Signal processing for fiber optic gyroscope (FOG_

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

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Citations (Scopus)

Abstract

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.

Original languageEnglish
Title of host publicationProceedings of SPIE - The International Society for Optical Engineering
EditorsRamon P. DePaula
PublisherSociety of Photo-Optical Instrumentation Engineers
Pages192-202
Number of pages11
ISBN (Print)0819416169
Publication statusPublished - 1994
Externally publishedYes
EventFiber Optic and Laser Sensors XII - San Diego, CA, USA
Duration: 1994 Jul 251994 Jul 27

Publication series

NameProceedings of SPIE - The International Society for Optical Engineering
Volume2292
ISSN (Print)0277-786X

Conference

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

ASJC Scopus subject areas

  • Electronic, Optical and Magnetic Materials
  • Condensed Matter Physics
  • Computer Science Applications
  • Applied Mathematics
  • Electrical and Electronic Engineering

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