Attitude Control of Unmanned Hypersonic Test Vehicle

摘要：

An attitude control system for the unmanned hypersonic test vehicle is presented. The key issues of hypersonic vehicle attitude establishment and linear control concept relating to Supersonic Combustion Ramjet test are considered. Robust controller is designed using mixed sensitivity method. The robustness is evaluated by use of CFD data and simulation results developed to date are presented.

关键词： hypersonic test flight attitude control nonlinear robust sensitivity

作者: Xin Wang Dongzhu Feng Yi Lin

作者单位: College of Astronautics,Northwestern Polytechnical University of China,Xian 710072 School of electronic engineering,Xidian University of China,Xian 710071

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 1202-1206

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）