DocumentCode :
3153779
Title :
Research on Control Method for Lateral Thrust Based on Interceptor in Aerosphere
Author :
Yin, Yongxin ; Yang, Ming ; Wang, Zicai
Author_Institution :
Control & Simulation Center Harbin
Volume :
1
fYear :
2006
fDate :
4-6 Oct. 2006
Firstpage :
713
Lastpage :
716
Abstract :
A method to control the lateral thrust is presented for combined control interceptor in aerosphere. The control command of the interceptor is divided into two commands: command of aerodynamic force and command of lateral thrust. A lateral thrust subsystem is constituted, lateral thrust from the pulse motor is presented, and detailed method to control the lateral thrust is designed. This method is useful to control the interceptor and is convenient for practical project. The simulation results show that this method tracks control command efficiently and accurately, economizes the quantity of pulse motors, and has satisfactory control precision, which shows the availability and advantage
Keywords :
aerodynamics; aerospace control; stepping motors; aerodynamic force; aerosphere; control interceptor; lateral thrust; pulse motor; switch control; Aerodynamics; Computational modeling; Control systems; Delay; Design methodology; Force control; Switches; Systems engineering and theory; Target tracking; Weight control; combined control; hybrid system; switch control; track command;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Engineering in Systems Applications, IMACS Multiconference on
Conference_Location :
Beijing
Print_ISBN :
7-302-13922-9
Electronic_ISBN :
7-900718-14-1
Type :
conf
DOI :
10.1109/CESA.2006.4281745
Filename :
4281745
Link To Document :
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