L. Lidov [1] is used. The use of a geometrical interpretation of Lidov's solutions has allowed us to create a visualized tool for a choice of evolving satellite orbits with a long time of ballistic existence.

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REFERENCES

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  2. Moiseev, N.D., Certain Basic Simplified Schemes of Celestial Mechanics Derived by Averaging the Restricted Circular Three-Point Problem, Trudy GAISh, 1945, vol. 15, part 1, p. 100.

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Prokhorenko, V.I. Investigation of the Time of Ballistic Existence for Elliptic Orbits Evolving under the Influence of Gravitational Perturbations of External Bodies. Cosmic Research 40, 264–273 (2002). https://doi.org/10.1023/A:1015929121296

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  • DOI: https://doi.org/10.1023/A:1015929121296

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