A new robust fault-tolerant control strategy for aircraft with asymmetric structure damage

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Abstract

This paper focuses on the control problem of the aircraft with asymmetric structure damage. The contribution of this study is to present a new robust fault-tolerant control strategy based on nonlinear extended state observer and nonlinear dynamic inverse, which well balances the system performance and the tolerance of damage. Firstly, the dynamic model of the aircraft with asymmetric structure damage is built adopting micro-element method. Meanwhile, the damaged aircraft control problem can be transformed into the problem of the suppression and adaptation of uncertain factors. Finally, simulations are carried on to demonstrated the control law based on the proposed strategy with NASA Generic Transport Model. Results show that the aircraft tracks the control commands quickly and accurately and the flight performance is well ensured after asymmetric structure damage occurring.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages7438-7442
Number of pages5
ISBN (Electronic)9789881563934
DOIs
StatePublished - 7 Sep 2017
Event36th Chinese Control Conference, CCC 2017 - Dalian, China
Duration: 26 Jul 201728 Jul 2017

Publication series

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

Conference

Conference36th Chinese Control Conference, CCC 2017
Country/TerritoryChina
CityDalian
Period26/07/1728/07/17

Keywords

  • asymmetric structure damage
  • dynamic inverse control
  • extended state observer
  • robust fault-tolerant control

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