Citation: | Wang Xinmin, Xiao Yahui, Deng Wan, et al. Robust control law design for fixed-wing airplane coordinated turns[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(7): 762-765,781. (in Chinese) |
[1] 白蒲江,王新民,余翔.基于迭代LMI的直升机协调转弯控制律设计[J].测控技术,2008,27(7):86-88 Bai Pujiang,Wang Xinmin,Yu Xiang.ILMI-based optimal control law design for helicopter coordinated turns[J].Measurement &Control Technique,2008,27(7):86-88(in Chinese) [2] Walker B,Saraf A,Godbole A.Robust flight control for coordinated turns[R].AIAA-2003-5553,2003 [3] Wichai Siwakosit.Robust and reconfigurable flight control system design[J].Mechanical and Aeronautical Engineering,2001,62(7):110-114 [4] Rozak J N,Ray A.Robust multivariable control of rotorcraft in forward flight [J].Journal of the American Helicopter Society,1997,42(2):149-160 [5] David Cabecinhas,Carlos Silvestre,Paulo Rosa,et al.Path-following control for coordinated turn aircraft maneuvers[R].AIAA-2007-6656,2007 [6] 孙秀霞,毛剑琴.基于LMI的降阶鲁棒控制器设计[J].北京航空航天大学学报,2000,26(6):722-725 Sun Xiuxia,Mao Jianqin.Robust reduced-order controller design based on LMI[J].Journal of Beijing University of Aeronautics and Astronautics,2000,26(6):722-725(in Chinese) [7] 俞立.鲁棒控制——线性矩阵不等式处理方法[M].北京:清华大学出版社,2002:41-44 Yu Li.Robust—LMI approach.[M].Beijing:Tsinghua University Press,2002:41-44(in Chinese)
|