[1]Liberzon D. Switching in systems and control [M]. Boston, MA: Birkhauser, 2003.[2]Liberzon D, Morse A S. Basic problems in stability and design of switched systems [J]. IEEE Control Systems Magazine, 1999, 19(5): 5970.[3]Jiang J, Yu X. Faulttolerant control systems: A comparative study between active and passive approaches [J]. Annual Reviews in Control, 2012, 36(1): 6072.[4]Guler M, Clements S, Wills L M, et al. Transition management for reconfigurable hybrid control systems [J]. IEEE Control Systems Magazine, 2003, 23(1): 3649.[5]Zhang Y M, Jiang J. Bibliographical review on reconfigurable faulttolerant control systems [J]. Annual Reviews in Control, 2008, 32(2): 229252.[6]Zhang Y M, Jiang J. Issues on integration of fault diagnosis and reconfigurable control in active faulttolerant control systems [C]∥The 6th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes. Beijing, China: [s.n.], 2006: 15131524.[7]Jiang J. Design of reconfigurable control system using eigenstructure assignment [J]. International Journal of Control, 1994, 59(2): 395410.[8]Tao G, Joshi S M, Ma X. Adaptive state feedback and tracking control of systems with actuator failures [J]. IEEE Transactions on Automatic Control, 2001, 46(1): 7895.[9]Ye D, Yang G H. Adaptive faulttolerant tracking control against actuator faults with application to flight control [J]. IEEE Transactions on Control Systems Technology, 2006, 14(6): 10881096.[10]Alwi H, Edwards C. Fault detection and faulttolerant control of a civil aircraft using a slidingmodebased scheme [J]. IEEE Transactions on Control Systems Technology, 2008, 16(3): 499510.[11]Jin J, Ko S, Ryoo C K. Fault tolerant control for satellites with four reaction wheels [J]. Control Engineering Practice, 2008, 16(10): 12501258.[12]Almeida F A D, Leibling D. Faulttolerant model predictive control with flighttest results [J]. AIAA Journal of Guidance, Control and Dynamics, 2010, 33(2): 363375.[13]Hu Q, Xiao B, Zhang Y M. Faulttolerant attitude control for spacecraft under loss of actuator effectiveness [J]. AIAA Journal of Guidance, Control and Dynamics, 2011, 34(3): 927932.[14]Yu X, Jiang J. Faulttolerant flight control system design against control surface impairments [J]. IEEE Transactions on Aerospace and Electronic Systems, 2012, 48(2): 10311051.[15]Zhang Y M, Jiang J. Integrated active faulttolerant contorl using IMM approach [J]. IEEE Transactions on Aerospace and Electronic Systems, 2001, 37(4): 12211235.[16]Hu J S, Yin D J, Hori Y. Faulttolerant traction control of electric vehicles [J]. Control Engineering Practice, 2011, 19(2): 204213.[17]Staroswiecki M, Yang H, Jiang B. Progressive accommodation of parametric faults in linear quadratic control [J]. Automatica, 2007, 43(2): 20702076.[18]Alwi H, Edwards C. Faulttolerant control using sliding modes with online control allocation [J]. Automatica, 2008, 44(7): 18591866.[19]Benosman M, Lum K Y. Online references shaping and control realloction for nonlinear fault tolerant control [J]. IEEE Transactions on Control Systems Technology, 2009, 18(1): 152163.[20]Lombaerts T J J, Chu Q P, Mulder J A, et al. Modular flight control reconfiguration design and simulation [J]. Control Engineering Practice, 2011, 19(6): 540554.[21]Hanus R, Kinnaert M, Henrotte J. Conditioning technique, a framework antiwindup and bumpless transfer method [J]. Automatica, 1987, 23(6): 729739.[22]Edwards C, Postlethwaite I. Antiwindup and bumplesstransfer schemes [J]. Automatica, 1998, 34(2): 199210.[23]Turner M C, Walker D J. Linear quadratic bumpless transfer [J]. Automatica, 2000, 36(8): 10891101.[24]Zaccarian L, Teel A R. The L2 bumpless transfer problem for linear plants: its definition and solution [J]. Automatica, 2005, 41(7): 12731280.[25]Zheng K, Basar T, Bentsman J. H∞ bumpless transfer under controller uncertainty [J]. IEEE Transactions on Automatic Control, 2009, 54(7): 17181723.[26]Zheng K, Lee A H, Bentsman J, et al. Steadystate bumpless transfer under controller uncertainty using the state/output feedback topology [J]. IEEE Transactions on Control Systems Technology, 2006, 14(1): 317.[27]Yu X, Jiang J. Hybrid faulttolerant flight control system design against partial actuator failures [J]. IEEE Transactions on Control Systems Technology, 2012, 20(4): 871886.[28]Zhao Q, Jiang J. Reliable state feedback control systems design against actuator failures [J]. Automatica, 1998, 34(10): 12671272.[29]Chen S H, Tao G, Joshi S M. On matching conditions for adaptive state tracking control of systems with actuator failures [J]. IEEE Transactions on Automatic Control, 2002, 47(3): 473478.[30]Forsell L, Nilsson U. ADMIRE the aerodata model in a research environment [R]. Stockholm, Sweden: [s. n.], 2005: 147. |