The propulsion/flight dynamics coupling analysis for air-breathing hypersonic vehicle

Dong Zhang, Shuo Tang

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

2 Scopus citations

Abstract

The airframe/propulsion integration configuration, brought strong couplings between aerodynamic and propulsion system, making modeling and control of hypersonic vehicles a huge challenge e. Therefore, true reflection the coupling characteristics was great significance. Based on response surface methods, aerodynamic/propulsion coupling model was built in this paper, and small perturbation linear model was also derived. Then, using matrix eigenvalue perturbation theory, propulsion system effects on flight dynamics were analyzed. The results showed that hypersonic flight dynamics was much more sensitive to the propulsion effects, which reflected the strong coupling between propulsion system and flight dynamics.

Original languageEnglish
Title of host publicationProceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
Pages53-57
Number of pages5
DOIs
StatePublished - 2012
Event2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012 - Nanchang, Jiangxi, China
Duration: 26 Aug 201227 Aug 2012

Publication series

NameProceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
Volume1

Conference

Conference2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
Country/TerritoryChina
CityNanchang, Jiangxi
Period26/08/1227/08/12

Keywords

  • Coupling modeling
  • Hypersonic vehicle
  • Integration configuration

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