高精度航空重力测量系统分项指标设计分析
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  • 英文篇名:Design and analysis of sub-index of high precision Airborne Gravity System
  • 作者:张虹 ; 屈进红 ; 姜作喜 ; 王萌 ; 李行素
  • 英文作者:ZHANG Hong;QU Jin-Hong;JIANG Zuo-Xi;WANG Meng;LI Xing-Su;Beijing information technology School of Information Management;Key laboratory of Airborne Geophysics and Remote Sensing Geology,Ministry of Natural Resources;China Aero Geophysical Survey and Remote Sensing Center for Natural Resources;
  • 关键词:高精度航空重力仪 ; 误差模型 ; 各项误差分析 ; 分项指标精度
  • 英文关键词:high precision Airborne Gravimeter;;error model;;error analysis;;sub item accuracy
  • 中文刊名:WTYH
  • 英文刊名:Geophysical and Geochemical Exploration
  • 机构:北京信息科技大学信息管理学院;自然资源部航空地球物理与遥感地质重点实验室;中国自然资源航空物探遥感中心;
  • 出版日期:2019-04-15
  • 出版单位:物探与化探
  • 年:2019
  • 期:v.43
  • 基金:国家重点研发计划项目(2017YFC0601706、2017YFC0601705)
  • 语种:中文;
  • 页:WTYH201902022
  • 页数:7
  • CN:02
  • ISSN:11-1906/P
  • 分类号:189-195
摘要
为研制高精度航空重力仪,开展了高精度航空重力仪分项指标设计与分析,为高精度航空重力测量系统设计提供依据。笔者基于航空重力测量的数学模型,归纳出影响航空重力测量的主要因素;结合航空重力测量的相关理论公式,使用理论模型,推导出各影响因素的误差模型;开展了各项误差的分析研究,并通过设定合理的分项指标精度来有效地控制分项误差,确保航空重力测量精度优于0.6×10-5m/s2。
        In order to meet the needs of development of high-precision airborne gravimeter,the sub-index design and analysis of highprecision airborne gravimeter were carried out,which provided the basis for the design of high-precision airborne gravimeter system.Based on the mathematical model of airborne gravimetry,this paper summarizes the main errors affecting airborne gravimetry,uses the theoretical model formula,deduces the error models of various influencing factors,and carries out the analysis and study of various errors,and sets reasonable sub-index by combining the relevant theoretical formula of airborne gravimetry. Accuracy can effectively control the sub item errors and ensure the accuracy of airborne gravity measurement is better than 0.6×10~(-5) m/s~2.
引文
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