柔性飞机大尺度LTI模型的降阶LPV模型生成

Charles Poussot-Vassal, C. Roos
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引用次数: 19

摘要

在民用航空工业中,柔性飞机模型通常是在冻结飞行和质量配置下建立和验证的。不幸的是,这些由高保真度数值工具导出的中(大)尺度模型通常不能很好地适应模拟、控制和分析。本文描述了一种从描述给定系统冻结构型的一组中(大)尺度线性时不变(LTI)模型中导出降阶线性参数变化(LPV)模型的方法。提出的方法分为三个步骤:(i)首先,使用SVD-Krylov方法的最新进展应用局部模型近似,(ii)然后,应用适当的基数变化来允许插值,(iii)最后,导出LPV模型并将其转换为适当大小的线性分数表示(LFR)用于分析和控制目的。在一组工业气动弹性飞机模型上对结果进行了全面评估。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Flexible aircraft reduced-order LPV model generation from a set of large-scale LTI models
In the civilian aeronautical industry, flexible aircraft models are often built and validated at frozen flight and mass configurations. Unfortunately, these medium(large)-scale models derived from high fidelity numerical tools are generally not well adapted for simulation, control and analysis. In this paper, a methodology to derive a reduced-order Linear Parameter Varying (LPV) model from a set of medium(large)-scale Linear Time Invariant (LTI) models describing a given system at frozen configurations is described. The proposed methodology is in three steps: (i) first, local model approximation is applied using recent advances in SVD-Krylov methods, (ii) then, an appropriate base change is applied to allow interpolation, (iii) and finally, an LPV model is derived and converted into a Linear Fractional Representation (LFR) of suitable size for analysis and control purposes. Results are thoroughly assessed on a set of industrial aeroelastic aircraft models.
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