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稳定裕度测试技术研究
引用本文:陈怀民,田宗超,程鹏飞,段晓军. 稳定裕度测试技术研究[J]. 现代电子技术, 2014, 0(16): 120-122,126
作者姓名:陈怀民  田宗超  程鹏飞  段晓军
作者单位:西北工业大学无人机特种技术重点实验室,陕西西安710065
摘    要:针对模型未知或不确定的情况下确定系统的稳定裕度的问题,提出了利用实验方法获得系统的稳定裕度。对于MIMO系统,通过实验方法获得频响矩阵,应用回差矩阵最小奇异值法对稳定裕度进行估计,在实例中应用μ方法进行验证。目前很少有文献介绍利用飞行试验方法直接获取系统稳定裕度的方法,因此该文对于工程中系统稳定裕度的确定有着一定的意义。

关 键 词:MIMO系统  飞行试验  稳定裕度  最小奇异值

Research on stability margin testing technology
CHEN Huai-min,TIAN Zong-chao,CHENG Peng-fei,DUAN Xiao-jun. Research on stability margin testing technology[J]. Modern Electronic Technique, 2014, 0(16): 120-122,126
Authors:CHEN Huai-min  TIAN Zong-chao  CHENG Peng-fei  DUAN Xiao-jun
Affiliation:(National Key Laboratory of Science and Technology on UAV, NWPU, Xi'an 710065, China)
Abstract:In order to determine the stability margin of system under the condition that model is unknown or uncertain,an experimental method is proposed to get system stability margin. For MIMO system,the experimental method is adopted to obtain frequency response matrix,and the minimum singular value method of return difference matrix is used to estimate the stability margin. The u method is applied to verify the results in the instance. At present,there are few literatures to introduce the method that a flight test is performed to obtain the stability margin of a system directly,so the research has a certain significance for de-termining the stability margin of a system.
Keywords:MIMO system  flight test  stability margin  minimum singular value
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