| 弹载双路磁传感器测角原理及实现方案 |
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| 引用本文： | 刘欣,李世中,薛谈顺,王军,黄小兵. 弹载双路磁传感器测角原理及实现方案[J]. 弹箭与制导学报, 2009, 29(4) |
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| 作者姓名： | 刘欣 李世中 薛谈顺 王军 黄小兵 |
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| 作者单位： | 1. 中北大学机电工程学院,太原,030051
2. 山西北方惠丰机电有限公司,山西长治,046012 |
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| 摘 要： | 基于磁通门传感器,文中提出了一种利用双路磁通门传感器,并根据零交叉时传感器输出的相位信息确定方位的原理和方法.同时借助一个二自由度实验转台模拟弹体在地磁场中的运动,利用磁传感器进行地磁测量从而确定弹体的飞行姿态.
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| 关 键 词： | 方位角 零交叉 磁通门传感器 弹体 |
Ball is Loaded with Pair of Road Magnetism Sensors Measure Angle Principle and Realize A Scheme |
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| LIU Xin,LI Shizhong,XUE Tanshun,WANG Jun,HUANG Xiaobing. Ball is Loaded with Pair of Road Magnetism Sensors Measure Angle Principle and Realize A Scheme[J]. Journal of Projectiles Rockets Missiles and Guidance, 2009, 29(4) |
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| Authors: | LIU Xin LI Shizhong XUE Tanshun WANG Jun HUANG Xiaobing |
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| Affiliation: | LIU Xin1,LI Shizhong1,XUE Tanshun2,WANG Jun2,HUANG Xiaobing2(1 School of Mechatronics Engineering,North University of China,Taiyuan 030051,China,2 Shanxi Beifang Huifeng Mechanical , Electronic Co.Ltd,Shanxi Changzhi 046012,China) |
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| Abstract: | Based on flux gate sensor,the principle and a method of determining the location using two-way flux gate sensor and phase information output by the sensor when zero crossing.At the same time,by simulating the movement of missile body in geomagnetic field with a two-degree-of-freedom experimental rotating platform to determine the flight attitude by geomagnetic measurement with the flux gate sensor. |
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| Keywords: | azimuth angle zero crossing flux gate sensor missile body |
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