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Pseudo Euler-Lagrange and Piecewise Affine Control Applied to Surge and Stall in Axial Compressors

机译:伪欧拉-拉格朗日和分段仿射控制应用于轴流压缩机的喘振和失速

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摘要

This thesis addresses the control of the axial compressor surge and stall phenomena using Pseudo Euler-Lagrange and Piecewise Affine (PWA) controller synthesis techniques. These phenomena are considered as major gas turbine compressor instabilities that may result in failures such as the engine flame-out or severe mechanical damages caused by high blade vibration. The common approach towards the detection of the rotating stall and surge is to install various types of pressure sensors, hot wires and velocity probes. The inception of the rotating stall and surge is recognized by the presence of pressure fluctuation and velocity disturbances in the gas stream that are obtained through sensors. The necessary measure is then taken by applying proper stall and surge stabilizing control actions. The Lyapunov stability of pseudo Euler-Lagrange systems in the literature is extended to include additional nonlinear terms. Although Lyapunov stability theory is considered as the cornerstone of analysis of nonlinear systems, the generalization of this energy-based method poses a drawback that makes obtaining a Lyapunov function a difficult task. Therefore, proposing a method for generating a Lyapunov function for the control synthesis problem of a class of nonlinear systems is of potential importance. A systematic Lyapunov-based controller synthesis technique for a class of second order systems is addressed in this thesis. It is shown, in terms of stability characteristics, that the proposed technique provides a more robust solution to the compressor surge suppression problem as compared to the feedback linearization and the backstepping methods. The second contribution is a proposed new PWA approximation algorithm. Such an approximation is very important in reducing the complexity of nonlinear systems models while keeping the global validity of the models. The proposed method builds upon previous work on piecewise affine (PWA) approximation methods, which can be used to approximate continuous functions of n-variables by a PWA function. Having computed the PWA model of the stall and surge equations, the suppression problem is then solved by using PWA synthesis techniques. The proposed solution is shown to have higher damping characteristics as compared to the backstepping nonlinear method.
机译:本文采用伪欧拉-拉格朗日和分段仿射(PWA)控制器综合技术来控制轴向压缩机喘振和失速现象。这些现象被认为是燃气涡轮压缩机的主要不稳定性,可能导致诸如发动机熄火或由于叶片高振动而引起的严重机械损坏等故障。检测旋转失速和喘振的常用方法是安装各种类型的压力传感器,热线和速度探头。通过传感器获得的气流中压力波动和速度干扰的存在,可以识别出旋转失速和喘振的开始。然后通过采取适当的失速和电涌稳定控制措施来采取必要的措施。伪Euler-Lagrange系统的Lyapunov稳定性在文献中得到扩展,以包括其他非线性项。尽管Lyapunov稳定性理论被认为是非线性系统分析的基石,但是这种基于能量的方法的推广存在一个缺点,即使得获得Lyapunov函数成为一项艰巨的任务。因此,提出一种针对一类非线性系统的控制综合问题生成李雅普诺夫函数的方法具有潜在的重要性。本文针对一类二阶系统提出了一种基于Lyapunov的系统控制器综合技术。从稳定性方面来看,与反馈线性化和反推方法相比,所提出的技术为压缩机喘振抑制问题提供了更可靠的解决方案。第二个贡献是提出了一种新的PWA近似算法。这种近似对于降低非线性系统模型的复杂性同时保持模型的整体有效性非常重要。所提出的方法建立在分段仿射(PWA)逼近方法的先前工作的基础上,该方法可用于通过PWA函数逼近n变量的连续函数。计算了失速和喘振方程的PWA模型,然后使用PWA综合技术解决了抑制问题。与反向非线性方法相比,所提出的解决方案具有更高的阻尼特性。

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