DocumentCode
2639101
Title
Attitude control of unmanned hypersonic test vehicle
Author
Wang, Xin ; Feng, Dongzhu ; Lin, Yi
Author_Institution
Coll. of Astronaut., Northwestern Polytech. Univ. of China, Xi´´an
fYear
2008
fDate
10-12 Dec. 2008
Firstpage
1
Lastpage
5
Abstract
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.
Keywords
aircraft control; attitude control; control system synthesis; linear systems; remotely operated vehicles; robust control; CFD data; attitude control system; linear control; mixed method; robust controller; simulation; supersonic combustion ramjet test; unmanned hypersonic test vehicle; Attitude control; Combustion; Computational fluid dynamics; Robust control; Robustness; System testing; Vehicles; attitude control; hypersonic test flight; nonlinear; robust sensitivity;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
Conference_Location
Shenzhen
Print_ISBN
978-1-4244-3908-9
Electronic_ISBN
978-1-4244-2386-6
Type
conf
DOI
10.1109/ISSCAA.2008.4776354
Filename
4776354
Link To Document