[1] [1] Liu Chunbo, Zhao Shaobo, Han Xiang′e. Detection of space debris of centimeters in size via spaceborne ladar[J]. Infrared and Laser Engineering, 2012, 41(5): 1244-1248.(in Chinese)

[2] [2] O′Brien R, Sang J. Semianalytic satellite theory using the method of multiple scales[C]//AIAA paper 2004-4852, AIAA/AAS Astrodynamics Specialist Conference, 2004, 1:243-254.

[3] [3] Liu J J F, Alford R L. Semianalytic theory for a close-Earth artificial satellite[J]. Journal of Guidance and Control, 1980, 3(4): 304-311.

[4] [4] Danielson D A, Sagovac C P, Neta B, et al. Semianalytic Satellite Theory[M]. US: Naval Postgraduate School, Monterey, 1995: 93943.

[5] [5] Bezděk A, D Vokrouhlicky. Semianalytic theory of motion for close-Earth spherical satellites including drag and gravitational perturbations[J]. Planetary and Space Science, 2004, 52(14): 1233-1249.

[6] [6] Nayfeh, A. Perturbation Methods[M]. New York: John Wiley & Sons, 1977.

[7] [7] Montenbruck O, Gill E. Satellite Orbits-Models, Methods, and Applications [M]. Berlin: Springer-Verlag, Heidelberg, 2000.

[8] [8] Sang J, Bennett J, Smith C. Estimation of ballistic coefficients of low altitude debris objects from historical two line elements[J]. Advances in Space Research, 2013, 52:117-124.