某型飞机导航系统惯导校正方式研究  

Research of Inertial Navigation Correction Modes in a Aircraft Navigation System

作　　者：刘志鹏[1] 郭岩[1] 梁尚军[1] 

机构地区：[1]中国人民解放军驻沈阳飞机工业(集团)有限公司军事代表室,沈阳110034

出　　处：《飞机设计》2005年第3期75-80,共6页Aircraft Design

摘　　要：从校正方式组成及原理入手,详细地介绍了某型飞机导航系统惯导几种校正方式的使用特点及相互交联关系。通过数学模型的建立,对几种校正方式的逻辑关系和转换关系进行了整理。本文的研究,为该型飞机导航系统校正方式控制率的改进研制,提供了相应的理论支持。Theory, operating features and interface relations of three correction modes for the inertial navigation; Short-Range Radio Navigation, Long-Range Radio Navigation and Visual, are presented. The logic and switching relations for these correction modes are established through mathematical modeling. This paper will provide the corresponding theoretical support for domestic development of correction mode control ratio in aircraft navigation systems.

关 键 词：飞机 导航系统 惯导校正方式 工作原理 无线电近距导航 

分 类 号：V249.324[航空宇航科学与技术—飞行器设计]