Integrated reconfigurable flight control method for aircraft with multiple control effectors

[1] Brinker J S,Wise K A．Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft ．AIAA-2000-3941,2000 [2] Bennani S,Sluis R,Schram G, et al．Control law reconfiguration using robust linear parameter varying control ．AIAA-99-4137,1999 [3] Boskovic J D,Mehra R K．Robust fault-tolerant control design for aircraft under state-dependent disturbances ．AIAA 2003-5490,2003 [4] Burken J J,Lu P,Wu Z L,et al．Two reconfigurable flight-control design methods:robust servomechanism and control allocation [J]．Journal of Guidance, Control and Dynamics,2001,24(3):482-493 [5] Joosten D A,Boom T J J, Lombaerts T J J．Computationally efficient use of MPC and dynamic inversion for reconfigurable flight control ．AIAA 2008-7431,2008 [6] Zhu J J．Nonlinear tracking and decoupling by trajectory linearization ．NASA Marshall Space Flight Center,1998 [7] Bevacqua T,Best E,Huizenga A,et al．Improved trajectory linearization flight controller for reusable launch vehicles ．AIAA 2004-875,2004 [8] Zhu J J．PD-spectral theory for multivariable linear time-varying systems Peshkin M．Proceeding of the 36th Conference on Decision & Control．San Diego:IEEE Control Systems Society,1997:3908-3913 [9] Yang Lingyu,Shen Gongzhang．A new optimal control allocation method for aircraft with multiple control effectors ．AIAA 2007-1052,2007 [10] 杨凌宇,钟友武,申功璋．多操纵面飞机控制分配的非线性闭环迭代结构 程代展,吴敏．第26届中国控制会议论文集(第四册)．北京:北京航空航天大学出版社,2007:755-757 Yang Lingyu,Zhong Youwu,Shen Gongzhang．The nonlinear iterative closed loop configuration of control allocation for aircraft with multiple control effectors Cheng Daizhan,Wu Min．Proceeding of the 26^th Chinese Control Conference(Volume 4)．Beijing:Beijing University of Aeronautics and Astronautics Press,2007:755-757 (in Chinese)