| 飞机侧向控制系统的鲁棒稳定性设计 |
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| 引用本文： | 赵军,毛剑琴. 飞机侧向控制系统的鲁棒稳定性设计[J]. 航空学报, 1990, 11(12): 610-616 |
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| 作者姓名： | 赵军 毛剑琴 |
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| 作者单位： | 北京航空航天大学(赵军)，北京航空航天大学(毛剑琴) |
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| 摘 要： | 1.前言 一个设计优良的反馈控制系统应当在对象含有不确定性的情形下，满足稳定性、动态特性和鲁棒稳定性的要求。
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| 关 键 词： | 多变量 鲁棒性 飞机侧向控制 |
THE DESIGN OF ROBUSTNESS STABILITY OF AIRCRAFT LATERAL CONTROL SYSTEM |
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| Beijing University of Aeronautics and Astronautics Zhao Jun and Mao Jianqin. THE DESIGN OF ROBUSTNESS STABILITY OF AIRCRAFT LATERAL CONTROL SYSTEM[J]. Acta Aeronautica et Astronautica Sinica, 1990, 11(12): 610-616 |
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| Authors: | Beijing University of Aeronautics and Astronautics Zhao Jun and Mao Jianqin |
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| Affiliation: | Beijing University of Aeronautics and Astronautics Zhao Jun and Mao Jianqin |
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| Abstract: | The Reversed-Frame-Normalizing (RFN) method is employed to analyse and design the robustness of aircraft lateral control system. In comparison with Inverse Nyquist-Array (IKA) method, the RFN method for the system could not only design the stability and dynamic performances but also provide robustness with respect to plant uncertainty. Numerical results are presented for a two-input/two-output lateral control system of a high-altitude and high-speed fighter. |
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| Keywords: | multivariable robustness aircraft lateral control system. |
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