摘要
为了适应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三轴正交放置的线圈,通过计算机控制三轴线圈驱动电流生成飞行器的外部静态地磁环境,给出了飞行器载体磁干扰补偿模型剩磁和感磁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 requirement of aircraft’s rapid response, according to the magnetic interference mechanism of aircraft carrier, in laboratory conditions a three-axis orthogonal coil is used and the drive current of the three-axis coil is controlled by a computer in order to generate aircraft’s external static magnetic environment. The accurate solution method of residual magnetic coefficients and induced magnetic coefficients of the aircraft carrier’s magnetic interference compensation model are given and verified through simulation experiment.
出处
《武汉理工大学学报（交通科学与工程版）》
2013年第6期1351-1354,共4页
Journal of Wuhan University of Technology（Transportation Science & Engineering）
关键词
三轴线圈
驱动电流
静态地磁环境
剩磁系数
感磁系数
three-axis coil
drive current
static magnetic environment
residual magnetic coefficients
induced magnetic coefficients
