| 基于智能软件的着舰飞行/推力控制系统 |
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| 引用本文： | 贾忠湖,侯志强,李冀鑫,庞向征,王春城.基于智能软件的着舰飞行/推力控制系统[J].飞行力学,2009,27(1). |
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| 作者姓名： | 贾忠湖 侯志强 李冀鑫 庞向征 王春城 |
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| 作者单位： | 1. 海军航空工程学院,飞行器工程系,山东,烟台,264001
2. 中国人民解放军,91498部队,河北,秦皇岛,066200 |
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| 摘 要： | 针对舰载飞机在低动压状态下操纵性能下降导致航迹角不能精确跟踪姿态角的问题,基于设计多变量鲁棒控制系统的正规矩阵参数优化方法,采用智能设计软件IntelDes 3.0设计了保持迎角恒定的着舰飞行/推力综合控制系统.非线性数值仿真结果表明,该控制系统的性能较好,对气动系数摄动的鲁棒性较强.
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| 关 键 词： | 舰载飞机 着舰 控制系统 智能设计 |
Carrier Landing Flight/Thrust Control System Based on Intelligent Design Software |
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| JIA Zhong-hu,HOU Zhi-qiang,LI Ji-xin,PANG Xiang-zheng,WANG Chun-cheng.Carrier Landing Flight/Thrust Control System Based on Intelligent Design Software[J].Flight Dynamics,2009,27(1). |
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| Authors: | JIA Zhong-hu HOU Zhi-qiang LI Ji-xin PANG Xiang-zheng WANG Chun-cheng |
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| Institution: | 1.Department of Aircraft Engineering;NAEI;Yantai 264001;China;2.The 91498 Unit of PLA;Qinhuangdao 066200;China |
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| Abstract: | Due to the degradation of aircraft handling characteristics in low dynamic pressure situation when approaching and landing on a carrier,flight path angle can not track attitude angle precisely.So based on the theory of optimization of the parameterized normal matrix,the integrated flight/thrust control system was designed using the intelligent design software of IntelDes 3.0.And the nonlinear numerical simulation shows that performance of this control system is good and its robust is satisfying. |
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| Keywords: | carrier-based aircraft carrier landing control system intelligent design |
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