ACTIVE CONTROL OF A CANTILEVER BEAM USING A POINTWISE FIBER BRAGG GRATING DISPLACEMENT SENSOR SYSTEM

来源 :The Third International Conference on Dynamics,Vibration and | 被引量 : 0次 | 上传用户:magicMan555
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
  We demonstrate an all-fiber displacement measurement system as well as a gluing concept for setting up fiber Bragg grating (FBG) sensor with high sensitivity.To show the dynamic measurement ability of the proposed system, active control of a smart cantilever beam with a surface-bonded piezoelectric actuator and the proposed pointwise-bonded FBG displacement sensor is investigated.The FBG filter-based demodulation technique is employed in our system.A non-contact laser Doppler vibrometer (LDV) is employed to compare the transient measurement and control results measured by the FBG sensors to demonstrate the performances of the proposed FBG system.
其他文献
High-power solid-state laser facilities have been developed for research in inertial confinement fusion(ICF) in the last few decades[1,2].In order to satisfy the engineering system requirements for op
The static stiffness of rubber isolator was obtained by static compression testing, and a new dynamic stiffness model with considering of rubber visco-hyperelastic was proposed with dynamic excitation
Synchrotron radiation has developed into an invaluable scientific tool for scientists [1].At synchrotron radiation facilities vibration is often a problem causing poor quality of photon beams since be
A fluid partly occupying a moving tank undergoes sloshing.These motions generate severe hydrodynamic loads that might be dangerous for structural integrity and stability of rockets, satellites, ships
In the future, with the development of space and robot technology, space robot manipulators will become more important in various space missions, for instance, constructing space station or repairing
based on the fact subject to physical constraints, space robots carried by the motor can not be done infinitely large, and also hopes to make motor may be small, so the driver output torque is limited
It is well-known that nonlinearities, no matter structural or aerodynamic, may exhibit a variety of responses that are typically associated with nonlinear regimes of response including Limit Cycle Osc
The optimal control of linear system led to a fruitful agreement on theoretical analysis and practical applications[1,2,3], and it achieved a breakthrough in the aeronautics and astronautics fields, s
Actuators are common control mechanisms in most aircrafts.This paper studies the vibration and flutter(a common kind of self-oscillation) characteristics of an actuator-redder system which has structu
会议
A satellite suffers complex vibration loads from the rocket in the launching process.Reduction of the launch-induced dynamical loads of the spacecraft would greatly reduce the risk that the spacecraft