In-flight calibration of the spaceborne fluxgate magnetometer in the Martian magnetosheath  

作　　者：GuoQiang Wang 

机构地区：[1]Institute of Space Science and Applied Technology,Harbin Institute of Technology,Shenzhen 518055,China

出　　处：《Earth and Planetary Physics》2022年第6期592-600,共9页地球与行星物理（英文版）

基　　金：supported by the Shenzhen Science and Technology Research Program (JCYJ20210324121412034);the Guangdong Basic and Applied Basic Research Foundation (2022A1515011698);supported by the NASA (National Aeronautics and Space Administration) Mars Exploration Program

摘　　要：In-flight calibration of the ze ro offset is crucial for ensuring high-precision measure ment of the spaceborne fluxgate magnetomete r.Tianwen-1 is China’s first Mars mission,and its orbiter will re main out of the solar wind for tens of days each year.Previous in-flight calibration methods might not be suitable for this orbiter during such a period.Recently,a new method was proposed by Wang GQ(2022 b),which we refer to as the Wang method Ⅱ for ease of description.Here,we test the performance of this method in the Martian magnetosheath by using magnetic field data measured by the Mars Atmosphere and Volatile EvolutioN(MAVEN) spacecraft.We find that the accuracy of the Wang method Ⅱ is affected by the number of magnetic field subinterval events,the eigenvalues of the minimum variance analysis for each event,and the position of the spacecraft in the magnetosheath.The estimated zero offset varies over a period of~27 days and has a 57.3% probability of accuracy within 2.0 nT.After being smoothed with a temporal window of 27 days,the ze ro offset has a 48.4%(99.3%) probability of accuracy within 1.0(2.0) nT.Our tests suggest that the Wang method Ⅱ provides an option for the Tianwen-1 orbiter to perform in-flight calibration when the orbiter remains out of the solar wind for an extended pe riod of time.

关 键 词：fluxgate magnetometer in-flight calibration zero offset Martian magnetosheath 

分 类 号：V476.4[航空宇航科学与技术—飞行器设计] P185.3[天文地球—天文学]