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A structured approach for input derivative index-2 descriptor dynamical model control

机译:输入导数索引2描述符动力学模型控制的结构化方法

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This paper reveals a practical manner to deal with the control design of dynamical systems governed by input derivative index-2 first order differential algebraic equations. This class of dynamical model embeds a polynomial which results in a infinite gain in high frequencies. The idea is grounded on the construction of an adequate SISO controller structure to make possible the control design on a model presenting both rational and a first order polynomial parts. The design approach then leads to a controller in a rational form without any algebraic constrain, which can be implemented on a real-time target. Application for gust load control of a complex aeroservoelastic aircraft dynamical model, which naturally embeds an input derivative action, illustrates the approach, using an H∞-norm minimization performance objective.
机译:本文提出了一种实用的方式来处理由输入导数索引一阶二阶微分代数方程控制的动力学系统的控制设计。此类动力学模型嵌入了一个多项式,该多项式会导致无限大的高频增益。该思想的基础是适当的SISO控制器结构的构建,以使控制设计有可能同时呈现有理多项式和一阶多项式部分。然后,该设计方法将导致一种没有任何代数约束的合理形式的控制器,该控制器可以在实时目标上实现。自然嵌入输入微分作用的复杂航空弹性航空器动力学模型的阵风载荷控制应用说明了使用H∞范数最小化性能目标的方法。

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