测控技术2011，Vol.30Issue(6)：8-11,4.
基于GPS与全站仪的惯性导航部件安装校准技术
Research on Installation and Calibration of INS Base on GPS and Total Station
武瑞娟 1何红丽 1惠广裕 1何正玲2
作者信息
- 1. 中航工业中国飞行试验研究院测试所,陕西,西安710089
- 2. 西安文理学院图书馆,陕西,西安710065
- 折叠
摘要
Abstract
The initial installation error of inertial navigation systems(INS) can not eliminate, this error will seriously influence the precision of INS. A technology for calibrating the installation of INS based on the GPS location and total station is researched. The technology calculates the angle of plane' s heading and north direction,compares with the indicated data of plane' s INS, achieves the purpose of calibrating the alignment error. Using this technology are tested, the result of test indicates that the technology can quickly calculate the alignment error of the plane, thus repair the output of INS and improve the navigation precision.关键词
惯性导航系统/安装误差/GPS/全站仪Key words
inertial navigation system/ alignment error/ GPS/ total station分类
航空航天引用本文复制引用
武瑞娟,何红丽,惠广裕,何正玲..基于GPS与全站仪的惯性导航部件安装校准技术[J].测控技术,2011,30(6):8-11,4.
