Uncertainty Disturbance Modeling and Effect on Hypersonic Test Vehicle

摘要：

Disturbance error mathematic model of unmanned hypersonic test vehicle (UHTV) is analyzed in the paper. To meet the requirement of UHTV flight integration test, the separation disturbance model, the stochastic wind speed model, and uncertainty model of elastic effect are designed. The aerodynamic uncertainty parameters during engine on and off in level flight are given.

关键词： hypersonic disturbance model wind speed attitude control

作者: Xin Wang Shijie Sun

作者单位: College of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China

会议类型: 国际会议

会议名称: The 22nd China Control and Decision Conference(2010年中国控制与决策会议)

会议地点: 徐州

会议语种:英文

页码: 930-933

在线出版日期: 2010-05-26（万方平台首次上网日期，不代表论文的发表时间）