Design and Application of Allfiber Velocity Interferometer

Qixian, 彭其先 Peng; Jianhua, 蒙建华 Meng; Detian, 王德田 Wang; Jun, 刘俊 Liu; Zeren, 李泽仁 Li

doi:10.3788/gzxb20103911.2008

光子学报

2010

DOI: 10.3788/gzxb20103911.2008

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Design and Application of Allfiber Velocity Interferometer

彭其先 Peng Qixian¹,

蒙建华 Meng Jianhua²,

王德田 Wang Detian³

et al.

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Research on Spacecraft Strain Measurement System and Impact Sensing Technology Based on Fiber Grating Sensors and All Fiber Optic Sensing

Luo¹,

Zhang²,

Zhang³

et al. 2021

J. Phys.: Conf. Ser.

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In the process of flight for in-orbit spacecraft, debris and particles in space will collide with the spacecraft at a high speed. These collision will produce strain, pit or perforation on the surface of the spacecraft cabin, forming damage accumulation. Therefore, it is necessary to monitor the strain and impact position of the spacecraft cabin in real time, which will provide a basis for ensuring the reliability and safety of the spacecraft. In this paper, the achievement of strain and vibration information during the process of impact is designed in two ways: touched style and untouched style. The design of touched style needs to meet the requirements of large capacity/ultra-high speed monitoring. The design of untouched style needs to meet the acquisition of high frequency vibration signal in the impact process.

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Research on Spacecraft Strain Measurement System and Impact Sensing Technology Based on Fiber Grating Sensors and All Fiber Optic Sensing

Luo¹,

Zhang²,

Zhang³

et al. 2021

J. Phys.: Conf. Ser.

View full text Add to dashboard Cite

show abstract

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Design and Application of Allfiber Velocity Interferometer

Cited by 1 publication

References 0 publications

Research on Spacecraft Strain Measurement System and Impact Sensing Technology Based on Fiber Grating Sensors and All Fiber Optic Sensing

Research on Spacecraft Strain Measurement System and Impact Sensing Technology Based on Fiber Grating Sensors and All Fiber Optic Sensing

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