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Application of fractional-order calculus in sliding mode control for hypersonic vehicles

  • Haidong Liu
  • , Weimin Bao
  • , Huifeng Li
  • , Chunye Gong
  • , Yuxin Liao
  • Beihang University
  • Science and Technology on Space Physics Laboratory
  • National University of Defense Technology

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

Abstract

In this paper, fractional-order calculus (FC) is applied in the sliding mode control of a generic hypersonic vehicle (GHV). In the design of the controller, dynamic inversion is applied to deal with strong couplings among pitch angle, yaw angle and roll angle. The effect of FC is evaluated in a sliding mode controller. Simulation results demonstrate that sliding mode controller becomes more robust and damping characteristic is strengthened by use of FC.

Original languageEnglish
Title of host publicationProceedings of the 35th Chinese Control Conference, CCC 2016
EditorsJie Chen, Qianchuan Zhao, Jie Chen
PublisherIEEE Computer Society
Pages936-940
Number of pages5
ISBN (Electronic)9789881563910
DOIs
StatePublished - 26 Aug 2016
Event35th Chinese Control Conference, CCC 2016 - Chengdu, China
Duration: 27 Jul 201629 Jul 2016

Publication series

NameChinese Control Conference, CCC
Volume2016-August
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference35th Chinese Control Conference, CCC 2016
Country/TerritoryChina
CityChengdu
Period27/07/1629/07/16

Keywords

  • control
  • dynamic inversion
  • fractional-order
  • hypersonic vehicle
  • sliding mode

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