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Kalman-based fault-tolerant control system for aeroengines

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

In this paper a fault-tolerant control system based on Kalman filter is presented to realize fault-tolerant control when there are multiples in aeroengine system. In this fault-tolerant control system, the fault estimation process and fault-tolerant regulation process is combined into one process to reduce the time cost of fault-tolerant control process, and the performance of the control system will be improved. The fault-tolerant regulator in this system is able to adjust its structure to adopt to different fault situations. According to the simulation results, the Kalman-based fault-tolerant control system is able to locate the faulty ones, estimate the variations of faults and minimize the influence of faults when the sensor faults and actuator faults coexist.

Original languageEnglish
Title of host publicationProceedings of the 38th Chinese Control Conference, CCC 2019
EditorsMinyue Fu, Jian Sun
PublisherIEEE Computer Society
Pages5085-5088
Number of pages4
ISBN (Electronic)9789881563972
DOIs
StatePublished - Jul 2019
Event38th Chinese Control Conference, CCC 2019 - Guangzhou, China
Duration: 27 Jul 201930 Jul 2019

Publication series

NameChinese Control Conference, CCC
Volume2019-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference38th Chinese Control Conference, CCC 2019
Country/TerritoryChina
CityGuangzhou
Period27/07/1930/07/19

Keywords

  • Actuator fault
  • Aeroengine
  • Fault estimator
  • Kalman filter
  • Onboard model
  • Sensor fault
  • Switching structure

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