DocumentCode :
2195869
Title :
Pole placement controller design for relaxed stable stability missile
Author :
Zhengyu, Guo ; Xiaogeng, Liang
Author_Institution :
Luoyang Opto-Electro Technol. Dev. Center, Luoyang, China
fYear :
2011
fDate :
9-11 Sept. 2011
Firstpage :
1577
Lastpage :
1580
Abstract :
Relaxed Stable Stability is a new way to rise the flying speed, distance and maneuverability of missile. The focus of this paper is on the pole placement controller design for RSS missile. First, a concise introduction of RSS and pole placement controller and the vertical direction perturbation equations are described. Then a controller is developed. By using this, we simulate a missile model. Simulation results as well as stability analysis of RSS missile demonstrate the validity of the proposed scheme.
Keywords :
control system synthesis; missile control; perturbation techniques; pole assignment; stability; RSS missile; flying speed; missile distance; missile maneuverability; missile model; perturbation equation; pole placement controller design; relaxed stable stability missile; Aerodynamics; Mathematical model; Missiles; Simulation; Stability analysis; State feedback; Controller Design; Pole Placement Controller; Relaxed Stable Stability Missile;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronics, Communications and Control (ICECC), 2011 International Conference on
Conference_Location :
Ningbo
Print_ISBN :
978-1-4577-0320-1
Type :
conf
DOI :
10.1109/ICECC.2011.6067734
Filename :
6067734
Link To Document :
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