Sidi M J. Spacecraft dynamics and control: a practical engineering approach. London: Cambridge University Press, 1997.
[2]
Wie B, Lu J B. Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints. Journal of Guidance, Control, and Dynamics, 1995, 18(6): 1372-1379.
[3]
Sharma R, Tewari A. Optimal nonlinear tracking of spacecraft attitude maneuvers. IEEE Transactions on Control Systems Technology, 2004, 12(5): 677-682.
[4]
Dalsmo M, Egeland O. State feedback H∞ suboptimal control of a rigid spacecraft. IEEE Transactions on Automatic Control, 1997, 42(8): 1186-1191.
[5]
Hu Q L, Shi P, Gao H J. Adaptive variable structure and commanding shaped vibration control of flexible spacecraft. Journal of Guidance, Control, and Dynamics, 2007, 30(3): 804-815.
[6]
Hu Q L. Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits. Nonlinear Dynamics, 2009, 55(4): 301-321.
[7]
Hung J Y, Gao W, Hung J C. Variable structure control: a survey. IEEE Transactions on Industrial Electronics, 1993, 40(1): 2-22.
[8]
Crassidis J L, Markley F L. Sliding mode control using modified Rodrigues parameters. Journal of Guidance, Control, and Dynamics, 1996, 19(6): 1381-1383.
[9]
Hu Q L. Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics. Nonlinear Dynamics, 2008, 52(3): 227-248.
[10]
Lim H C, Bang H. Adaptive control for satellite formation flying under thrust misalignment. Acta Astronautica, 2009, 65(1-2): 112-122.
[11]
Zou A M, Kumar K D. Adaptive attitude control of spacecraft without velocity measurements using Chebyshev neural network. Acta Astronautica, 2010, 66(5-6): 769- 779.
[12]
Hu Q L. Robust adaptive sliding mode attitude control and vibration damping of flexible spacecraft subject to unknown disturbance and uncertainty. Transactions of the the Institute of Measurement and Control, 2012, 34(4): 436-447.
[13]
Wang J Y, Sun Z W. 6-DOF robust adaptive terminal sliding mode control for spacecraft formation flying. Acta Astronautica, 2012, 73(5): 76-87.
[14]
Blanke M. Diagnosis and fault tolerant control. Berlin: Springer Verlag, 2003.
[15]
Jiang J, Yu X. Fault tolerant control systems: a comparative study between active and passive approaches. Annual Reviews in Control, 2012, 36(1): 60-72.
[16]
Zhang Y M, Jiang J. Bibliographical review on reconfigurable fault tolerant control systems. Annual Reviews in Control, 2008, 32(2): 229-252.
[17]
Cai W C, Liao X H, Song Y D. Indirect robust adaptive fault-tolerant control for attitude tracking of spacecraft. Journal of Guidance, Control, and Dynamics, 2008, 31(5): 1456-1463.
[18]
Jin J, Ko S, Ryoo C K. Fault tolerant control for satellites with four reaction wheels. Control Engineering Practice, 2008, 16(10): 1250-1258.
[19]
Hu Q L. Robust adaptive sliding mode fault tolerant control with L2-gain performance for flexible spacecraft using redundant reaction wheels. IET Control Theory and Applications, 2010, 4(6): 1055-1070.
[20]
Hu Q L, Xiao B, Friswell M I. Robust fault tolerant control for spacecraft attitude stabilisation subject to input saturation. IET Control Theory and Applications, 2011, 5(2): 271-282.
[21]
Tsiotras P, Luo J H. Control of underactuated spacecraft with bounded inputs. Automatica, 2000, 36(8): 1153- 1169.
[22]
Boskovic J D, Li S M, Mehra R K. Robust adaptive variable structure control of spacecraft under control input saturation. Journal Guidance, Control, and Dynamics, 2001, 24(1): 14-22.
[23]
Boskovic J D, Li S M, Mehra R K. Robust tracking control design for spacecraft under control input saturation. Journal of Guidance, Control, and Dynamics, 2004, 27(4): 627-633.
