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
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