High angle-of-attack control law design based on global stability analysis

[1] Richard J A, Andrew G S, Siva S B. A gain scheduled multivariable design for a manual flight control system[J]. IEEE Trans on Control Systems Tech, 1992, TM-31(1) :584~589 [2] 范子强. 过失速机动飞机的鲁棒非线性控制律设计及仿真 .北京:北京航空航天大学飞行器设计与应用力学系, 1999 Fan Ziqiang. Robust, nonlinear control design and simulation of post-stall maneuvering aircraft . Beijing:Dept. of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, 1999(in Chinese) [3] 陆启韶. 常微分方程的定性方法和分叉[M]. 北京:北京航空航天大学出版社,1993 Lu Qishao. Theory of ordinary differential equations and bifurcation analysis . Beijing:Beijing University of Aeronautics and Astronautics Press, 1993(in Chinese) [4] Andry A N, Shapiro E Y, Chung J C. Eigenstructure assignment for linear system[J]. IEEE Trans Aerospace & Electronics systems, 1983, Aes-19(5):711~729 [5] Vannelli A, Vidyasagar M. Maximal lyapunov functions and domain of attraction for autonomous nonlinear systems[J]. Automatica, 1985, 21(1):69~80 [6] Genesio R, Tartaglia M, Vicino A. On the estimation of asymptotic stability regions:state of the art and new proposals[J]. IEEE Trans on Automatic Control,1985, AC-30(8):574~581 [7] Chiang H, Hirsch M W, Wu F. Stability regions of nonlinear dynamical systems[J]. IEEE Trans on Automatic Control,1988, AC-33(1):16~27 [8]Taylor J H, Skow A M. F5E departure warning system algorithm development and validation[J]. Journal of Aircraft, 1988, 25(9):783~790 [9]Amitabh S, Girish D, Debasish G. Synthesis of nonlinear controller to recover an unstable aircraft from poststall regime[J]. Journal of Guidance, Control and Dynamics, 1999, 22(5):710~717 [10] 季海波,武际可.分叉问题及其数值方法[J].力学进展,1993,23(4):493~502 Ji Haibo, Wu Jike. Bifurcation and its numerical methods[J]. Advances in Mechanics, 1993,23(4):493~502(in Chinese) [11] 黎 康,方振平. 分叉分析方法在大迎角控制律设计中的应用[J]. 航空学报,2003,24(4):289~292 Li Kang, Fang Zhenping. Application of bifurcation analysis to high-angle-of-attack control law design[J]. Acta Aeronautica et Astronautica Sinica, 2003,24(4):289~292(in Chinese)