DocumentCode :
3226602
Title :
Modeling and active vibration control of rigid-flexible coupled system on vehicle
Author :
Liang, Qing ; Wu, Xinfeng ; Wang, Yong
Author_Institution :
Dept. of Autom., Univ. of Sci. & Technol. of China, Hefei, China
fYear :
2011
fDate :
22-24 April 2011
Firstpage :
4226
Lastpage :
4229
Abstract :
When the missile is carried by vehicle, vibration caused by the road surface environment can lead to the missile fatigue damage. To investigate the active vibration isolation method of vehicle-mounted flexible missile system, a rigid-flexible coupled model is built. The vehicle and the flexible missile are respectively simplified as a quarter suspension system and a flexible beam fixed on a mass. A robust H, controller is then designed for active vibration control. Simulation results verify that the proposed active vibration isolation method can reduce the vibration level more effectively compared with the passive isolation.
Keywords :
H control; beams (structures); fatigue; flexible structures; robust control; shear modulus; suspensions (mechanical components); vibration control; active vibration control; active vibration isolation method; flexible beam; missile fatigue damage; quarter suspension system; rigid-flexible coupled system; road surface environment; robust H controller; vehicle-mounted flexible missile system; Missiles; Robustness; Suspensions; Vehicles; Vibration control; Vibrations; Zirconium; active vibration isolation; flexible missile; rigid-flexible coupled; vehicle-mounted missile;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electric Technology and Civil Engineering (ICETCE), 2011 International Conference on
Conference_Location :
Lushan
Print_ISBN :
978-1-4577-0289-1
Type :
conf
DOI :
10.1109/ICETCE.2011.5774774
Filename :
5774774
Link To Document :
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