摘要
为了满足飞行器的快速反应要求,根据飞行器载体磁干扰的产生机理,在实验室条件下采用磁场产生器生成飞行器的外部动态地磁环境,给出了飞行器载体磁干扰补偿模型涡流磁场系数精确求解的方法,并通过仿真试验进行了验证。
In order to meet the requirements of aircraft＇s rapid response, according to the magnetic interference mechanism of aircraft carrier in laboratory conditions, a magnetic field generator is used to generate aircraft＇s external dynamic magnetic environment. The accurate solution method of eddy magnetic coefficients of the aircraft carrier＇s magnetic interference compensation model are given and verified through simulation experiment.
出处
《船电技术》
2014年第5期30-33,共4页
Marine Electric & Electronic Engineering
关键词
动态地磁环境
两轴同步
涡流磁场系数
dynamic magnetic environment
two axis synchronization
eddy magnetic coefficients
