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A predictor-based model reference adaptive controller for aircraft with center of gravity variations

  • Peking University

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

Abstract

The center of gravity variations have a direct impact on the control characteristic of the plane, which makes the control system design more complicated. In order to solve this problem, this paper puts forward the predictor-based model reference adaptive controller design method. the core part of this method is composed of three axis nonlinear dynamic inversion controller. Predictor-based model reference adaptive controller is added to the system as adaptive augmentation. System defines two error signals which improve the control accuracy. Simulation results show that this method has a stronger inhibitory effect on uncertainty, it make the system track command signal very well.

Original languageEnglish
Title of host publicationProceedings of the 32nd Chinese Control Conference, CCC 2013
PublisherIEEE Computer Society
Pages3079-3082
Number of pages4
ISBN (Print)9789881563835
StatePublished - 18 Oct 2013
Externally publishedYes
Event32nd Chinese Control Conference, CCC 2013 - Xi'an, China
Duration: 26 Jul 201328 Jul 2013

Publication series

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

Conference

Conference32nd Chinese Control Conference, CCC 2013
Country/TerritoryChina
CityXi'an
Period26/07/1328/07/13

Keywords

  • Center of gravity
  • adaptive
  • dynamic inversion
  • nonlinear

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