摘要
介绍了弹丸飞行姿态参数对于制导的重要性,并阐述了惯性导航和地磁导航在弹丸姿态测试中的常用方法,在导航技术发展现状的基础上提出了导航的主要研究方向——组合导航。
This paper introduces the importance of flight attitude parameters on the projectile guiding, and describes the common method of inertial navigation and geomagnetic navigation in attitude testing. Then it proposes the idea of combination navigation, which is the main research directions of navigation based on the current navigation technology development situation.
出处
《山西电子技术》
2013年第5期87-89,共3页
Shanxi Electronic Technology
关键词
惯性导航
地磁导航
姿态测试
组合导航
integrated navigation
geomagnetic navigation
attitude testing
integrated navigation
