A third-order solution of Vinti's problem with explicit expressions for the Poisson brackets

Astronomy and Astrophysics – Astrophysics

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Error Analysis, Orbit Perturbation, Orbital Elements, Satellite Observation, Vinti Theory, Artificial Satellites, Legendre Functions, Orbital Mechanics, Polynomials, Spherical Coordinates

Scientific paper

It is noted that, with increasing accuracy in satellite observations and greater refinement in research topics, the need for a third-order perturbation theory has become pressing. Such a theory is addressed here by first studying the perturbations of intermediate orbits. The Vinti-type intermediate orbit containing J3 is chosen because it contains many perturbations. Its potential functions contains the whole of J2 and J3 perturbations and two-thirds of the J4 perturbation. A detailed derivation is given of the basic solution that is accurate to the third order. Also given are the Poisson's brackets of the elements of this intermediate orbit.

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