DocumentCode
1871670
Title
Research on the method for attitude fuzzy control of the interceptor
Author
Yin, Yongxin ; Yang, Ming ; Wang, Zicai
Author_Institution
Harbin Inst. of Technol., Heilongjiang
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
308
Abstract
A new method for attitude fuzzy control has been presented for the interceptor by combined control of lateral thrust and aerodynamic force, and the torque received by interceptor has been analyzed, and the influences of jet have been described, models of the attitude motion have been constructed, and the new method for attitude fuzzy control has been presented, which is simple and is convenient for practical project. The simulation results show that this method can fleetly and effectual come true attitude control of the interceptor, and shows that these models have higher control precision, and shows the advantage of the method
Keywords
aerodynamics; attitude control; fuzzy control; jets; aerodynamic force; attitude fuzzy control; attitude motion; interceptor; jet; lateral thrust; Aerodynamics; Attitude control; Educational technology; Force control; Fuzzy control; Helium; Intelligent control; Motion analysis; Motion control; Torque control;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627632
Filename
1627632
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