[1] 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)

[2] XU K, JIN G, CHEN J, et al.. Switch algorithm for quick small satellite attitude maneuver［J］. Opt. Precision Eng., 2008, 16(8): 1528-1532. (in Chinese)

[3] GUO J L. Time optimal control for three-axis stabilized satellite reorientation［D］. Harbin: Dissertation for the Master Degree in Harbin Institute of Technology, 2013. (in Chinese)

[4] WANG SH H. The research of large angle maneuver attitude nonlinear control law for satellite ［D］. Harbin: Dissertation for the Master Degree in Harbin Institute of Technology,2010.(in Chinese)

[5] LI CH J. Research on nonlinear attitude control for spacecrafts based on Lyapunov method［D］. Harbin: Dissertation for the Doctoral Degree in Harbin Institute of Technology, 2006.(in Chinese)

[6] HE Y. Research on attitude maneuvers control of agile small satellite based on SGCMG［D］. harbin: Dissertation for the Master Degree in Harbin Institute of Technology, 2011.(in Chinese)

[7] GUAN P, LIU X H, LIU X J. Variable structure attitude control of flexible satellite ［J］. Control Theory and Applications,2007, 24(3): 480-484. (in Chinese)

[8] YANG Y G. Research on rapid maneuver and stabilization method for agile satellite［D］. Harbin: Dissertation for the Master Degree in Harbin Institute of Technology,2013. (in Chinese)

[9] XU K, JIN G, CHEN J, et al.. Application of variable structure algorithm on small satellite attitude control［J］. Opt. Precision Eng., 2007,15: 118-123. (in Chinese)

[10] ZHAO L, YAN X, HAO Y, et al.. Adaptive fault tolerant control for spacecraft based on fast terminal sliding mode［J］. Journal of Astronautics,2012, 33(4): 426-435. (in Chinese)

[11] HUANG Y, LI X J, WANG ZH H, et al.. Finite-time control of satellites formation based on terminal sliding mode［J］. Chinese Journal of Space Science,2014, 34(1): 109-115. (in Chinese)

[12] CHANG L, JIN G, FAN G W, et al.. Small satellite maneuver based on terminal sliding mode control［J］. Opt. Precision Eng., 2015,23(2): 485-496. (in Chinese)

[13] CHEN H. Model Predictive Control［M］. Beijing: Science Press, 2013. (in Chinese)

[14] CHEN L. Research on attitude control of agile small satellite based on SGCMG［D］. Harbin: Dissertation for the Master Degree in Harbin Institute of Technology,2009. (in Chinese)

[15] LIU G, LI CH J, MA G F, et al.. Time efficient controller design for satellite attitude maneuvers using SGCMG ［J］. Acta Aeronautica et Astronautica Sinica, 2011,32(10): 1905-1913. (in Chinese)