磁振子活动对LAPAN-A3卫星地球磁场测量的影响

Suraduita Mupasanta, Hidayah, Mukhamad Fajar Amiludin, Abdul Karim, Maria Syenni Kabes, S. Utama
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引用次数: 0

摘要

2021年,印度尼西亚国家航空航天研究所(LAPAN)成为国家研究与创新局(BRIN)的一部分,LAPAN开发并运营三颗地球观测卫星,以改善该国的监测。LAPAN- a3是LAPAN研制的第三颗卫星,其科学任务是利用磁力计传感器测量地球磁场。然而,卫星上的磁强计不仅测量地球磁场的强度和方向,而且还测量航天器电子设备引起的扰动场。此外,为了避免任务严重中断导致的姿态误差,卫星依靠分系统通过磁力矩器进行校正来保持精度。为了排除电子设备产生的磁场干扰,需要操作两台磁力计。然而,LAPAN-A3卫星只使用一个磁力计,因此它有不同的方法。因此,必须分析磁力矩器活动对LAPAN-A3卫星测量地球磁场的影响。本研究采用伪逆方法对LAPAN-A3卫星磁振器电流变化引起的磁强计数据差异进行修正。该方法的结果是一个矩阵函数,其残差在每3个磁强计的轴上。在X磁力矩器中改变1个rnA将在X方向上产生-43.2803 nT,在Z方向上产生-45.9198 nT,在Y方向上产生-0.8086 nT。由此可见,利用伪逆法可以对磁强计的测量结果进行校正。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effect of Magnetorquer Activity on the Measurement of Earth's Magnetic Field in LAPAN-A3 Satellite
In 2021, Indonesia's National Institute of Aeronautics and Space (LAPAN) become part of the National Research and Innovation Agency (BRIN), LAPAN develops and operates three earth observation satellites to improve the country's monitoring. LAPAN-A3, the third satellite developed by LAPAN, had a scientific mission to measure the earth's magnetic field by using a magnetometer sensor. However, the magnetometer onboard satellite not only measures the strength and direction of the earth's magnetic field but also a disturbance field induced by spacecraft electronics. Moreover, to avoid severely disrupted missions causing attitude error, the satellite depends on its subsystem to maintain its accuracy by using magnetorquer for correction. To exclude the disturbance of the magnetic field produced by the electronics, two magnetometers are operated. However, the LAPAN-A3 satellite only utilizes one magnetometer, hence it has a different approach. In consequence, the effect of magnetorquer activity on the measurement of the earth's magnetic field in the LAPAN-A3 Satellite has to be analyzed. In this research, a pseudo-inverse method is used to fix the difference in magnetometer data due to the changing of current in the magnetorquer on the LAPAN-A3 satellite. The method's result is a matrix function with its residual in each 3 magnetometer's axis. A change of 1 rnA in the X magnetorquer will give -43.2803 nT in the X direction, -45.9198 nT in the Z direction, and -0.8086 nT in the Y direction. It can be seen that by using pseudo-inverse, the magnetometer measurement can be corrected.
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