Decoupling control of a hypersonic gliding vehicle based on NESO

  • Chen Bai*
  • , Zhang Ren
  • , Xingyue Shao
  • *Corresponding author for this work

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

Abstract

According to attitude control of a hypersonic gliding vehicle, a decoupling control approach based on NESO is proposed. Decoupling control is realized through the decentralized control theory. The system coupling terms and uncertainties are estimated by NESO and added into the control law for compensation. Theoretical analysis proves that the tracking errors of the closed-loop system are consistently bounded. Simulations are carried on through the hypersonic gliding vehicle model comparing the proposed method and the traditional sub-channel control method. The results show that the tracking effectiveness of the proposed method is better and impact caused by coupling and uncertainties is eliminated.

Original languageEnglish
Title of host publicationProceedings of the 33rd Chinese Control Conference, CCC 2014
EditorsShengyuan Xu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages2311-2315
Number of pages5
ISBN (Electronic)9789881563842
DOIs
StatePublished - 11 Sep 2014
EventProceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China
Duration: 28 Jul 201430 Jul 2014

Publication series

NameProceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

ConferenceProceedings of the 33rd Chinese Control Conference, CCC 2014
Country/TerritoryChina
CityNanjing
Period28/07/1430/07/14

Keywords

  • Decoupling control
  • Hypersonic gliding vehicle
  • NESO
  • Uncertainties

Fingerprint

Dive into the research topics of 'Decoupling control of a hypersonic gliding vehicle based on NESO'. Together they form a unique fingerprint.

Cite this