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一种基于低精度光纤陀螺的组合导航系统

黄雪妮 李泱

兵工自动化2018,Vol.37Issue(1):11-14,4.
兵工自动化2018,Vol.37Issue(1):11-14,4.DOI:10.7690/bgzdh.2018.01.003

一种基于低精度光纤陀螺的组合导航系统

Integrated Navigation System Based on Low Precision Fiber Optic Gyroscope

黄雪妮 1李泱1

作者信息

  • 1. 中国飞行试验研究院,西安 710089
  • 折叠

摘要

Abstract

Aiming at the practical engineering requirement, design the flight test method for integrated navigation system based on low precision fiber optic gyroscope. Establish integrated navigation system based on low precision fiber optic gyroscope, including magnetic sensor, Doppler radar, and satellite navigation subsystem, design Kalman filter. Put forward the status equation and measurement equation, and carry out flight test. The test results show that the integrated navigation system can satisfy medium precision navigation requirements, with low design cost, and the system algorithm is scientific and feasible. The system is practical and can be widely used in civil aviation navigation field.

关键词

光纤陀螺/磁传感器/多普勒雷达/卫星导航/飞行试验

Key words

fiber optic gyroscope/magnetic sensor/Doppler radar/satellite navigation/flight test

分类

军事科技

引用本文复制引用

黄雪妮,李泱..一种基于低精度光纤陀螺的组合导航系统[J].兵工自动化,2018,37(1):11-14,4.

基金项目

国家自然科学基金(61203189, 61374054) (61203189, 61374054)

兵工自动化

OACSTPCD

1006-1576

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