Orbit Design of Spacecraft on Elliptical Orbit

Author:

Liu Fucheng,Lu Shan,Sun Yue

Publisher

Springer Singapore

Reference10 articles.

1. LU Shan, XU Xu, WU Hai-lei. A High Precision Attitude Tracking Control Method for Highly Eccentric Orbit Spacecraft Rendezvous with a HEO Target [C]. The 16th Conference on Space and Motion Control Technology, 2014: 288–293.

2. Xi Xiaoning, Wang Wei. Near-Earth Spacecraft Orbital Foundation [M]. Changsha: National University of Defense Technology Press, 2003.

3. Montenbruck O, Gill E. State Interpolation for on Board Navigation Systems [J]. Aerospace Science and Technology, 2001(5): 209–220.

4. Hoots F R, Roehrich R L. Spacetrack Report No.3 [C]. AIAA/AAS Astrodynamics Specialist Conference, 2006: 1984–2071.

5. Meng Bo, Han Chao. Development of Simulation Software for High Precision Spacecraft Orbit Prediction [J]. Computer Simulation, 2008, 25 (1): 62–65, 73.

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