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.
出处
《飞机设计》
2005年第3期75-80,共6页
Aircraft Design
