| 歼击机的鲁棒反馈控制器设计 |
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| 引用本文： | 胡寿松,胡中汉. 歼击机的鲁棒反馈控制器设计[J]. 南京航空航天大学学报, 1990, 0(2) |
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| 作者姓名： | 胡寿松 胡中汉 |
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| 作者单位： | 南京航空学院自动控制系(胡寿松)，南京航空学院自动控制系(胡中汉) |
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| 摘 要： | 本文应用时域多变量鲁棒控制方法设计歼击机的飞行控制系统。设计出的鲁棒控制器具有固定的设计参数和增益。在模型误差、参数波动和歼击机气动特性显著变化的情况下,可以保证飞行稳定并有良好的动态响应。
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| 关 键 词： | 飞行控制系统 歼击机 鲁棒控制 反馈控制器 设计方法 |
The Design of Robust Feedback Controller for a Fighter Aircraft |
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| Hu Shousong Hu Zhonghan. The Design of Robust Feedback Controller for a Fighter Aircraft[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1990, 0(2) |
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| Authors: | Hu Shousong Hu Zhonghan |
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| Affiliation: | Department of Automatic Control |
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| Abstract: | In this paper, the design of the control system of a [fighter by means of multivariable robuts feedback controller in the time domain is presented. The robust control system designed has fixed parameters and gain to ensure the stability and a well suited dynamical input-output behaviour of the closed loop system, under the condition of the model error, parameter fluctuations and the significant aerodynamic behaviour variations of the fighter. |
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| Keywords: | flight control systems fighter robust control feedback controller design method |
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