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Polynomial LPV synthesis applied to turbofan engines

机译:多项式LPV综合应用于涡扇发动机

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Results on polynomial fixed-order controller design are extended to SISO gain-scheduling with guaranteed stability and H_∞ performance over the whole scheduling parameter range. Salient features of the approach are: (a) the use of polynomials as modeling objects; (b) the use of flexible linear matrix inequalities (LM1) conditions allowing polynomial dependence of the open-loop system and controller transfer functions in the scheduling parameters; and (c) the decoupling in the LMI conditions between the Lyapunov variables and the controller variables, allowing both parameter-dependent Lyapunov functions and fixed-order controller design. The synthesis procedure is integrated into the ATOL framework developed by the manufacturer of aircraft and space engines Snecma to systematically design reduced complexity gain-scheduled control laws for aircraft turbofan engines.
机译:多项式固定阶控制器设计的结果扩展到SISO增益调度,在整个调度参数范围内具有保证的稳定性和H_∞性能。该方法的突出特点是:(a)使用多项式作为建模对象; (b)使用灵活的线性矩阵不等式(LM1)条件,允许调度参数中的开环系统和控制器传递函数具有多项式依赖性; (c)Lyapunov变量和控制器变量之间在LMI条件下的解耦,从而允许依赖于参数的Lyapunov函数和固定顺序控制器设计。综合程序被集成到飞机和航天发动机制造商斯奈克玛公司开发的ATOL框架中,以系统地设计降低复杂度的飞机涡扇发动机增益计划控制律。

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