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Nonlinear stability and post-critical analysis of an uncertain plant with Describing Functions and Integral Quadratic Constraints

机译:具有描述函数和积分二次约束的不确定工厂的非线性稳定性和临界后分析

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摘要

Two approaches to tackle the nonlinear robust stability problem of a plant are considered. The first employs a combination of the Describing Function method and μ analysis, while the second makes use of Integral Quadratic Constraints (IQCs). The model analyzed consists of an open-loop wing's airfoil subject to freeplay and LTI parametric uncertainties.One of the main contributions of the work is to provide methodologies to quantitatively determine the post-critical behaviour of the system, known as Limit Cycle Oscillation (LCO). When the first approach is adopted, this is studied by means of a worst-case LCO curve, whose definition is given in the paper. The IQC framework, typically used to find asymptotic stability certificates, is applied to this scenario by introducing a restricted sector bound condition for the nonlinearity.
机译:考虑了两种解决工厂非线性鲁棒稳定性问题的方法。第一种方法使用描述函数方法和μ分析的组合,而第二种方法则使用积分二次约束(IQC)。分析的模型由开环机翼的翼型组成,该翼型受到自由游隙和LTI参数不确定性的影响。这项工作的主要贡献之一是提供了定量确定系统的临界后行为的方法,称为极限循环振荡(LCO)。 )。当采用第一种方法时,将通过最坏情况的LCO曲线对其进行研究,其定义已在本文中给出。通常用于查找渐近稳定性证书的IQC框架通过为非线性引入受限的扇区约束条件而应用于此方案。

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