Space grade fiber optic gyroscope: R&D results and flight tests

被引：0

作者：

Korkishko, Yu. N. ^{[1
]}

Fedorov, V. A. ^{[1
]}

Prilutskiy, V. E. ^{[1
]}

Ponomarev, V. G. ^{[1
]}

Morev, I. V. ^{[1
]}

Morev, A. I. ^{[1
]}

Obuhovich, D. V. ^{[1
]}

Kostritskii, S. M. ^{[1
]}

Zuev, A. I. ^{[1
]}

Varnakov, V. K. ^{[1
]}

Belashenko, A. V. ^{[1
]}

Yakimov, E. N. ^{[2
]}

Titov, G. V. ^{[2
]}

Ovchinnikov, A. V. ^{[2
]}

Abdul'minov, I. B. ^{[2
]}

Latyntsev, S. V. ^{[2
]}

机构：

[1] LLC RPC Optolink, Sosnovaya Alley,Bldg 6a,Premises 5, Moscow 124489, Zelenograd, Russia

[2] Academician MF Reshetnev Informat Satellite Syst, Lenin St, Zheleznogorsk 662972, Krasnoyarsk Reg, Russia

来源：

2016 DGON INERTIAL SENSORS AND SYSTEMS (ISS) | 2016年

关键词：

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

The aims of the current work are R&D and flight tests of fiber-optic gyro for space applications VOBIS. Space-grade FOGs VOBIS are developed for the tasks of spacecraft orientation and navigation at the high orbit and are long-life radiation resistant. Its' estimated operation time is 15 years in high vacuum and radiation environment.

引用

页数：19

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