| 具有相对稳定性的鲁棒飞行控制系统设计方法 |
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| 引用本文： | 胡寿松,朱勇.具有相对稳定性的鲁棒飞行控制系统设计方法[J].南京航空航天大学学报,1990(1). |
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| 作者姓名： | 胡寿松 朱勇 |
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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(朱勇) |
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| 摘 要： | 本文提出了一种改进的稳定鲁棒飞行控制系统设计方法。当飞机气动参数在不同飞行状态下相应变化时,控制器可保证飞行控制系统始终稳定,同时具有要求的动态性能。
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| 关 键 词： | 飞行控制系统 鲁棒控制 相对稳定性 仿真 |
Design Method of Robust Flight Control System with Relative Stability |
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| Hu Shousong Zhu Yong.Design Method of Robust Flight Control System with Relative Stability[J].Journal of Nanjing University of Aeronautics & Astronautics,1990(1). |
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| Authors: | Hu Shousong Zhu Yong |
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| Institution: | Department of Automatic Control |
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| Abstract: | In this paper,an improved design method of flight control systems with stable robustness is introduced.When airplane pneumatic parameters change in different flying states,the controller can ensure the stability and the dynamic property requirements of the flight control system. A specific design of a certain type of flight control system is also introduced and satisfactory simulation results are obtained. |
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| Keywords: | flight control sytem robust control relative stability simulation |
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