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New algorithmic approach based on integral quadratic constraints for stability analysis of high order models

机译:基于积分二次约束的新算法方法,用于高阶模型的稳定性分析

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To analyze a non linear closed loop which represents a high order aeroelastic model of a large civil aircraft interconnected with non-linearities, an Integral Quadratic Constraints (IQC) approach has been involved. This approach is particularly interesting for two reasons. The first one is that it is possible with the same stability criterion to analyze a large class of stability problems. And the second reason is that the stability criterion is based on a frequency domain inequalities (FDI). Usually the Kalman-Yakubovich-Popov (KYP) lemma is involved to transform this infinite set of inequalities into one linear matrix inequality (LMI). But this kind of approach leads to a strong increase in the number of optimization variables. Consequently a new FDI based algorithmic approach has been developed. Usually the number of FDI to satisfy is infinite. To tackle this problem a specific technique has been developed. It consists in computing a frequency domain where the solution is valid. By an iterative approach this domain is extended until it covers [0, +∞[. In this way the solution obtained from the FDI is necessarily valid on the frequency domain continuum and the number of optimization variables remains limited which makes tractable the IQC approach for high order models.
机译:为了分析非线性闭环,该非线性闭环表示与非线性相互连接的大型民用飞机的高阶空气弹性模型,已经涉及一种积分二次约束(IQC)方法。这种方法尤其有趣,原因有两个。第一个是可以采用相同的稳定性标准来分析大类稳定性问题。第二个原因是稳定标准基于频域不等式(FDI)。通常,卡尔曼-yakubovich-popov(kyp)引理涉及将这种无限的不等式转化为一个线性矩阵不等式(LMI)。但这种方法导致优化变量的数量强劲增加。因此,已经开发了一种新的基于FDI的算法方法。通常,满足的FDI数量是无限的。为了解决这个问题,已经开发了特定的技术。它包括计算解决方案有效的频域。通过迭代方法,此域将扩展到它覆盖[0,+∞[。以这种方式,从FDI获得的解决方案必然适用于频域连续体,优化变量的数量仍然是限制,这使得易于高阶模型的IQC方法。

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