论文标题
基于全局MHD模拟的天气剩余加速度的分析
Analyses of residual accelerations for TianQin based on the global MHD simulation
论文作者
论文摘要
天气是一种提出的空间基于引力波观测站。它旨在检测0.1 MHz -1 Hz的频率范围内的重力波信号。在$ 10^5 $ km的地理距离处,地球磁层中的等离子体将成为环境噪音的主要来源。在这里,我们分析了天气测试质量的空间等离子体磁场引起的加速度噪声。高级组成资源管理器观察到的实际太阳风数据被视为磁流失动力学模拟的输入。空间天气建模框架用于模拟地球的整体磁层,我们从中获得了检测器轨道上的等离子体和磁场参数。我们计算残余加速度的时间序列以及这些轨道构型上的相应振幅光谱密度。我们发现,由太空磁场引起的TM的磁矩与航天器磁场($ \ bm {a} _ {\ rm m1} $)之间的相互作用产生的残差加速度是主要的术语,可以接近$ 10^{-15} $ M/s $/s $/s $/s $^2 $^2 $^2 $/hz $^$ 0.测试质量的磁化率($χ_ {\ rm m} = 10^{ - 5} $)和磁屏蔽因子($ξ_{\ rm m} = 10 $)。在1 MHz和10 MHz时,由空间磁场引起的加速度噪声的振幅光谱密度与惯性传感器的初步目标分别为0.38和0.08之间的比率。我们通过减少$χ_ {\ rm m} $和/或增加$ξ_ {\ rm m} $来进一步降低这种加速度噪声的进一步降低。
TianQin is a proposed space-based gravitational wave observatory. It is designed to detect the gravitational wave signals in the frequency range of 0.1 mHz -- 1 Hz. At a geocentric distance of $10^5$ km, the plasma in the earth magnetosphere will contribute as the main source of environmental noises. Here, we analyze the acceleration noises that are caused by the magnetic field of space plasma for the test mass of TianQin. The real solar wind data observed by the Advanced Composition Explorer are taken as the input of the magnetohydrodynamic simulation. The Space Weather Modeling Framework is used to simulate the global magnetosphere of the earth, from which we obtain the plasma and magnetic field parameters on the detector's orbits. We calculate the time series of the residual accelerations and the corresponding amplitude spectral densities on these orbit configurations. We find that the residual acceleration produced by the interaction between the TM's magnetic moment induced by the space magnetic field and the spacecraft magnetic field ($\bm{a}_{\rm M1}$) is the dominant term, which can approach $10^{-15}$ m/s$^2$/Hz$^{1/2}$ at $f \approx$ 0.2 mHz for the nominal values of the magnetic susceptibility ($χ_{\rm m} = 10^{-5}$) and the magnetic shielding factor ($ξ_{\rm m} = 10$) of the test mass. The ratios between the amplitude spectral density of the acceleration noise caused by the space magnetic field and the preliminary goal of the inertial sensor are 0.38 and 0.08 at 1 mHz and 10 mHz, respectively. We discuss the further reduction of this acceleration noise by decreasing $χ_{\rm m}$ and/or increasing $ξ_{\rm m}$ in the future instrumentation development for TianQin.