[1] Zhang W G, Li A J, Li G W, et al. Modern flight control system design[M]. Xi'an: Northwestern Polytechnical University Press, 2009: 246-255. (in Chinese) 章卫国, 李爱军, 李广文, 等. 现代飞行控制系统设计[M]. 西安: 西北工业大学出版社, 2009: 246-255.[2] Wang H Y, Xue F, Li Z S, et al. Method study of AOA limiter for large transport category airplanes[J]. Journal of System Simulation, 2009, 20(Suppl): 257-259. (in Chinese) 王华友, 薛峰, 李振水, 等. 大型飞机迎角限制方法研究[J]. 系统仿真学报, 2009, 20(增刊): 257-259.[3] Zhang X P, Chen Z J. A design method on limiter for angle of attack and normal acceleration[J]. Acta Aeronautica et Astronautica Sinica, 1995, 16(1): 87-91. (in Chinese) 张喜平, 陈宗基. 迎角过载边界限制器的设计方法[J]. 航空学报, 1995, 16(1): 87-91.[4] Falkena W, Borst C, Chu Q P, et al. Investigation of practical flight envelope protection systems for small aircraft[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(4): 976-988.[5] Yavrucuk I, Prasad J V R, Unnikrishnan S. Envelope protection for autonomous unmanned aerial vehicles[J]. Journal of Guidance, Control, and Dynamics, 2009, 32(1): 248-261.[6] Yavrucuk I, Prasad J V R. Online dynamic trim and control limit estimation[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(5): 1647-1656.[7] van Oort E R, Chu Q P, Mulder J A, et al. Robust model predictive control of a feedback linearized nonlinear F-16/MATV aircraft model, AIAA-2006-6318[R]. Reston: AIAA, 2006.[8] Krings M, Thielecke F. An integrated approach to predictive flight guidance and envelope protection, AIAA-2012-4712[R]. Reston: AIAA, 2012.[9] Glattfelder A H, Schaufelberger W. Control systems with input and output constraints[M]. London: Springer, 2003: 91-158.[10] Richter H. Control design with output constraints: multi-regulator sliding mode approach with override logic[C]//Proceedings of American Control Conference. Piscataway. NJ: IEEE, 2012: 6166-6171.[11] Blanchini F, Miani S. Set-theoretic mehtods in control[M]. New York: Springer, 2008: 86-94.[12] Richter H. A multi-regulator sliding mode control strategy for output-constrained systems[J]. Automatica, 2011, 47(10): 2251-2259.[13] Gao W B. Variable structure control theory and design method[M]. Beijing: Science Press, 1996: 6-10. (in Chinese) 高为炳. 变结构控制的理论及设计方法[M]. 北京: 科学出版社, 1996: 6-10.[14] Litt J S, Frederick D K, Guo T H. The case for intelligent propulsion control for fast engine response, AIAA-2009-1876[R]. Reston: AIAA, 2009.[15] Branicky M S. Analyzing continuous switching systems: theory and examples[C]//Proceedings of American Control Conference. Piscataway NJ: IEEE, 1994: 3110-3114.[16] Foss A M. Criterion to assess stability of a ‘lowest wins’ control strategy[J]. IEE Proceedings D: Control Theory and Application, 1981, 128(1): 1-8.[17] Johansson M. Piecewise linear control systems[M]. Heidelberg: Springer, 2002: 55-61.[18] Reigelsperger W C, Banda S S, Lemaster D P. Application of multivariable control theory to aircraft control laws, WL-TR-96-3099[R]. Wright-Patterson Air Force Base: Flight Dynamics Directorate, 1996. |