HEMISPHERICAL RESONANCE GYRO-BASED STRAPDOWN INERTIAL NAVIGATION SYSTEM

机译：基于半球共振陀螺的捷联惯导系统

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The results of the development of a mock-up of a strapdown inertial navigation system based on a hemispherical resonance gyro (HRG)and pendulous silicon accelerometers have been presented. The system block-diagram has been described. Particular emphasis has been placed on the description of the mathematical model used for the HRG calibration, as well as on the problems of calibration. The HRG characteristics before and after calibration have been described. The results of testing the system located on a fixed base, as well as when selecting angular motion of the turn table, have been given. The projected measures to improve the HRG-based SINS accuracy have been presented.

机译：提出了基于半球共振陀螺仪（HRG）和摆式硅加速度计的捷联惯性导航系统模型的开发结果。已经描述了系统框图。特别强调了用于HRG校准的数学模型的描述以及校准问题。已经描述了校准前后的HRG特性。给出了在固定底座上测试系统的结果，以及选择转台的角度运动时的结果。提出了改善基于HRG的SINS精度的计划措施。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20070528-30; Saint Petersburg(RU)》|2007年|P.116-124|共9页
会议地点 Saint Petersburg(RU)
作者
G.I. Djandzhgava; K.A. Bakhonin; G.M. Vinogradov; A.V.Trebukhov;
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作者单位

JSC Ramenskoye Design Company 2, Guryeva St., Ramenskoye, Moscow region;

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会议组织
原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
strapdown; inertial system; hemispherical resonance gyro (HRG)pendulous; accelerometer;

机译：捷联;惯性系统;半球共振陀螺（HRG）摆;加速度计;

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专利

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. Strapdown inertial navigation systems readings correction based on navigational data of other sensors and systems with intelligent selection of the priority adjuster [J] . P.M. Trefilov, M.V. Mamchenko, A.V. Korol’kov E3S Web of Conferences . 2020,第10期

机译：挂机惯性导航系统基于其他传感器和系统的导航数据读取校正，具有优先级调整的智能选择
4. HEMISPHERICAL RESONANCE GYRO-BASED STRAPDOWN INERTIAL NAVIGATION SYSTEM [C] . G. I. Djandzhgava, K. A. Bakhonin, G. M. Vinogradov, Saint Petersburg International Conference on Integrated Navigation Systems . 2007

机译：基于半球形的谐振陀螺仪惯性导航系统
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. Strapdown Inertial Navigation Systems: An Algorithm for Attitude and Navigation Computations [R] . Miller, R. B. 1980

机译：捷联惯导系统：一种姿态导航计算算法

HEMISPHERICAL RESONANCE GYRO-BASED STRAPDOWN INERTIAL NAVIGATION SYSTEM

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