Citation: | Chai Xue, Wang Ganglin, Wu Zheet al. Aileron control and reconfiguration of flying wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(12): 1511-1515. (in Chinese) |
[1] Moody L A.The history and future of flight control simulation .AIAA-2004-5149,2004 [2] 杨伟.容错飞行控制系统[M].西安:西北工业大学出版社,2007:107-114 Yang Wei.Fault tolerance flying control system [M].Xi-an: Northwestern Polytechnic University Press,2007:107-114(in Chinese) [3] 马松辉, 吴成富, 陈怀民.飞翼飞机稳定性与操纵性研究[J].飞行力学,2006,24(3): 17-23 Ma Songhui, Wu Chengfu, Chen Huaimin. Study on stability and maneuverability of flying wing aircraft [J].Flight Dynamics,2006,24(3): 17-23(in Chinese) [4] Burken J J. Reconfigurable flight control designs with application to the X-33 vehicle .AIAA-99-4134, 1999 [5] 冯巧玲.自动控制原理[M].北京:北京航空航天大学出版社, 2003:67-71 Feng Qiaoling. Automatic control theory [M].Beijing:Beijing University of Aeronautics and Astronautics Press, 2003: 67-71(in Chinese) [6] 吴森堂,费玉华.飞行控制系统[M].北京:北京航空航天大学出版社,2005: 52-79 Wu Sentang, Fei Yuhua. Aircraft control system [M].Beijing: Beijing University of Aeronautics and Astronautics Press,2005: 52-79(in Chinese) [7] Esteban S. Static and dynamic analysis of an unconventional plane: flying wing .AIAA-2001-4010, 2001 [8] 李林,马超,王立新.大展弦比飞翼构型的横航向操纵特性[J].北京:航空航天大学学报,2007,33(10):1186-1190 Li Lin,Ma Chao, Wang Lixin. Lateral-directional control characteristics of high aspect-ratio flying wing configurations [J]. Beijing: Journal of Beijing University of Aeronautics and Astronautics, 2007,33(10):1186-1190(in Chinese) [9] 王青,孙蕊.基于特征结构配置的导弹可重构控制器设计[J].北京:北京航空航天大学学报,2008,34(3):304-306 Wang Qing, Sun Rui.Reconfigurable controller design for missile using eigen structure assignments [J].Beijing: Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(3):304-306(in Chinese) [10] Tournes C, Shtessel Y B. Sliding mode control for tailless aircraft .AIAA-97-3633, 1997 [11] Dmitriev V G,Shkadov L M,Denisov V E,et al.The flying-wing concept-chances and risks .AIAA-2003-2887,2003 [12] Davidson R W.Flight control design and test of the joint unmanned combat air system(J-UCAS) X-45A .AIAA-2004-6557,2004
|