The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences. Vol. XXXVII. Part Bib. Beijing 2008 
Target[J]. Chinese Space Science and 
Technology,2007,27(4):7-13(In Chinese). 
[8] LUO Jian-jun, YUAN Jian-ping. The Application of GPS in 
a multi-spacecraft system[J], Flight Dynamics,2000,18(3):5- 
9(In Chinese). 
[9] Li Zifeng. A Relative Guidance Algorithm for Proximity of 
Docking[J], Aerospace Control, 2005,23(5):27-30(In Chinese). 
[10] Fei Weichun. Estimation Method of Relative Position and 
Attitude for Spacecraft Rendezvous and Docking[J]. CHINESE 
SPACE SCIENCE AND TECHNOLOGY,2004(3):l-6(In 
Chinese). 
[11] Liu Tao,XieYongchu. A Study on Relative Navigation for 
Spacecraft Rendezvous with a Non-cooperative Target[J], 
Aerospace Contro,2006,24(2):48-53(In Chinese). 
[12] ZHANG Shi-jie,CAO Xi-bin,CHEN Min. Monocular 
Vision-based Relative Pose Parameters Determination for Non 
cooperative Spacecrafts[J].Journal of Nanjing University of 
Science and Technology, 2006,30(5):564-568(In Chinese). 
[13] Carter TE.New form for the optimal rendezvous equations 
near a keplerian orbit[J]. Journal of Guidance, Control , and 
Dynamics, 1990,13(1): 1411-1416. 
[14] Goekhan Inalhan,Michael Tillerson and Jonathan P.How. 
Relative Dynamics and Control of Spacecraft Formations in 
Eccentric Orbits[J]. Journal of Guidance, Control , and 
Dynamics,2002,25( 1 ):48-59. 
[15] JIANG Gang-wu, GONG Hui, WANG Jing, JIANG Ting. 
The ooptical measurement of self-calibration in orbit for 
spacecraft rendezvous and docking[J]. Journal of Astronautics, 
2007,28( 1): 15-21 (In Chinese). 
[16] JIANG Gang-wu; JIANG Ting; WANG Yong; GONG Hui. 
Space Resection Independent of Initial Value Based on Unit 
Quatemions[J]. Acta Geodaetica et Cartographica Sinica, 
2007,36(29):! 69-175(In Chinese).