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Active and Passive Fault Tolerant Control for Winged Aircraft with Simultaneous Actuator and Sensor Faults

  • Xingguang Xu
  • , Changrong Chen*
  • , Zhang Ren
  • , Shusheng Li
  • *Corresponding author for this work
  • CAS - Institute of Mechanics
  • Beihang University

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

Abstract

Fault-tolerant control problems for the winged aircraft systems with simultaneous actuator and sensor faults are investigated via the T-S fuzzy observer and finite time integral sliding approach. Firstly, to ensure the fault amplitude to be estimated and the control input to be extracted explicitly, the T-S fuzzy model and Lie derivative are introduced to describe the winder aircraft longitudinal flight model respectively, and a more general sensor and actuator time-varying fault model is furthermore developed. Then an approach to decouple sensor faults from actuator faults is proposed. Sufficient conditions to achieve the sensor fault diagnosis and estimation using adaptive law are proposed. Moreover, based on the filtered sensor signals, a passive fault-tolerant control strategy using finite time integral sliding mode is proposed for winged aircraft with actuator faults. The obtained results suggest an effective way to maintain acceptable performance in the case that actuator and sensor faults occur simultaneously. Numerical simulations validate the effectiveness of the proposed approach.

Original languageEnglish
Title of host publicationProceedings of 2019 Chinese Intelligent Systems Conference - Volume III
EditorsYingmin Jia, Junping Du, Weicun Zhang
PublisherSpringer Verlag
Pages679-708
Number of pages30
ISBN (Print)9789813296978
DOIs
StatePublished - 2020
EventChinese Intelligent Systems Conference, CISC 2019 - Haikou, China
Duration: 26 Oct 201927 Oct 2019

Publication series

NameLecture Notes in Electrical Engineering
Volume594
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceChinese Intelligent Systems Conference, CISC 2019
Country/TerritoryChina
CityHaikou
Period26/10/1927/10/19

Keywords

  • Actuator and sensor
  • Fault-tolerant control
  • Finite time integral sliding mode
  • T-S fuzzy observer
  • Winded aircraft

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