舰船电子工程2016,Vol.36Issue(10):43-47,5.DOI:10.3969/j.issn.1672-9730.2016.10.012
基于速度匹配的舰载导弹 SINS 原位标定方法研究
Research for In-situ Calibration Method of Ship-launched Missile Strapdown Inertial Navigation System Based on Velocity Matching
庞晓楠 1王磊 2李向阳2
作者信息
- 1. 海军潜艇学院 青岛 266000
- 2. 海军航空工程学院指挥系 烟台 264001
- 折叠
摘要
Abstract
An all types of missile launcher shared and velocity matching based shipboard missile based in‐situ calibration technology is proposed .The SINS parameter error influence on the navigation accuracy is discussed ,and the calibration scheme and procedure are designed .The simulation results show the feasibility and effectiveness of the proposed approach .关键词
舰载导弹/速度匹配/SINS/原位标定方法Key words
ship-launched missile/velocity matching/SINS/In-situ calibration分类
信息技术与安全科学引用本文复制引用
庞晓楠,王磊,李向阳..基于速度匹配的舰载导弹 SINS 原位标定方法研究[J].舰船电子工程,2016,36(10):43-47,5.