贲放^1,3,,
黄威^1,3,,,
吴珊^1,3,
孟庆敏^1,3,
刘云鹤²,
廖桂香^1,3,
西永在^1,3
1. 国土资源部地球物理电磁法探测技术重点实验室, 中国地质科学院地球物理地球化学勘查研究所, 河北 廊坊 065000
2. 吉林大学地球探测科学与技术学院, 长春 130026
3. 国家现代地质勘查工程技术研究中心, 河北 廊坊 065000

基金项目: 国家重点研发计划（2017YFC0601900），基本科研业务费专项经费资助（JYYWF20180103），物化探所中央级公益性科研院所基本科研业务费专项资金资助项目（AS2017J06，AS2017Y04，AS2016J10，AS2017J02）联合资助


详细信息

作者简介: 贲放, 男, 1989年生, 工程师, 2016年博士毕业于吉林大学, 主要从事航空电磁正反演理论及数据处理与解释研究工作.E-mail:benfangzai2008@163.com

通讯作者: 黄威, 女, 1989年生, 工程师, 2016年博士毕业于吉林大学, 主要从事航空物探方法技术理论研究与应用.E-mail:huangwei2012511@163.com

中图分类号: P631

收稿日期:2017-12-02
修回日期:2018-05-15
上线日期:2018-07-05

Influence of attitude change for time domain airborne electromagnetic system

BEN Fang^1,3,,
HUANG Wei^1,3,,,
WU Shan^1,3,
MENG QingMin^1,3,
LIU YunHe²,
LIAO GuiXiang^1,3,
XI YongZai^1,3
1. Laboratory of geophysical Electromagnetic Probing Technologies, Ministry of land and Resources, Institute of Geophysical and Geochemical Exploration, Chinese Academy of Geological Science, Hebei Langfang 065000, China
2. College of Geo-exploration Sciences and Technology, Jilin University, Changchun 130026, China
3. Laboratory of Geophysical EM Probing Technologies, MLR, Hebei Langfang 065000, China


More Information

Corresponding author: HUANG Wei,E-mail:huangwei2012511@163.com

MSC: P631

--> Received Date: 02 December 2017
Revised Date: 15 May 2018
Available Online: 05 July 2018


摘要
摘要:航空电磁系统的收发线圈受外界因素影响会发生姿态变化，使测量结果产生一定偏差.传统的数据处理方法考虑姿态变化情况单一，且主要以频率域系统为主，而目前复杂姿态变化对时间域航空电磁系统全时响应的影响尚未有系统研究.本文在前人研究基础上拓宽思路，不仅研究姿态的角度变化，同时改进前人计算方法，研究线圈发生位置变化的影响，并将线圈与大地的耦合感应效应考虑在内.本文通过定义姿态变化前后两种坐标系，确定姿态变化的角度和旋转矩阵，并将一维层状半解析解与姿态角度变化和位置变化进行整合，推导出收发线圈任意姿态变化的表达式.以直升机吊舱分离装置为例，对时间域航空电磁系统收发线圈任意姿态变化进行细致分析.基于重叠偶极子的假设，给出可应用于实际工作中的姿态校正因子，以提高实测数据的处理效率与精度.
关键词: 时间域航空电磁法/
全时/
任意姿态变化/
校正因子

Abstract:The attitude of the receiver and transmitter coil of the airborne electromagnetic (AEM) system will be influenced by many external factors, which lead to a certain deviation of the measurement results. In previous studies, the processing methods of AEM data mainly consider the attitude change in frequency-domain. However, few of them focus on the complex situation of attitude change for time-domain AEM system. In this paper, we not only carry on a series of researches on angle change of attitude, but also improve the existing algorithm and take the coupling effect of coils and earth into account to study the influence of position change of coils by defining the two coordinate systems of attitude, we determine angle and rotation matrix of attitude change. Integrating the 1D layered semi-analytical solution with the change of angle and location, we derive the equation of attitude change of transform and receive coil. Additional, we taking the towed-bird separation system of helicopter as an example to analysis the arbitrary attitude change of the transceiver coil of time-domain AEM system. Moreover, based on the assumption of superposed dipole model, we provide the attitude correction factors which can be applied in practical work and improve the efficiency and precision of the measured data processing.
Key words:Time-domain AEM method/
Full-time/
Arbitrary attitude change/
Correction factor



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