Research on afterburning control of more electric engine with a nonlinear fuel supply system

被引:2
|
作者
Xi, Zhihua [1 ,4 ]
Wang, Yong [1 ]
Zhang, Haibo [1 ]
Sun, Fengyong [2 ]
Zheng, Qiangang [1 ]
Zhu, Zhemin [3 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R China
[2] Wuxi Univ, Coll Automat Engn, Wuxi, Peoples R China
[3] Shenyang Engine Res Inst, Shenyang, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, 29 Yudao St, Qinhuai Dist, Nanjing 210016, Peoples R China
关键词
more electric engine; afterburner fuel actuator; dead-zone characteristics; stability control; co-simulation;
D O I
10.1177/09544100231155696
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
More electric engine (MEE) with electric pump metering fuel has the problem of unstable engine control due to the dead-zone characteristics of afterburner fuel actuator. On the basis of conventional mu modified adaptive control method, a compound modified adaptive control (CMAC) system based on neural network inverse model is proposed in this study. At first, the afterburner fuel actuator model of MEE is established through Simulink/AMESim co-simulation to study its fuel supply characteristics and reveal the reasons for dead-zone characteristics of the actuator. Subsequently, an integrated model of afterburner fuel actuator/MEE is established to investigate the effect of dead-zone characteristics on engine performance. Finally, the CMAC system for afterburner fuel flow closed-loop control based on neural network inverse model and improved mu modified adaptive control method is designed. The simulation results show that the dead-zone characteristics of afterburner fuel actuator can cause engine shaking and unstable operation. The engine thrust has a continuous fluctuation with amplitude of about 0.2%. The proposed CMAC system can effectively avoid the dead-zone interval of actuator and achieve stable transition of the engine state in the entire operating range of the afterburner fuel actuator. Thus, the stability of the control system can be significantly improved. Meanwhile, the improved mu modified adaptive control algorithm in the CMAC system has better dynamic characteristics when compared with the conventional mu modified adaptive control algorithm.
引用
收藏
页码:2647 / 2664
页数:18
相关论文
共 50 条
  • [1] Direct Performance Control Method for Turbofan Afterburning Control with a Nonlinear Fuel Supply System
    Zhihua Xi
    Ming Chen
    Haibo Zhang
    Yong Wang
    International Journal of Aeronautical and Space Sciences, 2024, 25 : 293 - 307
  • [2] Direct Performance Control Method for Turbofan Afterburning Control with a Nonlinear Fuel Supply System
    Xi, Zhihua
    Chen, Ming
    Zhang, Haibo
    Wang, Yong
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2024, 25 (01) : 293 - 307
  • [3] DEVELOPMENT OF FUEL CONTROL SYSTEM FOR MORE ELECTRIC ENGINE
    Seki, Naoki
    Morioka, Noriko
    Oyori, Hitoshi
    Yamamoto, Yasuhiko
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 6, 2015,
  • [4] SIMULATION RESEARCH ON THE AFTERBURNING DYNAMIC CHARACTERISTICS OF ENGINE CONTROL SYSTEM
    Mao Kejiu and Wang XuBeijing University of Aeronautics and Astronautics
    Chinese Journal of Aeronautics, 1990, (01) : 23 - 33
  • [5] DEVELOPMENT OF THE ELECTRIC FUEL SYSTEM FOR THE MORE ELECTRIC ENGINE
    Morioka, Noriko
    Oyori, Hitoshi
    Gonda, Yukinori
    Takamiya, Kenji
    Yamamoto, Yasuhiko
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 6, 2014,
  • [6] FUEL SYSTEM DESIGN FOR THE MORE ELECTRIC ENGINE
    Morioka, Noriko
    Oyori, Hitoshi
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 1, 2012, : 767 - +
  • [7] SIMULATION RESEARCH ON THE AFTERBURNING DYNAMIC CHARACTERISTICS OF ENGINE CONTROL-SYSTEM
    MAO, KJ
    WANG, X
    NINTH INTERNATIONAL SYMPOSIUM ON AIR BREATHING ENGINES, VOLS 1 AND 2: SYMPOSIUM PAPERS, 1989, : 774 - 781
  • [8] Nonlinear optimal control of turbofan engine afterburning process
    School of Power and Energy, Northwestern Polytechnical Univ., Xi'an 710072, China
    Tuijin Jishu, 2006, 4 (339-344):
  • [9] Study on Control System of Fuel Supply for Scramjet Engine
    Du Yuhuan
    Zhang Xiaodong
    PROCEEDINGS OF THE 2013 IEEE 8TH CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS (ICIEA), 2013, : 342 - 347
  • [10] Research into a Fuel Supply System in the Aircraft Diesel Opposed Engine
    Grabowski, Lukasz
    Sochaczewski, Rafal
    Baranski, Grzegorz
    Bialy, Michal
    2020 IEEE 7TH INTERNATIONAL WORKSHOP ON METROLOGY FOR AEROSPACE (METROAEROSPACE), 2020, : 620 - 624