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