Dynamic Limits on Planar Libration-Orbit Coupling Around an Oblate Primary

TL;DR

This paper analyzes the dynamic behavior of an ellipsoidal satellite orbiting an oblate primary, identifying conditions for libration and circulation, and deriving bounds and analytical conditions for these motions.

Contribution

It introduces new analytical conditions and bounds for libration and circulation in the planar libration-orbit coupling system around an oblate primary.

Findings

Existence of stable equilibrium points for libration.

Zero-velocity curves define bounds on libration and circulation.

Analytical conditions for maximum libration angle and circulation are derived.

Abstract

This paper explores the dynamic properties of the planar system of an ellipsoidal satellite in an equatorial orbit about an oblate primary. In particular, we investigate the conditions for which the satellite is bound in librational motion or when the satellite will circulate with respect to the primary. We find the existence of stable equilibrium points about which the satellite can librate, and explore both the linearized and non-linear dynamics around these points. Absolute bounds are placed on the phase space of the libration-orbit coupling through the use of zero-velocity curves that exist in the system. These zero-velocity curves are used to derive a sufficient condition for when the satellite's libration is bound to less than 90 degrees. When this condition is not satisfied so that circulation of the satellite is possible, the initial conditions at zero libration angle are determined which lead to circulation of the satellite. Exact analytical conditions for circulation and the maximum libration angle are derived for the case of a small satellite in orbits of any eccentricity.