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Shaft Speed Control of Laboratory Gas Turbine Engine

机译:实验室燃气轮机轴速控制

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The paper presents a modern control-based system design approach for ensuring stability and performance of a laboratory gas turbine engine, between various operation ranges. The primary objective of the control design is to compute the required fuel flow to the engine such that the shaft speed of a gas turbine engine tracks its commanded signal. A nonlinear controller, using Lyapunov based feedback control technique, is implemented on a physics-based model of the laboratory engine to improve the tracking response of shaft speed. The mathematical model of a gas turbine engine is developed using the First principle which sufficiently captures the steady state, as well as the dynamic behavior of a gas turbine engine. The mathematical model has also been validated against the experimental data. Simulation results indicate that the proposed control design approach is quite successful in obtaining satisfactory performance of the engine.
机译:本文介绍了一种基于现代控制的系统设计方法,可确保实验室燃气轮机在各种操作范围之间的稳定性和性能。控制设计的主要目的是将所需的燃料流量计算到发动机,使得燃气轮机发动机的轴速度跟踪其命令信号。使用基于Lyapunov的反馈控制技术的非线性控制器在实验室发动机的基于物理学模型上实现,以改善轴速的跟踪响应。燃气轮机发动机的数学模型是使用足够捕获稳态的第一个原理,以及燃气轮机发动机的动态行为来开发。数学模型也针对实验数据验证。仿真结果表明,所提出的控制设计方法在获得令人满意的发动机性能方面非常成功。

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