基于新型终端滑模的航天器执行器故障容错姿态控制

doi:10.7527/S1000-6893.2013.0298

Abstract

Abstract:

An exponent nonsingular fast terminal sliding mode (ENFTSM) control law is investigated in this paper for a rigid spacecraft with redundant thrusters in which thruster faults, and control input saturation as well as external disturbances have to be explicitly considered simultaneously. More specifically, in this proposed control scheme, fast convergence of spacecraft attitude tracking is achieved and faster reaching time can be guaranteed in comparison with the terminal sliding mode. When thruster fault occurs, the control parameters are adjusted dynamically in such a fashion that no fault detection and isolation mechanism is required in advance, and only the remaining active thrusters are assumed to be able to produce a combined force sufficient to allow the spacecraft to perform the given operations within the saturation magnitude. Lyapunov stability analysis shows that the resulting closed-loop system is stable it can withstand the effect of external disturbances, control input saturation and even faults by appropriately choosing the design parameters. The attitude tracking performance using the controller is evaluated through a numerical example.

Key words: spacecraft, actuator fault, control constraint, fault tolerant control, terminal sliding mode

CLC Number:

V448.2
TP13

HU Qinglei, JIANG Boyan, SHI Zhong. Novel Terminal Sliding Mode Based Fault Tolerant Attitude Control for Spacecraft Under Actuator Faults[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(1): 249-258.

References

[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.

Novel Terminal Sliding Mode Based Fault Tolerant Attitude Control for Spacecraft Under Actuator Faults

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