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    A Model-Based Framework for Dynamic Antiwindup Strategy for Gas Turbine Engine Fuel Control System

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 005::page 06022002
    Author:
    Xiaofeng Liu
    ,
    Chenshuang Luo
    ,
    Enshu Song
    DOI: 10.1061/(ASCE)AS.1943-5525.0001468
    Publisher: ASCE
    Abstract: Fuel control is usually required to work with the acceleration and deceleration schedules to provide limit protection. However, limit protection will deteriorate controller performance. In this work, we investigate a model-based framework for gas turbine engine fuel control system. First, the gas turbine engine performance degradation due to the actuator saturation in fuel control system is described, and the thermodynamic component-level model and small deviation linear control model are obtained from the experimental data. Then, the problem of antiwindup in gas turbine engine control system is formed and the traditional static antiwindup compensator is introduced. Next, a dynamic antiwindup compensator based on Lyapunov stability is proposed to improve the control performance, and the design of the compensator is formulated and solved in linear matrix inequality framework. One of the notable features of the proposed approach is that the original controller does not need to redesign, and its previous control performance remains unchanged in set-point control. Compared with the static compensator in hardware-in-loop simulation, the proposed dynamic compensator can achieve better performance.
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      A Model-Based Framework for Dynamic Antiwindup Strategy for Gas Turbine Engine Fuel Control System

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4287559
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    • Journal of Aerospace Engineering

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    contributor authorXiaofeng Liu
    contributor authorChenshuang Luo
    contributor authorEnshu Song
    date accessioned2022-12-27T20:33:17Z
    date available2022-12-27T20:33:17Z
    date issued2022/09/01
    identifier other(ASCE)AS.1943-5525.0001468.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4287559
    description abstractFuel control is usually required to work with the acceleration and deceleration schedules to provide limit protection. However, limit protection will deteriorate controller performance. In this work, we investigate a model-based framework for gas turbine engine fuel control system. First, the gas turbine engine performance degradation due to the actuator saturation in fuel control system is described, and the thermodynamic component-level model and small deviation linear control model are obtained from the experimental data. Then, the problem of antiwindup in gas turbine engine control system is formed and the traditional static antiwindup compensator is introduced. Next, a dynamic antiwindup compensator based on Lyapunov stability is proposed to improve the control performance, and the design of the compensator is formulated and solved in linear matrix inequality framework. One of the notable features of the proposed approach is that the original controller does not need to redesign, and its previous control performance remains unchanged in set-point control. Compared with the static compensator in hardware-in-loop simulation, the proposed dynamic compensator can achieve better performance.
    publisherASCE
    titleA Model-Based Framework for Dynamic Antiwindup Strategy for Gas Turbine Engine Fuel Control System
    typeJournal Article
    journal volume35
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001468
    journal fristpage06022002
    journal lastpage06022002_8
    page8
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 005
    contenttypeFulltext
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