| 飞行控制系统鲁棒性分析 |
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| 引用本文： | 王忠俊 徐笑萍. 飞行控制系统鲁棒性分析[J]. 飞行力学, 1994, 12(1): 90-96 |
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| 作者姓名： | 王忠俊 徐笑萍 |
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| 作者单位： | 西北工业大学，西北税务学校 |
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| 基金项目： | 航空科学基金、西工大青年科学基金 |
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| 摘 要： | 简要叙述了特性结构配置及奇异摄动法，介绍了用系统回差矩阵奇异值计算各回路幅值裕量、相位裕量的稳定变化范围，最后以某飞机纵向小扰动运动为例，设计直接力控制律，分析了两种设计方法所设计的控制系统鲁棒性，展示了上述方法的应用。
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| 关 键 词： | 奇异摄动法 鲁棒性 飞行控制系统 |
ROBUSTNESS ANALYSIS OF FLIGHT CONTROL SYSTEM BY USING RETURN DIFFERENCE MATRIX |
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| Wang Zhongjun,Jiang Yunxiang. ROBUSTNESS ANALYSIS OF FLIGHT CONTROL SYSTEM BY USING RETURN DIFFERENCE MATRIX[J]. Flight Dynamics, 1994, 12(1): 90-96 |
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| Authors: | Wang Zhongjun Jiang Yunxiang |
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| Affiliation: | Wang Zhongjun;Jiang Yunxiang(Northwesteru Polytechuical University)Xu Xiaoping(Northwestern Tax School) |
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| Abstract: | Based on the achievements of previous works,the following problems areincluded in this paper.Abrief introduction of eigenstructure assignment method andsingular perturbation method of flight control system design is given. It introduces mini-mum singular value of return difference matrix to calculate stability margin of closedloop system. Finally,one design example of direct lift control is presented to illustratedabove method. |
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| Keywords: | Eigenstructure assignment singular perturbation method Re-turn difference matrix Minimum singular value Robustness |
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