First-order accurate theory of perturbed circular motion

Astronomy and Astrophysics – Astronomy

Scientific paper

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Circular Orbits, Orbit Perturbation, Satellite Orbits, Euler-Lagrange Equation, Fourier Series, Iterative Solution, Numerical Integration, Perturbation Theory

Scientific paper

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 coefficents. 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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