1Paul Nacozy,Victor Szebehely. The computation of relative motion with increased precision[J] 1976,Celestial Mechanics(4):449～453
2T. F. Berreen,J. D. C. Crisp. An exact and a new first-order solution for the relative trajectories of a probe ejected from a space station[J] 1976,Celestial Mechanics(1):75～88
5MARTIN M, STALLARD M J. Distributed satellite missions and technologies-The TechSat 21 program [C].AIAA-99-4479, AIAA Space Technology Conference & Exposition, Albuquerque, NM, September, 1999.
6FOLTA D, HAWKINS A. Results Of NASA's First Autonomous Formation Flying Experiment: Earth Observing-1 (EO-1)[C]. AIAA 2002-4743, AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Monterey, California, August, 2002.
7FINNEGAN E J, CARLISLE C C. Space Technology 5: Pathfinder for Future Micro-Sat Constellations [J~. IEEE AC paper-1353, 2003, 3:227-239.
8CLOHESSY W H, WILSHIRE R S. Terminal Guidance System for Satellite Rendezvous [J]. Journal of The Aerospace Science, 1960, 27 (9): 653-674.
9SCHAUB H. Relative Orbit Geometry through Classical Orbit Element Differences [J]. Journal of Guidance, Control, and Dynamics, 2004, 27(5):839-848.
10CHEN TONG, XU SHIJIE, WANG SONGXIA. Relative Motion Control for Autonomous Rendezvous Based on Classical Orbit Element Differences [J]. Journal of Guidance, Control, and Dynamics, 2007, 30 (4): 1003-1014.
