光纤陀螺在M-V火箭惯导系统中的应用

2002 15th Optical Fiber Sensors Conference Technical Digest. OFS 2002(Cat. No.02EX533) Pub Date : 2002-05-10 DOI:10.1109/OFS.2002.1000491

J. Nasu, K. Saito, A. Kurokawa, F. Hayashi, I. Nakatani

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引用次数: 5

摘要

采用光纤陀螺(FOGs)的惯性导航和制导系统(ING)是为ISAS(空间航天科学研究所)M-V火箭开发的。M-V-1火箭在1997年2月成功发射。一系列M-V火箭发射了三次，fogg - ings在所有飞行中都表现良好。本文结合M-V-1火箭的ING飞行数据，提出了突破点。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Application of fiber gyros at MPC - Inertial Navigation and Guidance system for M-V rocket

The Inertial Navigation and Guidance system (ING) with fiber gyros (FOGs) was developed for the ISAS (Institute of Space and Astronautical Science) M-V rocket. The M-V-1 rocket was successfully launched in February 1997. A series of M-V rockets was launched three times and FOG-INGs worked well in all flights. This paper presents the breakthrough points with the flight data of M-V-1 rocket's ING.

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2002 15th Optical Fiber Sensors Conference Technical Digest. OFS 2002(Cat. No.02EX533)

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