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On a case of integrable equations of perturbed motion of a satellite

โœ Scribed by K.G. Valeev


Publisher
Elsevier Science
Year
1965
Tongue
English
Weight
97 KB
Volume
29
Category
Article
ISSN
0021-8928

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A New Approach for Analytical Computatio
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The problem of computation of the Hamiltonian for the perturbed motion of an artificial Earth satellite with large eccentricity is considered. The method of calculation of items of the perturbing function, which is presented in the form of Jacobi nome series, is described. Some advantages of the new