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
Link To Document :
بازگشت