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- [1] The Implementation of Maintaining Constant Distance Between Satellites in Coplanar Elliptic OrbitsThe Journal of the Astronautical Sciences, 2002, 50 (1) : 53 - 69Zhaozhi TanPeter M. BainumAvaine Strong
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- [3] The implementation of maintaining constant distance between satellites in elliptic orbitsSPACEFLIGHT MECHANICS 2000, VOL 105, PTS I AND II, 2000, 105 : 667 - 683Tan, ZZBainum, PMStrong, A
- [4] The implementation of maintaining constant distance between satellites in elliptic orbitsAdvances in the Astronautical Sciences, 2000, 105 I : 667 - 683Tan, ZhaozhiBainum, Peter M.Strong, Avaine
- [5] OPTIMAL TRANSFERS BETWEEN COPLANAR ELLIPTIC ORBITSJOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (03) : 788 - 791LAWDEN, DF
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- [7] OPTIMAL AEROASSISTED TRANSFER BETWEEN COPLANAR ELLIPTIC-ORBITSACTA ASTRONAUTICA, 1986, 13 (6-7) : 291 - 299VINH, NXJOHANNESEN, JR
- [8] A strategy for maintaining distance between satellites in an orbiting constellationSPACEFLIGHT MECHANICS 1999, VOL 102, PTS I AND II, 1999, 102 : 343 - 354Tan, ZZBainum, PMStrong, A
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- [10] Initial deployment and near optimal control for maintaining constant distance between satellites in an elliptically orbiting constellationAdv Astronaut Sci, 1600, (555-573):Department of Mechanical Engineering, Howard University, Washington, DC 20059, United States
