| [1] Hu Q L. Robust Adaptive attitude tracking control with L2-gain performance and vibration reduction of an orbiting flexible spacecraft[J]. Journal of Dynamic Systems, Measurement and Control, 2011, 133(1): 011009.[2] Hu Q L, Ma G F, Xie L H. Robust and adaptive variable structure output feedback control of uncertain systems with input nonlinearity[J]. Automatica, 2008, 44(2): 552-559.[3] Hou Q, Cheng Y H, Lu N Y, et al. Study on FDD and FTC of satellite attitude control system based on the effectiveness factor[C]//The 2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008: 1096-1101.[4] Jiang Y, Hu Q L, Ma G F. Adaptive backstepping fault-tolerant control for flexible spacecraft with unknown bounded disturbances and actuator failures[J]. ISA Transactions, 2010, 49(1): 57-69.[5] Hu Q L, Zhang A H, Li B. Adaptive variable structure fault tolerant control of rigid spacecraft under thruster faults[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(4): 909-918.(in Chinese) 胡庆雷, 张爱华, 李波. 推力器故障的刚体航天器器自适应变结构容错控制[J]. 航空学报, 2013, 34(4): 909-918.[6] Wallsgrove R J, Akella M R. Globally stabilizing saturated attitude control in the presence of bounded unknown disturbances[J]. Journal of Guidance, Control, and Dynamics, 2005, 28(5): 957-963.[7] Huo X, Hu Q L, Xiao B, et al. Variable-structure fault-tolerant attitude control for flexible satellite with input saturation[J]. Control Theory & Applications, 2011, 28(9): 1063-1068. (in Chinese) 霍星, 胡庆雷, 肖冰, 等. 带有饱和受限的挠性卫星变结构姿态容错控制[J]. 控制理论与应用, 2011, 28(9): 1063-1068.[8] Hu Q L. Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits[J]. Nonlinear Dynamics, 2009, 55(4): 301-321.[9] Lu K F, Xia Y Q, Fu M Y. Controller design for rigid spacecraft attitude tracking with actuator saturation[J]. Information Sciences, 2013, 220: 343-366.[10] Ding S H, Li S H, Li Q. Stability analysis for a second-order continuous finite-time control system subject to a disturbance[J]. Journal of Control Theory and Applications, 2009, 7(3): 271-276.[11] Jin E D, Sun Z W. Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control[J]. Aerospace Science and Technology, 2008, 12(4): 324-330.[12] Hu Q L, Huo X, Xiao B, et al. Robust finite-time control for spacecraft attitude stabilization under actuator fault[J]. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2012, 226(4): 416-428.[13] Zou A M, Kumar K D, Hou Z G, et al. Finite-time attitude tracking control for spacecraft using terminal sliding mode and Chebyshev neural network[J]. IEEE Transactions on Systems, Man, and Cybernetics, Part B: Cybernetics, 2011, 41(4): 950-963.[14] Hu Q L, Li B, Zhang A H. Robust finite-time control allocation in spacecraft attitude stabilization under actuator misalignment[J]. Nonlinear Dynamics, 2013, 73(1-2): 53-71.[15] Man Z H, Paplinski A P, Wu H R. A robust MIMO terminal sliding mode control scheme for rigid robotic manipulators[J]. IEEE Transactions on Automatic Control, 1994, 39(12): 2464-2469.[16] Yu S H, Yu X H, Man Z H. Robust global terminal sliding mode control of SISO nonlinear uncertain systems[C]//Proceedings of the 39th IEEE Conference on Decision and Control, 2000, 3: 2198-2203.[17] Feng Y, Yu X H, Man Z. Non-singular terminal sliding mode control of rigid manipulators[J]. Automatica, 2002, 38(9): 2159-2167.[18] Yang L, Yang J Y. Nonsingular fast terminal sliding-mode control for nonlinear dynamical systems[J]. International Journal of Robust and Nonlinear Control, 2010, 21(16): 1865-1879.[19] Li H, Dou L H, Su Z. Adaptive nonsingular fast terminal sliding mode control for electromechanical actuator[J]. International Journal of Systems Science, 2013, 44(3): 401-415.[20] Abramowitz M, Stegun I A. Handbook of mathematical functions: with formulas, graphs, and mathematical tables[M]. New York: Dover Publications, 1972.[21] Yu S H, Yu X H, Shirinzadeh B, et al. Continuous finite-time control for robotic manipulators with terminal sliding mode[J]. Automatica, 2005, 41(11): 1957-1964. |
CJA
