DLLE-EWMA based Incipient Fault Detection for Satellite Attitude Control System

被引：0
|
作者：
Zhao, Gang [1 ]
Yang, Tia Tianshe [1 ]
Liu, Min [2 ]
Cheng, Yuehua [3 ]
Lu, Ningyun [2 ]
机构：
[1] Xian Satellite Control Ctr, Xian, Shaanxi, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing, Jiangsu, Peoples R China
来源：
2018 CHINESE AUTOMATION CONGRESS (CAC) | 2018年
关键词：
Incipient Fault Detection; Locally Linear Embedding; Satellite Attitude Control System; DIAGNOSIS;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, an incipient fault detection (FD) method that is applied to satellite attitude control system (ACS), is proposed based on the locally linear embedding algorithm with dynamic neighborhood parameters (DLLE) and the exponentially weighted moving average (EWMA) strategy. Dynamic neighborhood parameter selection is introduced to LLE, so that the weight reconstruction matrix can be determined according to the sample density of the manifold. Then, the DLLE algorithm is integrated with EWMA in both the latent and residual subspaces to establish the EWMA-T-2 and EWMA-SPE statistics for incipient fault detection. Case study is conducted using the real telemetry data from two on-orbit satellites, and the results can demonstrate the effectiveness and feasibility of this proposed incipient FD method.
引用
收藏
页码：709 / 714
页数：6
相关论文
共 50 条
  • [1] Data-based Incipient Fault Detection and Prediction for Satellite's Attitude Control System
    Liu Min
    Lu Ningyun
    Cheng Yuehua
    Jiang Bin
    2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2017, : 1202 - 1207
  • [2] Actuator fault detection and isolation for the attitude control system of satellite
    Wang, Zhenhua
    Zhang, Miao
    Shen, Yi
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2013, 45 (02): : 72 - 76
  • [3] On Fault Diagnosis of Satellite Attitude Control System Based On ARRs
    Liu Wenjing
    Liu Chengrui
    2014 33RD CHINESE CONTROL CONFERENCE (CCC), 2014, : 3130 - 3135
  • [4] Small fault detection method for actuator of satellite attitude control system
    Li L.
    Gao Y.
    Wu Z.
    Zhang X.
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 45 (03): : 529 - 537
  • [5] SVM Classifier Based Fault Diagnosis of the Satellite Attitude Control System
    Zhao, Shi-Lei
    Mang, Ying-Chun
    INTERNATIONAL CONFERENCE ON INTELLIGENT COMPUTATION TECHNOLOGY AND AUTOMATION, VOL 2, PROCEEDINGS, 2008, : 907 - 911
  • [6] Fault estimation in satellite attitude control system based on ATSUKF algorithm
    Chen, Xueqin
    Sun, Rui
    Wu, Fan
    Jiang, Wancheng
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (05):
  • [7] Hierarchical fault detection for nano-pico satellite attitude control system
    Fei Y.
    Meng T.
    Jin Z.-H.
    Zhejiang Daxue Xuebao (Gongxue Ban)/Journal of Zhejiang University (Engineering Science), 2020, 54 (04): : 824 - 832
  • [8] Sensor fault detection and recovery in satellite attitude control
    Nasrolahi, Seiied Saeed
    Abdollahi, Farzaneh
    ACTA ASTRONAUTICA, 2018, 145 : 275 - 283
  • [9] Kalman filter innovation sequence based fault detection in LEO satellite attitude determination and control system
    Okatan, A.
    Hajiyev, Ch.
    Hajiyeva, U.
    2007 3RD INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES, VOLS 1 AND 2, 2007, : 411 - +
  • [10] A System for Incipient Fault Detection and Fault Diagnosis Based on MCSA
    Gazzana, Daniel da S.
    Pereira, Luis Alberto
    Fernandes, Denis
    2010 IEEE PES TRANSMISSION AND DISTRIBUTION CONFERENCE AND EXPOSITION: SMART SOLUTIONS FOR A CHANGING WORLD, 2010,
12345