Abstract
This paper presents a basic frame applicable to any perturbed circular motion in any orbital inclination, and a method of resolution leading to a formal solution given here to the first order. The main advantage of the solution, expanded in Fourier series and non-singular variables, is the presence of iterative formation laws for its coefficients. The theory is then particularly accurate and suitable for various periodic perturbations. The comparison of the results with a numerical integration is convincing.
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Bois, E. First-order accurate theory of perturbed circular motion. Celestial Mech Dyn Astr 58, 125–138 (1994). https://doi.org/10.1007/BF00695788
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DOI: https://doi.org/10.1007/BF00695788