| [1] Zheng F Y, Yang Y D. Flight control system design of explicit model-following for helicopter based on control distribution matrix decouple[J]. Journal of Naval Aeronautical Engineering Institute, 2007, 22(1): 119-124. (in Chinese) 郑峰婴, 杨一栋. 控制阵解耦的直升机显模型跟踪飞控系统设计[J]. 海军航空工程学院学报, 2007, 22(1): 119-124.[2] Wen P, Lu T W. Decoupling control of a twin rotor MIMO system using robust deadbeat control technique[J]. IET Control Theory & Applications, 2008, 2(11): 999-1007.[3] Ahmed Q, Bhatti A I, Iqbal S. Robust decoupling control design for twin rotor system using Hadamard weights//IEEE Conference on Control Applications, (CCA) & Intelligent Control,(ISIC), 2009: 1009-1014.[4] Wang H Q, Wang D B, Mian A A, et al. Robust tracking decoupled flight control of an unmanned helicopter[J]. Mechanical Science and Technology for Aerospace Engineering, 2009, 28(4): 536-541. (in Chinese) 王宏强, 王道波, Mian Ashfaq Ahmad,等. 无人直升机鲁棒跟踪解耦飞行控制研究[J]. 机械科学与技术, 2009, 28(4): 536-541.[5] Tadayoni S A, Gholami B, Demirli K. Vision-based fuzzy 2D motion control of a model helicopter//Fuzzy Information Processing Society, Annual Meeting of the North American, 2006: 714-719.[6] Zeng L L, Wang D B, Fan C X. An unmanned helicopter decoupling control based on the fuzzy PID control method[J]. Journal of Applied Sciences, 2004, 22(4): 498-502. (in Chinese) 曾丽兰, 王道波, 樊春霞. 基于模糊 PID的无人直升机解耦控制研究[J]. 应用科学学报, 2004, 22(4): 498-502.[7] Xu G F, Chen M. Decoupling analysis between yaw and collective pitch controls of coaxial helicopter using free wake arithmetic[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(2): 249-252. (in Chinese) 徐冠峰, 陈铭. 基于自由尾迹的共轴直升机航向/总距解耦分析[J]. 北京航空航天大学学报, 2011, 37(2): 249-252.[8] Jiang H X, Xu J F, Gao Z, et al. Hover/Landing control for the novel compound unmanned aerial helicopter[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(B5): 46-54. (in Chinese) 蒋鸿翔, 徐锦法, 高正,等. 新型复合式无人直升机悬停/着陆控制[J]. 航空学报, 2008, 29(B5): 46-54.[9] Yuan Z H, Zhang W, Mu X. Adaptive optimal decoupling control in helicopter rotor concordant loading system[J]. China Mechanical Engineering, 2007, 18(22): 2691-2696. (in Chinese) 袁朝辉, 张伟, 穆旭. 直升机旋翼协调加载自适应最优解耦控制[J]. 中国机械工程, 2007, 18(22): 2691-2696.[10] Liu P, Wang Q, Meng Z J, et al. Unmanned helicopter robust controller design based on aircraft flying qualities evaluation[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(9): 1587-1597. (in Chinese) 刘鹏, 王强, 蒙志君,等. 基于飞行品质评估的无人直升机鲁棒控制器设计[J]. 航空学报, 2012, 33(9): 1587-1597.[11] Yang C D, Liu W H. Robust H∞ decoupling hover control of uncertain nonlinear helicopter, AIAA-2003-5489. Reston: AIAA, 2003.[12] Yang C D, Liu W H, Chang P W, et al. Decoupling control for hovering flight vehicle with parameter uncertainties, AIAA-2006-6091. Reston: AIAA, 2006.[13] Zhen Z Y, Wang Z S, Wang D B. Optimal preview tracking control based on information fusion in error system[J]. Control Theory & Applications, 2009, 26(4): 425-428. (in Chinese) 甄子洋, 王志胜, 王道波. 基于误差系统的信息融合最优预见跟踪控制[J]. 控制理论与应用, 2009, 26(4): 425-428.[14] Zhen Z Y, Wang Z S, Wang D B. Information fusion estimation based preview control for discrete linear system[J]. Acta Automatica Sinica, 2010, 36(2): 347-352. (in Chinese) 甄子洋, 王志胜, 王道波. 基于信息融合估计的离散线性系统预见控制[J]. 自动化学报, 2010, 36(2): 347-352.[15] Yang Y D. Helicopter flight control[M]. 2nd ed. Beijing: National Defense Industry Press, 2011: 133-134. (in Chinese) 杨一栋. 直升机飞行控制[M]. 2版. 北京: 国防工业出版社, 2011: 133-134.[16] Wang Z S, Jiang B, Zhen Z Y. Fusion estimation and fusion control[M]. 2nd ed. Beijing: Science Press, 2009: 57-58. (in Chinese) 王志胜, 姜斌, 甄子洋. 融合估计与融合控制[M]. 2版. 北京: 科学出版社, 2009: 57-58. |
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