| 基于非线性动态逆的飞机控制规律仿真 |
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| 引用本文： | 贾忠湖,齐红德,侯志强. 基于非线性动态逆的飞机控制规律仿真[J]. 海军航空工程学院学报, 2007, 22(1): 125-128 |
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| 作者姓名： | 贾忠湖 齐红德 侯志强 |
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| 作者单位： | 海军航空工程学院飞行器工程系,山东烟台,264001;海军驻沈阳地区航空军事代表室,辽宁沈阳,110034 |
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| 摘 要： | 介绍了采用非线性动态逆方法对常规飞机的各回路进行的控制规律解算,并以某型飞机为模型进行仿真,结果表明,该控制规律解算能提供精确的纵向和横向控制,具有良好的指令跟踪性能。
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| 关 键 词： | 非线性动态逆 控制律 飞行仿真 |
| 修稿时间： | 2006-09-30 |
Design and simulation of aircraft control law based on the nonlinear dynamic inversion |
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| JIA Zhonghu,QI Hongde and HOU Zhiqiang. Design and simulation of aircraft control law based on the nonlinear dynamic inversion[J]. Journal of Naval Aeronautical Engineering Institute, 2007, 22(1): 125-128 |
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| Authors: | JIA Zhonghu QI Hongde HOU Zhiqiang |
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| Affiliation: | Department of Airborne Vehicle Engineering,NAEI,Yantai,264001,Aeronautical Military Representatives Office of Navy in Shenyang,Shenyang,Liaoning,110034 and Department of Airborne Vehicle Engineering,NAEI,Yantai,264001 |
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| Abstract: | Nonlinear dynamic inversion methods are adopted to design control law of each loop for general aircraft. And taking a fighter plane for example, simulation according to relevant theory is accomplished. The result shows that this law has a good performance of command tracing. |
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| Keywords: | nonlinear dynamic inversion control law flight simulation |
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