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    Off-Equilibrium Linearization-Based Control of Nonlinear Time-Delay System and Application to a Turbofan Engine

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 010::page 101017-1
    Author:
    Yang, Wenchong
    ,
    Tang, Yifeng
    ,
    Zhou, Wenxiang
    ,
    Yang, Gang
    ,
    Huang, Jinquan
    ,
    Cui, Tao
    DOI: 10.1115/1.4065993
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbofan engines exhibit pronounced nonlinearity due to component characteristics and thermal processes, necessitating linearization to connect engine control with linear control theory. Off-equilibrium linearization offers excellent transient tracking and controller performance, making it ideal for military turbofan engines with rapid acceleration and deceleration. Hardware-in-Loop (HIL) experiments are crucial for verifying controller performance, but time delays in the HIL platform can cause oscillations in state variables when using this linearization method. To address this issue, this paper introduces an off-equilibrium linearization-based control strategy. This strategy employs an off-equilibrium linearized model to approximate the nonlinear time-delay system, followed by designing an H∞ controller for the linear time-delay system. The effectiveness of this approach applied to turbofan engines, including its antidelay and robust tracking capabilities, is validated through simulations, HIL experiments, and semiphysical experiments.
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      Off-Equilibrium Linearization-Based Control of Nonlinear Time-Delay System and Application to a Turbofan Engine

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4302956
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorYang, Wenchong
    contributor authorTang, Yifeng
    contributor authorZhou, Wenxiang
    contributor authorYang, Gang
    contributor authorHuang, Jinquan
    contributor authorCui, Tao
    date accessioned2024-12-24T18:54:17Z
    date available2024-12-24T18:54:17Z
    date copyright8/16/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_146_10_101017.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302956
    description abstractTurbofan engines exhibit pronounced nonlinearity due to component characteristics and thermal processes, necessitating linearization to connect engine control with linear control theory. Off-equilibrium linearization offers excellent transient tracking and controller performance, making it ideal for military turbofan engines with rapid acceleration and deceleration. Hardware-in-Loop (HIL) experiments are crucial for verifying controller performance, but time delays in the HIL platform can cause oscillations in state variables when using this linearization method. To address this issue, this paper introduces an off-equilibrium linearization-based control strategy. This strategy employs an off-equilibrium linearized model to approximate the nonlinear time-delay system, followed by designing an H∞ controller for the linear time-delay system. The effectiveness of this approach applied to turbofan engines, including its antidelay and robust tracking capabilities, is validated through simulations, HIL experiments, and semiphysical experiments.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOff-Equilibrium Linearization-Based Control of Nonlinear Time-Delay System and Application to a Turbofan Engine
    typeJournal Paper
    journal volume146
    journal issue10
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4065993
    journal fristpage101017-1
    journal lastpage101017-15
    page15
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 010
    contenttypeFulltext
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