Signal processing for fiber optic gyroscope (FOG_

Ryuichi Tanaka, Akihiro Kurokawa, Yoshiyuki Sato, Tsutomu Magome, Yoshiaki Hayakawa, Ichiro Nakatani, Junichiro Kawaguchi

研究成果: Conference contribution

3 被引用数 (Scopus)

抄録

A fiber-optic gyroscope (FOG) is expected to be the next generation gyroscope for guidance and control, because of various advantages. We have been developing the FOG-Inertial Navigation and Guidance (ING) for M-V satellite launching rocket of the Institute of Space and Astronautical Science (ISAS) since 1990. The FOG-ING consists of an Inertial Measurement Unit (IMU) and an Central Processing Unit Assembly. At current status, the proto-flight model FOG-IMU is being actively developed. And the flight test of the FOG-ING was performed on February 20, 1993, aboard M-3SII-7 satellite launching rocket at the ISAS test facilities in Uchinoura, Japan. This paper presents the signal processing technologies of our FOG which are used for the above FOG-ING.

本文言語English
ホスト出版物のタイトルProceedings of SPIE - The International Society for Optical Engineering
編集者Ramon P. DePaula
出版社Society of Photo-Optical Instrumentation Engineers
ページ192-202
ページ数11
ISBN(印刷版)0819416169
出版ステータスPublished - 1994
外部発表はい
イベントFiber Optic and Laser Sensors XII - San Diego, CA, USA
継続期間: 1994 7 251994 7 27

出版物シリーズ

名前Proceedings of SPIE - The International Society for Optical Engineering
2292
ISSN(印刷版)0277-786X

Conference

ConferenceFiber Optic and Laser Sensors XII
CitySan Diego, CA, USA
Period94/7/2594/7/27

ASJC Scopus subject areas

  • 電子材料、光学材料、および磁性材料
  • 凝縮系物理学
  • コンピュータ サイエンスの応用
  • 応用数学
  • 電子工学および電気工学

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