Online actuator parameter estimation method for aero-engine control system

被引:0
|
作者
Ji, Chunsheng [1 ,2 ]
Wang, Yuan [2 ]
Lu, Junjie [2 ]
机构
[1] School of Power and Energy, Northwestern Polytechnical University, Xi’an,710072, China
[2] Aero Engine Control System Institute, Aero Engine Corporation of China, Jiangsu, Wuxi,214063, China
来源
关键词
In order to solve the problem of performance degradation that consequently reduces the engine control quality and even endangers the engine operation safety; a method of estimating the real-time state and performance variation trend for the actuator was proposed. Considering the measurable signals of practical aero-engine servo actuator were less than the performance parameters; a adaptive estimation method of combined state was put forward by means of recognition and classification of the actuation pattern; the balanced current of electro-hydraulic servo in the steady state was estimated by unscented Kalman filter; the actuation gain and actuation time delay in the dynamic state were estimated by the method of Broyden-Fletcher-Goldforb-Shanno (BFGS); the performance parameters were updated in real time; and the adaptive model of servo actuator was established. A vane servo actuator loop of turbofan engine was simulated. The simulation results showed that; when single servo parameter can be measured; the absolute error of balance current estimation was less than ±0.2 mA; the relative error of actuation gain estimation was less than 4%; and the absolute error of actuation delay period estimation was less than one control period in different actuation states; and the adaptive model can estimate the state of actuator accurately and track the performance variation trend in real time; so the method can provide technical support of the control loop design and fault diagnosis for aero-engine servo actuator. © 2024 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved;
D O I
10.13224/j.cnki.jasp.20220574
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [1] A temperature modeling method for the servo actuator of aero-engine
    Liu, Xiaoxue
    Yin, Yaobao
    Xu, Yang
    Xu, Yan
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2025,
  • [2] Identification method for parameter uncertain model of aero-engine
    Bai J.
    Liu S.
    Wang W.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2020, 35 (01): : 178 - 184
  • [3] Clamp assembly stress test of aero-engine and assembly parameter control method
    Liu Z.
    Jia D.
    Wang X.
    Liu X.
    Gao D.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2020, 35 (02): : 368 - 377
  • [4] Convex Polyhedron Construction Based Parameter Estimation for Aero-engine Polynomial Linear Parameter Varying System
    Han, Xiaobao
    Wang, Zhongsheng
    SECOND INTERNATIONAL SYMPOSIUM ON COMPUTATIONAL INTELLIGENCE AND DESIGN, VOL 2, PROCEEDINGS, 2009, : 279 - 282
  • [5] Actuator Fault-Tolerant Control for Aero-Engine Control System: A Zonotope-Based Approach
    Fu, Shui
    Tang, Wentao
    Wang, Rui
    Wen, Si-Xin
    Sun, Xi-Ming
    IEEE TRANSACTIONS ON INTELLIGENT TRANSPORTATION SYSTEMS, 2024, 25 (11) : 18861 - 18871
  • [6] Stability analyzation of aero-engine distributed control system
    Peng, Jing-Bo
    Xie, Shou-Sheng
    Wu, Wei
    Sun, Dong
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (10): : 2362 - 2367
  • [7] Method study on fault-tolerant dispatch of the control system of the aero-engine
    Yan Feng
    Shang Yongfeng
    Li Meng
    Wei Wuguo
    Zuo Yuyu
    2013 25TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2013, : 4111 - 4116
  • [8] FDIA simulation of aero-engine control system sensor FDIA system
    College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    Hangkong Dongli Xuebao, 2008, 2 (396-400):
  • [9] Assessment method of structural efficiency on bearing system in aero-engine
    Ma Y.-H.
    Cao C.
    Li X.
    Hong J.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2016, 31 (02): : 274 - 281
  • [10] CONTROL OF QUALITY IN AN AERO-ENGINE FACTORY
    TREWIN, ET
    AIRCRAFT ENGINEERING, 1976, 48 (07): : 9 - &