A novel tracking control method for a flexible air-breathing hypersonic vehicle

Jian Feng Cui, Ke Zhang, Mei Bo Lv

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

Abstract

This paper is focused on developing a non-fragile state feedback tracking control for a flexible air-breathing hypersonic vehicle under the condition that the elastic modal is not measured. First, the linear model of the FAHV is obtained under given trim condition by using Jacobian linearization. Second, through treating flexibility as the input disturbance, the non-fragile state feedback controller has been designed to stabilize the closed-loop systems and reduce the fragility encountered in controller implementation. Linear matrix inequalities constraints are formulated for designing a velocity and altitude tracking controller. Finally, numerical simulations have demonstrated the effectiveness of the proposed approach.

Original languageEnglish
Title of host publication2013 IEEE International Conference of IEEE Region 10, IEEE TENCON 2013 - Conference Proceedings
DOIs
StatePublished - 2013
Event2013 IEEE International Conference of IEEE Region 10, IEEE TENCON 2013 - Xi'an, Shaanxi, China
Duration: 22 Oct 201325 Oct 2013

Publication series

NameIEEE Region 10 Annual International Conference, Proceedings/TENCON
ISSN (Print)2159-3442
ISSN (Electronic)2159-3450

Conference

Conference2013 IEEE International Conference of IEEE Region 10, IEEE TENCON 2013
Country/TerritoryChina
CityXi'an, Shaanxi
Period22/10/1325/10/13

Keywords

  • elastic modal
  • flexible air-breathing hypersonic vehicle
  • non-fragile state feedback control
  • tracking control

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