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STABILITY MARGIN ANALYSIS IN MULTIOBJECTIVE DESIGN: APPLICATION TO AN AEROSPACE LAUNCHER

机译:多目标设计中的稳定性裕度分析:在航空航天发射器中的应用

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To check the stability margins the designers commonly use the graphical method which is very constraining when the verication must be done several times, as for instance when a routine is to be developped. In this paper a practical method is proposed, based on the Kalman-Yakubovich-Popov (KYP) lemma. This method avoids the conservatism induced by H∞ analysis and a huge calculation as the one derived by μ-analysis.
机译:为了检查稳定性裕度,设计人员通常使用图形方法,这种方法在必须多次进行验证时(例如在开发例程时)会受到很大的限制。本文基于Kalman-Yakubovich-Popov(KYP)引理提出了一种实用的方法。这种方法避免了H∞分析引起的保守性,也避免了μ分析得出的巨大计算量。

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