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

Dong Zhang, Shuo Tang

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

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.

源语言英语
主期刊名Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
53-57
页数5
DOI
出版状态已出版 - 2012
活动2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012 - Nanchang, Jiangxi, 中国
期限: 26 8月 201227 8月 2012

出版系列

姓名Proceedings of the 2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
1

会议

会议2012 4th International Conference on Intelligent Human-Machine Systems and Cybernetics, IHMSC 2012
国家/地区中国
Nanchang, Jiangxi
时期26/08/1227/08/12

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