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Geostationary Satellites Collocation aims to find solutions for deploying a safe and reliable collocation control. Focusing on the orbital perturbation analysis, the mathematical foundations for orbit and control of the geostationary satellite. The mathematical and physical principle of orbital maneuver and collocation strategies for multi geostationary satellites sharing with the same dead band is also stressed. Moreover, the book presents some applications using the above algorithms and mathematical models to help readers master the corrective method for planning station keeping maneuvers. Engineers and scientists in the fields of aerospace technology and space science can benefit from this book. Hengnian Li is the Deputy Director of State Key Laboratory of Astronautic Dynamics, China.

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9783642407987

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Publication List: [1] Li H. N., Geostationary Satellite Orbital Analysis and Collocation Strategies [M], Beijing: National Defense industry Press, 2010.10. [In Chinese] [2] Li H. N., Gao Y. J., etc. the strategies and algorithms study for multi-GEO satellites collocation[J], Journal of Astronautics, Vol. 30, No. 3:967-973. [In Chinese] [3] Li H. N., The Separation Methods and Station Keeping Algorithms For Multi-GEOS Collocation [C], the 60th International Astronautical Congress,Daejeon, Republic of Korea. [4] Li H. N., Li J. S., on-line orbit determination method for satellite with continuous thrust acceleration [J], System Engineering and Electronics, 2010(09):1957-1961.[in Chinese] [5] Li H. N., Li J. S., A dynamic model compensation orbit determination method for maneuvering satellite [J], Journal of Astronautics, Vol. 31, No. 10: 2269:2275. [6] Li H. N., Li J. S., Analyzing perturbation motion and studying configuration maintenance strategy for compass-M navigation constellation, Journal of Astronautics, Vol. 31, No. 7:1756-1761. [in Chinese] [7] Li H. N., Li J. S., on-line minimum variance estimation for thrust acceleration during orbit transfer process, Journal of Astronautics, Vol. 23, No. 5, 2002(09):76:80.

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