DocumentCode
2733408
Title
Research on Spin Rocket Double-channel Proportional Control Characteristics
Author
Mo, Bo ; Gao, En-yu ; Yang, Shu-xing
Author_Institution
Beijing Inst. of Technol., Beijing
fYear
2007
fDate
5-7 Sept. 2007
Firstpage
12
Lastpage
12
Abstract
This paper mainly focuses on double-channel proportional control characteristic of the endoatmospheric spin rocket. The divided command model is built under spin condition and the control process is simulated in mathematic method. In the end, it is conclusion of spin rocket proportional control characteristic.
Keywords
aerospace control; proportional control; rockets; endoatmospheric spin rocket; mathematic method; spin rocket double-channel proportional control; Aerospace control; Control systems; Force control; Mathematical model; Mathematics; Missiles; Process control; Proportional control; Rockets; Transfer functions;
fLanguage
English
Publisher
ieee
Conference_Titel
Innovative Computing, Information and Control, 2007. ICICIC '07. Second International Conference on
Conference_Location
Kumamoto
Print_ISBN
0-7695-2882-1
Type
conf
DOI
10.1109/ICICIC.2007.486
Filename
4427659
Link To Document