Feedback linearization control for HRV attitude control based on high order disturbance observer

Hongru Jiang, Yuanqing Xia*, Ganghui Shen, Dailiang Ma, Qun Cao

*Corresponding author for this work

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

1 Citation (Scopus)

Abstract

High response speed, coupling dynamics and nonlinearities of hypersonic re-entry vehicles (HRVs) makes the attitude control a significant technology. This paper proposes a feedback linearization control scheme based on backstepping technology design for attitude tracking control of HRV in the presence of disturbances. In the proposed control design scheme, the higher order disturbance observer (HODO) is adopted to estimate and compensate for the disturbances. Then the convergence of HODO and stability of closed-loop system are presented. Finally, simulation results are given to illustrate the effectiveness of the proposed method.

Original languageEnglish
Title of host publicationProceedings of the 37th Chinese Control Conference, CCC 2018
EditorsXin Chen, Qianchuan Zhao
PublisherIEEE Computer Society
Pages10037-10042
Number of pages6
ISBN (Electronic)9789881563941
DOIs
Publication statusPublished - 5 Oct 2018
Event37th Chinese Control Conference, CCC 2018 - Wuhan, China
Duration: 25 Jul 201827 Jul 2018

Publication series

NameChinese Control Conference, CCC
Volume2018-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference37th Chinese Control Conference, CCC 2018
Country/TerritoryChina
CityWuhan
Period25/07/1827/07/18

Keywords

  • Backstepping technology
  • Feedback linearization
  • HRV
  • Higher order disturbance observer

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