摘要
简述了磁通门磁强计的工作原理 ,讨论了利用磁通门技术进行飞行体飞行姿态实时测量的磁通门磁强计姿态测试系统的基本原理、探头和电路的设计方法 .制作了三轴磁通门磁强计并进行了基础实验 。
The theory of fluxgate magnetometer is described briefly.The basic principle of real-time attitude testing system using fluxgate magnetometer technique and design methods of fluxgate probe & circuit are discussed.The feasibility of the fly body attitude testing using fluxgate magnetometer is approved after making and testing a three axes fluxgate magnetometer.
出处
《弹道学报》
CSCD
北大核心
2002年第2期79-83,共5页
Journal of Ballistics
