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歼击机的鲁棒反馈控制器设计
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)
作者姓名:胡寿松  胡中汉
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)
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。

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
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)
Authors:Hu Shousong Hu Zhonghan
Affiliation:Department of Automatic Control
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.
Keywords:flight control systems   fighter   robust control   feedback controller   design method
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