@inproceedings{3be9d3f3046944aa87c0f95eb0a57cce,
title = "Signal processing for fiber optic gyroscope (FOG_",
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.",
author = "Ryuichi Tanaka and Akihiro Kurokawa and Yoshiyuki Sato and Tsutomu Magome and Yoshiaki Hayakawa and Ichiro Nakatani and Junichiro Kawaguchi",
year = "1994",
language = "English",
isbn = "0819416169",
series = "Proceedings of SPIE - The International Society for Optical Engineering",
publisher = "SPIE",
pages = "192--202",
editor = "DePaula, {Ramon P.}",
booktitle = "Proceedings of SPIE - The International Society for Optical Engineering",
address = "United States",
note = "Fiber Optic and Laser Sensors XII ; Conference date: 25-07-1994 Through 27-07-1994",
}