[1] [1] WEI X G, XU J, ZHANG G J. S-curve error compensation of centroiding location for star sensors ［J］. Opt. Precision Eng., 2013, 21(4): 849-857.(in Chinese)

[2] [2] JIANG F, WU Q W, LIU J, et al.. Thermal design of lightweight space remote sensor integrated with satellite in low earth orbit ［J］. Chinese Optics, 2013, 6(2): 237-243.(in Chinese)

[3] [3] LIEBE C C. Pattern recognition of star constellations for spacecraft applications ［J］. IEEE Aerospace and Electronic Systems Magazine, 1992, 7(6): 34-41.

[4] [4] WEI X G, WANG Q L, LI J, et al.. On-orbit calibration for cross-angle between optical axes of star sensor and remote sensing camera ［J］. Opt. Precision Eng., 2013, 21(2): 274-280.(in Chinese)

[5] [5] LAHER R. Attitude control system and star tracker performance of the wide-field infrared explorer spacecraft ［J］. American Astronomical Society, AAS 2000, 145: 723-751.

[6] [6] 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)

[7] [7] SAMMAN M A. Toward faster and more accurate star sensors using recursive centroiding and star identification ［D］. Texas: Dept Texas A & M University, 2006.

[8] [8] JIANG J, LI X, ZHANG G J, et al.. Fast star tracking technology in star sensor ［J］.Proc. SPIE, 2006: 6358, 63580A.

[9] [9] JIE J, ZHANG G J, WEI X G, et al.. Rapid star tracking algorithm for star sensor ［J］. IEEE A & E Systems Magazine, 2009, 24(9): 23-33.

[10] [10] XU W, PIAO Y J. Analysis of new generation high-performance small satellite technology based on the Pleiades ［J］. Chinese Optics, 2013, 6(1): 9-19.(in Chinese)