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Discrete-time actuator fault estimation design for flight control application

  • Jiong Sang Yee
  • , Bin Jiang
  • , Jian Liang Wang*
  • , Yan Li
  • *Corresponding author for this work

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

Abstract

This paper proposes a new discrete-time fault estimation scheme that deals with multiple, simultaneous and abrupt actuator failures. The proposed actuator fault estimation scheme is applied to design a fault-tolerant H flight controller for a combat aircraft in tracking bank-angle and pitch-rate commands with zero lateral acceleration. Simulation results demonstrate good performance using the fault-tolerant H flight controller.

Original languageEnglish
Title of host publicationProceedings of the 7th International Conference on Control, Automation, Robotics and Vision, ICARCV 2002
PublisherNanyang Technological University
Pages1287-1292
Number of pages6
ISBN (Print)9810483643, 9789810483647
DOIs
Publication statusPublished - 2002
Externally publishedYes
Event7th International Conference on Control, Automation, Robotics and Vision, ICARCV 2002 - Marine Mandarin, Singapore
Duration: 2 Dec 20025 Dec 2002

Publication series

NameProceedings of the 7th International Conference on Control, Automation, Robotics and Vision, ICARCV 2002
Volume1

Conference

Conference7th International Conference on Control, Automation, Robotics and Vision, ICARCV 2002
Country/TerritorySingapore
CityMarine Mandarin
Period2/12/025/12/02

ASJC Scopus subject areas

  • General Engineering

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