Presentation 2015-02-19
Application of Fiber Optic Sensors in Space Engineering
Tadahito MIZUTANI, Shinji MITANI,
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Abstract(in English) Structural design verification becomes critical under the situation in which an observation performance of spacecraft is extremely required and, hence, the interdisciplinary investigations are needed to solve technical difficulties in the structural design. In this paper, a conceptual study was summarized for a structural design verification technique using fiber optic sensors especially for thermal strain measurement. A concept of sensor-integrated space structures was included in this study. In addition, a reduction of thermally induced drift of an interferometric fiber optic gyroscope (I-FOG), which is currently under development by JAXA, was discussed as an example of the precise structural design.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) Space Engineering / Design Verification / Thermal Strain / Thermal Deformation / Fiber Optic Sensor / Fiber Optic Gyroscope
Paper # OCS2014-106,OFT2014-63,OPE2014-208
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Conference Information
Committee OCS
Conference Date 2015/2/12(1days)
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Registration To Optical Communication Systems (OCS)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) Application of Fiber Optic Sensors in Space Engineering
Sub Title (in English)
Keyword(1) Space Engineering
Keyword(2) Design Verification
Keyword(3) Thermal Strain
Keyword(4) Thermal Deformation
Keyword(5) Fiber Optic Sensor
Keyword(6) Fiber Optic Gyroscope
1st Author's Name Tadahito MIZUTANI
1st Author's Affiliation Structures and Mechanisms Group, ARD, JAXA()
2nd Author's Name Shinji MITANI
2nd Author's Affiliation Guidance and Control Group, ARD, JAXA
Date 2015-02-19
Paper # OCS2014-106,OFT2014-63,OPE2014-208
Volume (vol) vol.114
Number (no) 451
Page pp.pp.-
#Pages 6
Date of Issue