FIELD RELIABILITY OF RING LASERS USED IN STRAPDOWN INERTIAL NAVIGATION SYSTEMS

机译：捷联惯导系统中环形激光的现场可靠性

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There analyzed conditions of field reliability of ring helium-neon lasers used in strapdown inertial navigation systems. There have been investigated electric breakdown of the gas and factors affecting the time delay in discharge ignition. There identified the role of additional electrodes in the process of gas discharge formation. There have been calculated the borders of stable bilateral DC gas discharge in the parameter space of the ring laser and its electric circuit. There has been created software used in the design of the ring lasers.

机译：分析了捷联惯性导航系统中使用的环形氦氖激光器的场可靠性条件。已经研究了气体的电击穿以及影响放电点火时间延迟的因素。确定了附加电极在气体放电形成过程中的作用。已经计算出环形激光器及其电路的参数空间中稳定的双边直流气体放电的边界。已经创建了用于环形激光器设计的软件。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20040524-26; Saint Petersburg(RU)》|2004年|P.271-273|共3页
会议地点 Saint Petersburg(RU)
作者
A.V. Molchanov; D.A. Morozov; I.V. Osetrov; M.V. Chirkin;
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作者单位

Moscow Institute of Electromechanics and Automatics 5 Aviatzionny Pereulok, 125319, Moscow, Russia;

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会议组织
原文格式 PDF
正文语种 eng
中图分类无线电导航;
关键词
laser gyro; ring laser; breakdown; discharge ignition; time delay;

机译：激光陀螺;环形激光器;击穿;放电点火;延时;

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1. Combined Use of Strapdown Inertial Navigation Systems and Odometers from the Standpoint of Mechanics of Inertial Navigation Systems. Part 1 [J] . A. A. Golovan, I.V. Nikitin Moscow University Mechanics Bulletin . 2015,第2期

机译：从惯性导航系统的力学角度出发，结合使用捷联惯性导航系统和里程表。第1部分
2. Combined Use of Strapdown Inertial Navigation Systems and Odometers from the Standpoint of Mechanics of Inertial Navigation Systems. Part 2 [J] . A. A. Golovan, I.V. Nikitin Moscow University Mechanics Bulletin . 2015,第4期

机译：从惯性导航系统的力学角度出发，结合使用捷联惯性导航系统和里程表。第2部分
3. Two-dimensional laser Doppler velocimeter and its integrated navigation with a strapdown inertial navigation system [J] . Wang Qi, Gao Chunfeng, Zhou Jian, Applied optics . 2018,第13期

机译：二维激光多普勒速度计及其带有截头惯性导航系统的集成导航
4. Design and analysis of dual-axis rotating scheme for ring laser strapdown inertial navigation system [C] . Chong Qin, Jiabin Chen, Yongqiang Han, Chinese Control Conference . 2016

机译：环形激光捷联惯性导航系统双轴旋转方案设计与分析
5. Real time global positioning system aided strapdown inertial navigation unit system for unmanned aerial vehicle motion sensing [D] . Chot Hun, Lim. 2014

机译：实时全球定位系统辅助的捷联惯性导航单元系统，用于无人机运动传感
6. Field Programmable Gate Array Based Parallel Strapdown Algorithm Design for Strapdown Inertial Navigation Systems [O] . Zong-Tao Li, Tie-Jun Wu, Can-Long Lin, 2011

机译：捷联惯导系统基于现场可编程门阵列的并联捷联算法设计
7. Field Programmable Gate Array Based Parallel Strapdown Algorithm Design for Strapdown Inertial Navigation Systems [O] . Li, Zong-Tao, Wu, Tie-Jun, Lin, Can-Long, 2011

机译：捷联惯性导航系统基于现场可编程门阵列的并联捷联算法设计
8. Flight Test Results of the Strapdown Ring Laser Gyro Tetrad Inertial Navigation System [R] . Carestia, R. A., Hruby, R. J., Bjorkman, W. S. 1983

机译：捷联环形激光陀螺四分体惯性导航系统的飞行试验结果

FIELD RELIABILITY OF RING LASERS USED IN STRAPDOWN INERTIAL NAVIGATION SYSTEMS

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