On eccentricity functions for eccentric orbits
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Abstract
Situations arise in celestial mechanics where orbital eccentricities are large and yet it is desirable to maintain the Darwin-Kaula Fourier decomposition of the perturbing function. Evaluation of the appropriate eccentricity functionsG lpq (e) requires a double summation which, for practical purposes, must be truncated. In this note criteria have been established for truncation of the expansion for eccentricities ≦0.75.
Keywords
Fourier Practical Purpose Celestial Mechanic Eccentric Orbit Fourier Decomposition
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