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Quasi-LPV Model of a NDI-Controlled Missile Based on Function Substitution

机译:基于功能替代的NDI控制导弹的准LPV模型

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The paper presents an example how a nonlinear missile model controlled by a nonlinear dynamic inversion (NDI) based feedback structure can be approximated by a linear fractional representation (LFR). The aim is to obtain an LFR of suitable complexity for applying LFT-based robust stability analysis. The first step is the transformation of the nonlinear closed loop into a quasi linear parameter varying (LPV) system via a method called function substitution. In the second step the nonlinear dependencies in the quasi-LPV model, which are not rational in the parameters, are approximated using polynomial fitting based on ?_1 -regularized least squares. Using this approach an almost Pareto front between the accuracy and complexity of the resulting LFR can be easily obtained. The quality of the closed loop LFR is assessed by using Monte-Carlo simulations.
机译:本文提出了一种示例,该示例如何通过线性分数表示(LFR)来近似由非线性动态反转(NDI)的反馈结构的非线性导弹模型。目的是获得适当复杂性的LFR,用于应用基于LFT的鲁棒稳定性分析。第一步是通过称为功能替换的方法将非线性闭环转换为准线性参数变化(LPV)系统。在第二步中,使用基于Δ_1-Regular化最小二乘的多项式拟合来近似于参数的Quasi-LPV模型中的非线性依赖性。使用这种方法可以容易地获得所得LFR的精度和复杂性之间的几乎帕累托正面。通过使用Monte-Carlo模拟来评估闭环LFR的质量。

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