Stability Margin Analysis in Multiobjective Design: Application to an Aerospace Launcher
نویسندگان
چکیده
To check the stability margins the designers commonly use the graphical method which is very constraining when the verification 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. Copyright c ©2005 IFAC
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تاریخ انتشار 2005