USE OF PRECISION QUARTZ MEASURING INSTRUMENTS APPARENT ACCELERATION IN MODERN INERTIAL NAVIGATION CONTROL SYSTEMS

机译：在现代惯性导航控制系统中使用精密石英测量仪显像加速度

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This report touches upon the problem of use of quartz precision apparent acceleration instruments in modern inertial navigation control systems and the problems of providing temperature independence of both accelerometer units and separate primary measuring components.

机译：该报告涉及在现代惯性导航控制系统中使用石英精密视在加速度仪器的问题，以及提供加速度计单元和单独的主要测量组件都与温度无关的问题。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20040524-26; Saint Petersburg(RU)》|2004年|P.280-284|共5页
会议地点 Saint Petersburg(RU)
作者
L.J. Kalihman; D.M. Kalihman; N.A. Kaldimov; A.V. Polushkin; S.F. Nahov;
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作者单位

FGUP ON 'Korpus', 1 Osipov street, 410019, Saratov, 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
control systems; apparent acceleration instrument; temperature error compensation;

机译：控制系统;表观加速度仪;温度误差补偿;

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专利

1. USE OF A DEVICE FOR MEASURING ABSOLUTE ACCELERATION IN INERTIAL NAVIGATION SYSTEMS [J] . A. S. Devyatisilnyi Measurement techniques . 2003,第7期

机译：在惯性导航系统中测量绝对加速度的设备的使用
2. Absolute acceleration measurers usage in the inertial navigation systems [J] . S. Devyatisilny Измерительная техниκа . 2003,第7期

机译：惯性导航系统中绝对加速度测量仪的使用
3. Absolute acceleration measurers usage in the inertial navigation systems [J] . S. Devyatisilny Измерительная техниκа . 2003,第7期

机译：绝对加速度测量仪在惯性导航系统中使用
4. Six-Axis Unit of Apparent Acceleration Meters Based on a Precision Quartz Pendulum Accelerometer with Digital Feedback for Control Systems of Soyuz-MS and Progress-MS Spacecrafts [C] . V. I. Grebennikov, D.M. Kalikhman, L.Ya. Kalikhman, Saint Petersburg International Conference on Integrated Navigation Systems . 2019

机译：基于带有数字反馈的精密石英摆加速度计的六轴视在加速度计，用于联盟号-MS和Progress-MS航天器的控制系统
5. High precision navigation integrating satellite information -GPS- and inertial system data [D] . Cunha, Telmo Reis. 2002

机译：集成卫星信息-GPS和惯性系统数据的高精度导航
6. Economical High–Low Temperature and Heading Rotation Test Method for the Evaluation and Optimization of the Temperature Control System for High-Precision Platform Inertial Navigation Systems [O] . Qiang Yang, Rong Zhang, Haixia Li 2018

机译：高精度平台惯性导航系统温度控制系统评估与优化的经济高低温航向旋转测试方法
7. Economical High–Low Temperature and Heading Rotation Test Method for the Evaluation and Optimization of the Temperature Control System for High-Precision Platform Inertial Navigation Systems [O] . Qiang Yang, Rong Zhang, Haixia Li 2018

机译：高精度平台惯性导航系统温度控制系统评估和优化的经济高低温和旋转试验方法
8. Dynamics of a System of Control Which Includes Inertial Coordinate Measuring Instruments - USSR -. [R] . Bodner, V. A., Kozlov, M. S. 1960

机译：包含惯性坐标测量仪器的控制系统动力学 - 苏联 - 。

USE OF PRECISION QUARTZ MEASURING INSTRUMENTS APPARENT ACCELERATION IN MODERN INERTIAL NAVIGATION CONTROL SYSTEMS

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