Isochronic derivatives in the Euler-Poinceau problem

Astronomy and Astrophysics – Astronomy

Scientific paper

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Astrodynamics, Euler Equations Of Motion, Satellite Perturbation, Derivation, Differential Equations

Scientific paper

A Euler-Poinceau approach is developed for determining the attitude of a
slightly perturbed satellite. The method involves the division of the
time interval under consideration into segments within which the
satellite motion with respect to its center of mass is assumed to be
unperturbed.

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