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
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;
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
DOI :
10.1109/ISSCAA.2008.4776354
