DocumentCode :
3206316
Title :
Two-Degree Controller Design for Flexible Missile Based on H-inf Interference Suppression
Author :
Zhuo Zhang ; Shunli Li
Author_Institution :
Dept. of Astronaut. Eng., Harbin Inst. of Technol. Harbin, Harbin, China
fYear :
2012
fDate :
8-10 Dec. 2012
Firstpage :
1653
Lastpage :
1656
Abstract :
A flexible missile is researched in this paper. A model of flexible missile containing rigid motion and undesired vibration signal is derived in the pitch channel. The pitch-angle and pitch-rate form the inputs of the controller. The vibration signals are regarded as the interference signals. The problem of interference suppression is regarded as the problem of standard H-inf control, and then we design a two-degree controller. Simulation results show that the two-degree controller can restrain the vibration signals and measurement noise well.
Keywords :
H control; control system synthesis; interference suppression; missile control; H-inf interference suppression; flexible missile; interference signals; measurement noise; pitch-angle form; pitch-rate form; standard H-inf control; two-degree controller design; vibration signals; Equations; Interference suppression; Mathematical model; Missiles; Standards; Vibrations; H-inf control; flexible missile; interference suppression; two-degree controller; vibration signals;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4673-5034-1
Type :
conf
DOI :
10.1109/IMCCC.2012.384
Filename :
6429221
Link To Document :
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