FDIA System for Sensors of the Aero-Engine Control System Based on the Immune Fusion Kalman Filter

被引:8
|
作者
Gou, Linfeng [1 ]
Sun, Ruiqian [1 ]
Han, Xiaobao [1 ]
机构
[1] Northwestern Poly Tech Univ, Sch Power & Energy, Xian 710129, Peoples R China
关键词
AIRCRAFT; DIAGNOSTICS;
D O I
10.1155/2021/6662425
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The Kalman filter plays an important role in the field of aero-engine control system fault diagnosis. However, the design of the Kalman filter bank is complex, the structure is fixed, and the parameter estimation accuracy in the non-Gaussian environment is low. In this study, a new filtering method, immune fusion Kalman filter, was proposed based on the artificial immune system (AIS) theory and the Kalman filter algorithm. The proposed method was used to establish the fault diagnosis, isolation, and accommodation (FDIA) system for sensors of the aero-engine control system. Through a filtering calculation, the FDIA system reconstructs the measured parameters of the faulty sensor to ensure the reliable operation of the aero engine. The AIS antibody library based on single sensor fault was constructed, and with feature combination and library update, the FDIA system can reconstruct the measured values of multiple sensors. The evaluation of the FDIA system performance is based on the Monte Carlo method. Both steady and transient simulation experiments show that, under the non-Gaussian environment, the diagnosis and isolation accuracy of the immune fusion Kalman filter is above 95%, much higher than that of the Kalman filter bank, and compared with the Kalman particle filter, the reconstruction value is smoother, more accurate, and less affected by noise.
引用
收藏
页数:17
相关论文
共 50 条
  • [21] 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
  • [22] A novel analytical redundancy method based on decision-level fusion for aero-engine sensors
    Jin, Peng
    Zhou, Xin
    Lu, Feng
    Huang, Jinquan
    Qin, Haiqin
    Gao, Yahui
    NONLINEAR DYNAMICS, 2023, 111 (14) : 13215 - 13234
  • [23] Kalman Filter Based Detection of FDIA on a Hybrid Nonlinear Hydro-power Plant Control System Model
    Babunski, Darko
    Poposki, Filip
    Koleva, Radmila
    Zaev, Emil
    Rath, Gerhard
    2022 11TH MEDITERRANEAN CONFERENCE ON EMBEDDED COMPUTING (MECO), 2022, : 286 - 289
  • [24] Model reference adaptive control for aero-engine based on system equilibrium manifold expansion model
    Liu, Xiaofeng
    Zhang, Liming
    Luo, Chenshuang
    INTERNATIONAL JOURNAL OF CONTROL, 2023, 96 (04) : 883 - 898
  • [25] Condition monitoring for aero-engine based on chaos exponents of dynamic system
    Li, Tian-Liang
    He, Li-Ming
    Cheng, Bang-Qin
    Zou, Shi-Jun
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2008, 23 (11): : 2133 - 2136
  • [26] Development of aero-engine corrosion sensitivity test system
    Ma, Pingchang
    Liu, Yue
    Gao, Fei
    Rui, Peng
    Xu, Haibo
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2024, 39 (10):
  • [27] 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
  • [28] Study of system monitoring and fault diagnosis for aero-engine
    Chen, Zhiying
    Tuijin Jishu/Journal of Propulsion Technology, 1998, 19 (05): : 52 - 54
  • [29] An industrial CT system for monitoring a running aero-engine
    常铭
    肖永顺
    陈志强
    NuclearScienceandTechniques, 2014, 25 (06) : 26 - 32
  • [30] Fault Detection and Diagnosis for Sensor in an Aero-Engine System
    Zhao, Zhen
    Sun, Yi-gang
    Zhang, Jun
    PROCEEDINGS OF THE 28TH CHINESE CONTROL AND DECISION CONFERENCE (2016 CCDC), 2016, : 2977 - 2982