[1] Sabol C, Hill K, Alfriend K, et al. Nonlinear effects in the correlation of tracks and covariance propagation[J]. Acta Astronautica, 2013, 84:69-80.
[2] Alfriend K T, Lim J. Performance of a dynamic algorithm for processing uncorrelated tracks[C]. AAS 99-365, AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska, Aug. 15-19, 1999.
[3] Wang R, Liu J, Zhang Q M. Propagation errors analysis of TLE data[J]. Advances in Space Research, 2009, 43(7):1065-1069.
[4] Bai X Z. Research on orbital prediction error and collision probability of space objects[D]. Changsha:National University of Defense Technology, 2013. (in Chinese)
[5] Chen Lei, Han Lei, Bai Xianzong, et al. Orbital Dynamics and Error Analysis of Space Object[M]. Beijing:National Defense Industry Press, 2010. (in Chinese)
[6] Bai Xianzong, Chen Lei, Tang Guojin. Explicit expression of collision probability in terms of RSW and NTW components of relative position[J]. Advances in Space Research, 2013, 52(6):1078-1096.
[7] Bai Xianzong, Chen Lei, Tang Guojin. Periodicity characterization of orbital prediction error and Poisson series fitting[J]. Advances in Space Research, 2012, 50(5):560-575.
[8] Cao Yuhui, Fan Pengcheng. Initial error propagation of elliptical orbit based on T-H equation[J]. Chinese Space Science and Technology, 2014(2):28-35. (in Chinese)
[9] Yan Ruidong, Wang Ronglan. Study of covariance calculation in space objects collision warning[J]. Chin J Space Sci, 2014, 34(4):441-448. (in Chinese)
[10] Tapley B D, Schutz B E, Born G R, Statistical Orbit Determination[M]. New York:Academic Press, 2004.
[11] Markley F L, Seidewitz E, Nicholson M. A general model for attitude determination error analysis[C]//NASA Conference Publication 3011:Flight Mechanics/Estimation Theory Symposium, 1988.
[12] Markley F L, Seidewitz E, Deutschmann J. Attitude determination error analysis:general model and specific application[C]//Proceedings of the CNES Space Dynamics Conference, 1989:251-266.
[13] Carpenter J R, Markley F L, Alfriend K T, et al. Sequential probability ratio test for collision avoidance maneuver decisions based on a bank of norm-inequality-constrained epoch-state filters[C]//AAS/AIAA Astrodynamics Specialist Conference, No. AAS 11-437, 2011.
[14] Montenbruck O. An epoch state filter for use with analytical orbit models of low earth satellites[J]. Aerosp Sci Technol, 2000, 4:277-287.
[15] Zong Rui, Lin Defu, Liu Tairan, et al. Compensation method for scale error of optical strapdown seeker using UKF[J]. Infrared and Laser Engineering, 2014, 43(11):3577-3584. (in Chinese)
[16] Fu Ying, Tang Ziyue. Methodology for tracking multi-target hidden in Doppler blind zone based on airborne and ground-based early warning radar cooperation[J]. Infrared and Laser Engineering, 2014, 43(7):2379-2386. (in Chinese)
[17] Zhao Xijing, Liu Guangbin. Fifth degree cubature Kalman filter algorithm and its application[J]. Infrared and Laser Engineering, 2015, 44(4):1377-1381. (in Chinese)