| 仿真试验条件下飞行器外部静态磁环境模拟 |
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| 引用本文： | 还迎春,林春生,余杰.仿真试验条件下飞行器外部静态磁环境模拟[J].武汉水运工程学院学报,2013(6):1351-1354. |
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| 作者姓名： | 还迎春 林春生 余杰 |
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| 作者单位： | 海军工程大学兵器工程系,武汉430033 |
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| 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。
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| 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 |
Simulation of aircraft external static magnetic environment in the laboratory |
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| Authors: | HUAN Yingchun LIN Chunsheng YU Jie |
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| Institution: | (Department of Weapon Engineering, Naval University of Engineering, Wuhan 430033, China) |
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| Abstract: | 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. |
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| Keywords: | three-axis coil drive current static magnetic environment residual magnetic coefficients induced magnetic coefficients |
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