Active control of beam vibration excited by moving rigid body

Haibin Li; Shihua Bi; Yuanqiao Fang; Zengfeng Yuan

Active control of beam vibration excited by moving rigid body

Haibin Li^*, Shihua Bi, Yuanqiao Fang, Zengfeng Yuan

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

Research output: Contribution to journal › Article › peer-review

1 Citation (Scopus)

Abstract

From the simplified model of rocket and/or missile launcher, the beam vibration excited by the moving rigid body was analyzed. The optimal inputs were given on the basis of the optimal control theory. The simulation test showed that the input suppressed the vibration of the beam and the initial disturbance of the rocket.

Original language	English
Pages (from-to)	610-615
Number of pages	6
Journal	Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
Volume	17
Issue number	5
Publication status	Published - 1997

Keywords

Active control
Beam
Launcher
Vibration analysis
Vibration control

Cite this

Li, H., Bi, S., Fang, Y., & Yuan, Z. (1997). Active control of beam vibration excited by moving rigid body. Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 17(5), 610-615.

@article{be3ab9d54d3641fc954ac7211bcf1e83,

title = "Active control of beam vibration excited by moving rigid body",

abstract = "From the simplified model of rocket and/or missile launcher, the beam vibration excited by the moving rigid body was analyzed. The optimal inputs were given on the basis of the optimal control theory. The simulation test showed that the input suppressed the vibration of the beam and the initial disturbance of the rocket.",

keywords = "Active control, Beam, Launcher, Vibration analysis, Vibration control",

author = "Haibin Li and Shihua Bi and Yuanqiao Fang and Zengfeng Yuan",

year = "1997",

language = "English",

volume = "17",

pages = "610--615",

journal = "Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology",

issn = "1001-0645",

publisher = "Beijing Institute of Technology",

number = "5",

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TY - JOUR

T1 - Active control of beam vibration excited by moving rigid body

AU - Li, Haibin

AU - Bi, Shihua

AU - Fang, Yuanqiao

AU - Yuan, Zengfeng

PY - 1997

Y1 - 1997

N2 - From the simplified model of rocket and/or missile launcher, the beam vibration excited by the moving rigid body was analyzed. The optimal inputs were given on the basis of the optimal control theory. The simulation test showed that the input suppressed the vibration of the beam and the initial disturbance of the rocket.

AB - From the simplified model of rocket and/or missile launcher, the beam vibration excited by the moving rigid body was analyzed. The optimal inputs were given on the basis of the optimal control theory. The simulation test showed that the input suppressed the vibration of the beam and the initial disturbance of the rocket.

KW - Active control

KW - Beam

KW - Launcher

KW - Vibration analysis

KW - Vibration control

UR - http://www.scopus.com/inward/record.url?scp=0004470322&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:0004470322

SN - 1001-0645

VL - 17

SP - 610

EP - 615

JO - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology

JF - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology

IS - 5

ER -

Active control of beam vibration excited by moving rigid body

Abstract

Keywords

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