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Paper Abstract and Keywords
Presentation 2008-06-27 17:50
High Precision Fiber Optic Gyro IRU for Spacecraft Systems
Shinji Mitani, Yoshiyuki Ishijima, Takanori Iwata, Hideto Suzuki, Shin-ichiro Sakai, Tomoaki Toda, Tatsuaki Hashimoto, Hirobumi Saito (JAXA), Aritaka Ohno, Yasuaki Miyahara, Haruhiko Okikura (JAE) SANE2008-40
Abstract (in Japanese) (See Japanese page) 
(in English) For future advanced Earth observation or astronomy missions, an inertial reference unit (IRU) having high accuracy, a wide dynamic range, a long useful lifetime, and high reliability is required. The fiber optic gyro (FOG) is a strong candidate to fulfill those requirements: it has already been applied widely to satellites. We have been developing a high-performance FOG inertial reference unit (FOG-IRU) for use in future satellites. This paper describes the architecture and design results of the FOG-IRU. In addition, it presents a summary of performance test results and analyses of gyros’ critical items: angle random walk, scale factor, and bias repeatability.
Keyword (in Japanese) (See Japanese page) 
(in English) Interferometer Fiber Optic Gyroscope / IFOG / Satellite / Attitude Control / / / /  
Reference Info. IEICE Tech. Rep., vol. 108, no. 100, SANE2008-40, pp. 149-154, June 2008.
Paper # SANE2008-40 
Date of Issue 2008-06-19 (SANE) 
ISSN Print edition: ISSN 0913-5685    Online edition: ISSN 2432-6380
Copyright
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All rights are reserved and no part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, recording, or any information storage and retrieval system, without permission in writing from the publisher. Notwithstanding, instructors are permitted to photocopy isolated articles for noncommercial classroom use without fee. (License No.: 10GA0019/12GB0052/13GB0056/17GB0034/18GB0034)
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Conference Information
Committee SANE  
Conference Date 2008-06-26 - 2008-06-27 
Place (in Japanese) (See Japanese page) 
Place (in English) Tsukuba Space Center (JAXA) 
Topics (in Japanese) (See Japanese page) 
Topics (in English) Space applications symposium 
Paper Information
Registration To SANE 
Conference Code 2008-06-SANE 
Language Japanese 
Title (in Japanese) (See Japanese page) 
Sub Title (in Japanese) (See Japanese page) 
Title (in English) High Precision Fiber Optic Gyro IRU for Spacecraft Systems 
Sub Title (in English)  
Keyword(1) Interferometer Fiber Optic Gyroscope  
Keyword(2) IFOG  
Keyword(3) Satellite  
Keyword(4) Attitude Control  
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1st Author's Name Shinji Mitani  
1st Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
2nd Author's Name Yoshiyuki Ishijima  
2nd Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
3rd Author's Name Takanori Iwata  
3rd Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
4th Author's Name Hideto Suzuki  
4th Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
5th Author's Name Shin-ichiro Sakai  
5th Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
6th Author's Name Tomoaki Toda  
6th Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
7th Author's Name Tatsuaki Hashimoto  
7th Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
8th Author's Name Hirobumi Saito  
8th Author's Affiliation Japan Aerospace Exploration Agency (JAXA)
9th Author's Name Aritaka Ohno  
9th Author's Affiliation Japan Aviation Electronics Industry, Limited (JAE)
10th Author's Name Yasuaki Miyahara  
10th Author's Affiliation Japan Aviation Electronics Industry, Limited (JAE)
11th Author's Name Haruhiko Okikura  
11th Author's Affiliation Japan Aviation Electronics Industry, Limited (JAE)
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Speaker Author-1 
Date Time 2008-06-27 17:50:00 
Presentation Time 25 minutes 
Registration for SANE 
Paper # SANE2008-40 
Volume (vol) vol.108 
Number (no) no.100 
Page pp.149-154 
#Pages
Date of Issue 2008-06-19 (SANE) 


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