Citation: | ZHANG Ping, CHEN Zong-ji. Reconfiguration of Control Surface Faults with Thrust Vectoring Technique[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(3): 257-260. (in Chinese) |
[1]Napolitano M R, Swaim R L. New technique for aircraft flight control reconfiguration[J]. J Gidance, 1991,14(1):184~190. [2]Chiang C, Youssef H M. Neural network approach to aerodynamic coefficients estimation and aircraft failure isolation design . AIAA943599,1994. [3]Ochi Y. Application of feedback linearization method in a digital restructurable flight control systems[J]. J of Gidance, Control and Dynamics, 1993,16(1):111~117. [4]张 平,陈宗基. 飞机操纵面故障研究及其补偿重构[J]. 飞行力学, 1997,15(3):67~72. [5]Waiker L A. Flight testing the X36the test pilot's perspective .NASA Contract NAS, 1997, 214269. [6]高彦玺. 推力矢量控制与过失速机动研究 . 北京:北京航空航天大学飞行器设计与应用力学系,1997. [7]李俊杰编. 矩阵分析[M].北京:机械工业出版社,1995.
|