Research on multi-model of hypersonic vehicle based on bifurcation theory

Erlong Su, Changwan Min, Zhen Xiao, Ming Yang, Ying Wang, Jianjun Luo

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The bifurcation theory was employed to divide the multi-model of hypersonic vehicle. The eigenvalue topologies of nonlinear dynamics of hypersonic vehicle were obtained through applying the continuation method, and the relation between the eigenvalue and dynamics of sub-model was established. Based on the variation of dynamic characteristics, the multi-models were successfully divided. Firstly, the relation between eigenvalue and dynamics of sub-model was established, and the topologies of eigenvalue of longitudinal model (short period mode) was being computed and the relation between eigenvalue and sub-model dynamics was given, after that the three sub-models for longitudinal model were obtained; Correspondingly, for the lateral dynamic model, the topologies of eigenvalue corresponding to Dutch roll mode and roll subsistence mode were computed and the lateral model was divided into 6 sub-models finally. Lastly, the eigenvalue topologies for 5 order coupled model was computed and coupled dynamic model was divided into 4 sub-models. The results above can provide the important information for strategies of control and switch of the sub-models as well as controller design for hypersonic vehicle.

源语言英语
主期刊名21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624104633
出版状态已出版 - 2017
活动21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 - Xiamen, 中国
期限: 6 3月 20179 3月 2017

出版系列

姓名21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017

会议

会议21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
国家/地区中国
Xiamen
时期6/03/179/03/17

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