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Generation of a reduced-order LPV/LFT model from a set of large-scale MIMO LTI flexible aircraft models

机译:从一组大型MIMO LTI柔性飞机模型中生成降阶LPV / LFT模型

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In the civilian aviation industry, the aeroelastic behavior of an aircraft is often modeled at frozen flight and mass configurations using high fidelity numerical tools. Unfortunately, the resulting large-scale models cannot be handled in such form by modem analysis and control techniques, which generally require the considered models to be written as low-order Linear Fractional Representations (LFR). In this context, a methodology is described to derive a reduced-order Linear Parameter Varying (LPV) model from a reference set of large-scale Multiple Input Multiple Output (MIMO) Linear Time Invariant (LTI) models describing a given system at frozen configurations. The proposed approach is in two steps. The reference models are first reduced using recent advances in Krylov methods, leading to a set of low-order state-space representations with consistent state vectors. An LPV model is then obtained by polynomial approximation and converted into an LFR of reasonable size. A special effort is made to avoid data overfitting by using as simple as possible approximation formulas. The method is applied to a long-range commercial aircraft model developed in an industrial context: a set of large-scale flexible models linearized at different mass configurations is converted into a single low-order LPV model. More generally, any kind of purely numerical models for which the analytical structure is unknown can be considered.
机译:在民用航空业中,通常使用高保真数值工具在冻结的飞行和质量配置下对飞机的气动弹性行为进行建模。不幸的是,所得的大规模模型不能通过调制解调器分析和控制技术以这种形式处理,这通常需要将考虑的模型写为低阶线性分数表示(LFR)。在此上下文中,描述了一种方法,该方法可从大规模多输入多输出(MIMO)线性时不变(LTI)模型的参考集中得出低阶线性参数变化(LPV)模型,该模型描述了冻结配置下的给定系统。提议的方法分两个步骤。首先使用Krylov方法的最新进展来简化参考模型,从而得到一组具有一致状态向量的低阶状态空间表示。然后通过多项式逼近获得LPV模型,并将其转换为合理大小的LFR。通过使用尽可能简单的近似公式,为避免数据过度拟合做出了特别的努力。该方法应用于在工业环境中开发的远程商用飞机模型:将在不同质量配置下线性化的一组大型柔性模型转换为单个低阶LPV模型。更一般地,可以考虑分析结构未知的任何种类的纯数值模型。

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