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