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Modeling spurious forces on the LISA spacecraft across a full solar cycle
Classical and Quantum Gravity ( IF 3.5 ) Pub Date : 2020-08-04 , DOI: 10.1088/1361-6382/ab9bba
Barrett M Frank 1, 2 , Brandon Piotrzkowski 1, 3 , Brett Bolen 1 , Marco Cavagli 4 , Shane L Larson 5
Affiliation  

One source of noise for the laser interferometer space antenna (LISA) will be time-varying changes of the space environment in the form of solar wind particles and photon pressure from fluctuating solar irradiance. The approximate magnitude of these effects can be estimated from the average properties of the solar wind and the solar irradiance. We use data taken by the ACE (advanced Compton explorer) satellite and the VIRGO (variability of solar iRradiance and gravity oscillations) instrument on the SOHO satellite over an entire solar cycle to calculate the forces due to solar wind and photon pressure irradiance on the LISA spacecraft. We produce a realistic model of the effects of these environmental noise sources and their variation over the expected course of the LISA mission.

中文翻译:

在整个太阳周期内模拟LISA航天器上的杂散力

激光干涉仪空间天线(LISA)的一种噪声来源将是空间环境的时变变化,其形式为太阳风粒子和太阳辐照度波动引起的光子压力。这些影响的近似大小可以从太阳风和太阳辐照度的平均属性来估计。我们使用ACE(高级Compton探测器)卫星和SOHO卫星上的VIRGO(太阳辐照度和重力振荡的变异性)仪在整个太阳周期内获取的数据来计算LISA上由于太阳风和光子压力辐照而产生的力飞船。我们为这些环境噪声源的影响及其在LISA任务预期过程中的变化提供了一个逼真的模型。
更新日期:2020-08-05
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