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Fault diagnosis and active fault tolerant control for near space vehicle based on adaptive observer

  • Yufei Xu*
  • , Bin Jiang
  • , Zhang Ren
  • , Zhifeng Gao
  • *Corresponding author for this work
  • Nanjing University of Aeronautics and Astronautics

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

Abstract

In this paper, Takagi-Sugeno (T-S) fuzzy modeling for Near Space Vehicle (NSV) is first introduced. The nonlinear dynamics of NSV are represented by a T-S fuzzy model. The fault diagnosis and active fault-tolerant control (FTC) problems for NSV with actuator fault are then investigated. An adaptive fault diagnosis observer (AFDO) is designed to detect and estimate fault. The residual is defined as the norm of the output error between AFDO and actual system to detect the actuator fault, and an adaptive fault estimation algorithm is proposed to estimate the fault. An active fault tolerant controller is designed by utilizing the diagnostic fault information to compensate for the loss of actuator effectiveness. Finally, simulation results on the longitudinal model of NSV are presented to demonstrate the efficiency of the proposed approach.

Original languageEnglish
Title of host publicationEarth and Space 2010
Subtitle of host publicationEngineering, Science, Construction, and Operations in Challenging Environments - Proceedings of the 12th International Conference
Pages1865-1875
Number of pages11
DOIs
StatePublished - 2010
Event12th International Conference on Engineering, Science, Construction, and Operations in Challenging Environments - Earth and Space 2010 - Honolulu, HI, United States
Duration: 14 Mar 201017 Mar 2010

Publication series

NameProceedings of the 12th International Conference on Engineering, Science, Construction, and Operations in Challenging Environments - Earth and Space 2010

Conference

Conference12th International Conference on Engineering, Science, Construction, and Operations in Challenging Environments - Earth and Space 2010
Country/TerritoryUnited States
CityHonolulu, HI
Period14/03/1017/03/10

Keywords

  • Accuracy
  • Control systems
  • Spacecraft

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