An In-Plane $J_2$-Invariance Condition and Control Algorithm for Highly Elliptical Satellite Formations

TL;DR

This paper introduces a new in-plane J2-invariance condition and control strategy for maintaining highly elliptical satellite formations efficiently, reducing propellant use and controlling out-of-plane motion.

Contribution

It presents a novel in-plane J2-invariance condition and a control algorithm specifically designed for highly elliptical satellite formations, including the boomerang perch formation.

Findings

The proposed condition minimizes propellant consumption.

The control strategy effectively manages out-of-plane motion.

Application to the boomerang perch formation demonstrates practical benefits.

Abstract

Phased formations of satellites provide an important means of keeping multiple satellites in close proximity without becoming dangerously close to one another. In order to minimize the amount of propellant necessary to keep a set of satellites in a phased formation, this paper presents a new condition for in-plane linearized secular J2-invariance in highly eccentric orbits. A maintenance strategy outlined here combats the growth of out-of-plane motion, and the delta-v cost of this strategy is analyzed. For context, this paper also discusses relevant formations that benefit from this condition and maintenance strategy. A highly elliptical perching formation called the boomerang perch is also discussed.