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 28 条
  • [1] [Anonymous], 2021, LIU SHUOSHUO RES AFT
  • [2] [Anonymous], 2013, SAE TECHNICAL PAPERS
  • [3] [Anonymous], 2010, AERO ENGINE, V36, P54
  • [4] CONTROL OF AN AIRCRAFT ELECTRIC FUEL PUMP DRIVE
    CATHEY, JJ
    WEIMER, JA
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1988, 24 (02) : 171 - 176
  • [5] Electric Power Transfer Concept for Enhanced Performance of the More Electric Engine
    Enalou, Hossein Balaghi
    Bozhko, Serhiy
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2021, 143 (09):
  • [6] Demonstrating the more electric engine: a step towards the power optimised aircraft
    Hirst, M.
    McLoughlin, A.
    Norman, P. J.
    Galloway, S. J.
    [J]. IET ELECTRIC POWER APPLICATIONS, 2011, 5 (01) : 3 - 13
  • [7] Husband M., 2015, DISTRIBUTED ELECT AE
  • [8] Jaw L.C., 2010, Aircraft Engine Controls: Design, System Analysis, and Health Monitoring, V1st
  • [9] Neural network inverse control techniques for PD controlled robot manipulator
    Jung, S
    Hsia, TC
    [J]. ROBOTICA, 2000, 18 (03) : 305 - 314
  • [10] Kraikitrat K., 2011, INT C ELECT MACHINES, P20