Control-oriented Modeling for Hypersonic Vehicle Control

摘要：

Hypersonic vehicles have great promising in civil and military application. The physics related to hypersonic flight is quite different from traditional aircraft, such as strong nonlinear, strong aerodynamic coupling and so on. In this work, we apply oblique-shock theory and Prandtl-Meyer flow to obtain a control-orienied model for a hypersonic flight. The results compare well with results of computational fluid dynamics, but can be achieved much quicker, which is preferred for control investigation. As an example, a complete feedback control system for the flight model is demonstrated in the end of this paper.

关键词： hypersonic vehicle control-oriented modeling oblique-shock theory flight control

作者: Wei Qngkai Huang Xun

作者单位: College of Engineering, Peking University, Beijing, China

会议类型: 国际会议

会议名称: 2010 Asia-Pacific International Symposium on Aerospace Technology(2010 亚太航空航天技术研讨会 APISAT 2010)

会议地点: 西安

会议语种:英文

页码: 597-599

在线出版日期: 2010-09-01（万方平台首次上网日期，不代表论文的发表时间）