[1] [1] KIRAN K G, DECLAN C H, JOHN L J, et al.. A vision-based DSP embedded navigation sensor ［J］. IEEE Sensors Journal, 2002, 2(5): 428-442.

[2] [2] DEBO S, JOHN L C. Observability analysis of six degree of freedom configuration determination using vector observations［J］. J. Guid. Control. Dyn, 2002, 25(6): 1149-1157.

[3] [3] ROBERTO A, JOHN L C. Vision-based relative navigation for formation flying of spacecraft［C］. 2000 AIAA Guidance, Navigation, and Control Conference and Exhibit, 14-17 August, 2000, Denver, CO.

[4] [4] SON-GOO K. Kalman filtering for relative spacecraft attitude and position estimation［D］. Department of Mechanical & Aerospace Engineering State University of New York at Buffalo, 2005.

[5] [5] SON-GOO K, CRASSIDIS J, YANG C.Kalman filtering for relative spacecraft attitude and position estimation ［J］. J. Guid. Control. Dyn, 2007, 30(1): 133-143.

[6] [6] TANG X J, YAN J, ZHONG D D. Square-root sigma-point kalman filtering for spacecraft relative navigation ［J］. Acta Astronautica, 2010, 66(5-6): 704-713.

[7] [7] DAERO L, HENRY P. Vision-based relative state estimation using the unscented kalman filter ［J］. International Journal of Aeronautical and Space Sciences, 2011, 12(1): 24-36.

[8] [8] YOUNG-GU L, HYOCHOONG B. Relative state estimation of satellite formation flying using kalman filter［C］. Proceedings of the 17th World Congress The International Federation of Automatic Control, Seoul, Korea, 2008.

[9] [9] HILL G W. Researches in the lunar theory ［J］. American Journal of Mathematics, 1878, 1(1): 5-26.

[10] [10] SUN G F, ZHANG G Y, JIANG H L, et al..Design of very high accuracy star simulator［J］. Opt. Precision Eng., 2011, 19(8): 1730-1735.(in Chinese)

[11] [11] CLOHESSY W, WILTSHIRE R. Terminal guidance system for satellite rendezvous ［J］. Journal of the Aerospace Sciences, 1960, 27(9): 653-658.

[12] [12] CHEN X Q, GENG Y H, WANG F, et al..Staring imaging attitude tracking control of agile small satellite［J］. Opt. Precision Eng., 2012, 20(5): 1031-1040.(in Chinese)

[13] [13] FARRENKOPF R L.Analytic steady-state accuracy solutions for two common spacecraft attitude estimators ［J］. Journal of Guidance and Control, 1978, 1(4): 282-284.

[14] [14] MARKLEY F L. Attitude error representations for Kalman filtering ［J］. Journal of Guidance, Control, and Dynamics, 2003, 26(2): 311-317.

[15] [15] ZHANG R W. Satellite Orbit Attitude Dynamics and Control ［M］. Beijing: Beihang University Press, 1998: 39-70.(in Chinese)

[16] [16] JULIER S J, UHLMANN J K. Reduced sigma point filters for the propagation of means and covariances through nonlinear transformations ［C］. Proceedings of the American Control Conference, Defferson City, 2002: 887-892.

[17] [17] LIU G X, MA T, CHEN SH L. Unscented particle filtering algorithm using minimal skew sampling ［J］. Opt. Precision Eng., 2008, 16(4): 746-751.(in Chinese)

[18] [18] JULIER S, UHLMANN J K. A new approach for filtering nonlinear systems［C］. Proceedings of the American control conference. IEEE Press, 1995: 1628-1632.

[19] [19] JULIER S J, UHLMANN J K. Reduced sigma point filters for the propagation of means and covariances through nonlinear transformations ［C］. Proceedings of the American Control Conference, Defferson City, 2002: 887-892.

[20] [20] JULIER S, UHLMANN J. Unscented filtering and nonlinear estimation［C］. Proceedings of IEEE. 2004, 92(3): 401-422.

[21] [21] BROWN O, EREMENKO P. Fractionated space architectures: a vision for responsive space［C］. 4th Responsive Space Conference, April 24-27, 2006, Los Angeles, CA: 1-13.