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Shaft Speed Control of Laboratory Gas Turbine Engine

机译:实验室燃气轮机轴转速控制

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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:本文提出了一种基于现代控制的系统设计方法,以确保实验室燃气涡轮发动机在各种运行范围之间的稳定性和性能。控制设计的主要目标是计算流向发动机的所需燃料量,以使燃气涡轮发动机的轴速跟踪其指令信号。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的模型上实现,以改善轴速的跟踪响应。使用第一原理开发了燃气涡轮发动机的数学模型,该原理充分捕获了燃气涡轮发动机的稳态以及动态行为。数学模型也已经根据实验数据进行了验证。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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