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
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;
Conference_Titel :
Innovative Computing, Information and Control, 2007. ICICIC '07. Second International Conference on
Conference_Location :
Kumamoto
Print_ISBN :
0-7695-2882-1
DOI :
10.1109/ICICIC.2007.486
