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切换系统的无扰切换控制及其在航空发动机中的应用

赵颖 付俊 赵军

赵颖, 付俊, 赵军.切换系统的无扰切换控制及其在航空发动机中的应用.自动化学报, 2020, 46(10): 2165-2176 doi: 10.16383/j.aas.c190007
引用本文: 赵颖, 付俊, 赵军.切换系统的无扰切换控制及其在航空发动机中的应用.自动化学报, 2020, 46(10): 2165-2176 doi: 10.16383/j.aas.c190007
Zhao Ying, Fu Jun, Zhao Jun. Bumpless transfer control for switched systems and its application to aero-engines. Acta Automatica Sinica, 2020, 46(10): 2165-2176 doi: 10.16383/j.aas.c190007
Citation: Zhao Ying, Fu Jun, Zhao Jun. Bumpless transfer control for switched systems and its application to aero-engines. Acta Automatica Sinica, 2020, 46(10): 2165-2176 doi: 10.16383/j.aas.c190007

切换系统的无扰切换控制及其在航空发动机中的应用

doi: 10.16383/j.aas.c190007
基金项目: 

国家自然科学基金 61773098

详细信息
    作者简介:

    赵颖   东北大学信息科学与工程学院博士研究生.主要研究方向为切换系统的控制设计, 无扰切换控制, 航空发动机控制设计.
    E-mail: zhaoying198916@163.com

    付俊  东北大学流程工业综合自动化国家重点实验室教授.主要研究方向为动态优化, 切换系统, 非线性控制.
    E-mail: junfu@mail.neu.edu.cn

    通讯作者:

    赵军  东北大学信息科学与工程学院教授.主要研究方向为切换系统, 混杂控制, 非线性系统, 鲁棒控制.本文通信作者.
    E-mail: zhaojun@ise.neu.edu.cn

  • 本文责任编委 倪茂林

Bumpless Transfer Control for Switched Systems and Its Application to Aero-engines

Funds: 

the National Natural Science Foundation of China 61773098

More Information
    Author Bio:

    ZHAO Ying   Ph.D. candidate at the College of Information Science and Engineering, Northeastern University. Her research interest covers control design of switched systems, bumpless transfer control methods, and aero-engine control design

    FU Jun   Professor at the State Key Laboratory of Synthetical Automation for Process Industries, Northeastern University. His research interest covers dynamic optimization, switching systems, and nonlinear control

    Corresponding author: ZHAO Jun   Professor at the College of Information Science and Engineering, Northeastern University. His research interest covers switched systems, hybrid control, nonlinear systems, and robust control. Corresponding author of this paper
  • Recommended by Associate Editor NI Mao-Lin
  • 摘要: 利用多Lyapunov函数方法, 本文研究了一类切换线性系统的状态跟踪无扰切换控制问题.首先, 刻画了控制信号在切换时刻处的抖振抑制水平.其次, 通过控制器与切换律的同时设计, 实现了系统的状态跟踪和控制信号抖振抑制.最后, 将所提出的状态跟踪无扰切换控制策略应用于一个涡扇航空发动机模型的控制设计上, 说明了所提出方法的有效性.
    Recommended by Associate Editor NI Mao-Lin
    1)  本文责任编委 倪茂林
  • 图  1  切换信号

    Fig.  1  The switching signals

    图  2  燃油流量变化

    Fig.  2  The fuel flow increments

    图  3  风扇转速跟踪误差

    Fig.  3  The tracking errors of the fan speed

    图  4  核心机转速跟踪误差

    Fig.  4  The tracking errors of the core speed

    图  5  切换信号

    Fig.  5  The switching signals

    图  6  燃油流量变化

    Fig.  6  The fuel flow increments

    图  7  风扇转速跟踪误差

    Fig.  7  The tracking errors of the fan speed

    图  8  核心机转速跟踪误差

    Fig.  8  The tracking errors of the core speed

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出版历程
  • 收稿日期:  2019-01-03
  • 录用日期:  2019-05-19
  • 刊出日期:  2020-10-29

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