@inproceedings{0362fa95511b4945a9a28c6f286af0ea,
title = "Closed-form solutions for satellite relative motion in an axially-symmetric gravitational field",
abstract = "A different approach is proposed for the study of satellite relative motion in an axially-symmetric gravitational field. Instead of using the Keplerian motion as the generating nominal orbit for the absolute motion, another {"}unperturbed{"} orbit is proposed instead: An equatorial orbit about an oblate planet. Based on the superintegrability of such motion, closed-form solutions for the equatorial relative motion are obtained. Analytic conditions for the periodicity of the relative motion in a generic central force field are presented, and utilized to design long-term bounded relative motion under high-order even zonal perturbations.",
author = "Vladimir Martinu{\c s}i and Pini Gurfil",
year = "2011",
language = "الإنجليزيّة",
isbn = "9780877035695",
series = "Advances in the Astronautical Sciences",
pages = "1525--1544",
booktitle = "Spaceflight Mechanics 2011 - Advances in the Astronautical Sciences",
note = "21st AAS/AIAA Space Flight Mechanics Meeting ; Conference date: 13-02-2011 Through 17-02-2011",
}