Impact of tone errors in future satellite gravimetry missions

IF 2.8 3区 地球科学 Q2 ASTRONOMY & ASTROPHYSICS
Nikolas Pfaffenzeller, Roland Pail, Thomas Gruber
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引用次数: 0

Abstract

One of the main limiting factors to observe variations of the very low degrees and orders of the spherical harmonic (SH) spectrum of the Earth’s gravity field with satellite gravimetry missions like GRACE and GRACE-FO are the so-called tone errors. They are deterministic errors occurring periodically at the orbital frequency of the spacecraft (one cycle-per-revolution, 1 CPR) and its multiples. Tone errors are generated by external perturbations acting on the satellite at the spacecraft environment and by spacecraft-internal processes. In this study, we investigate the impact of tone errors on the resulting gravity field model and their mitigation by numerical simulations for selected mission concepts. We start with a GRACE/GRACE-FO-like single polar pair mission concept and extend the simulations to a so-called Bender double pair constellation by adding an inclined (70°) satellite pair. Within our gravity-field simulation approach, we consider realistic instrument noise assumptions for the accelerometers and the inter-satellite ranging instrument, leading to instrument-only simulation scenarios. Tone error contributions are modeled at so-called orbital harmonics at 1, 2, and 3 CPR and incorporated into the instrumental noise time series. Three selected sets of low, moderate and large tone amplitudes and the occurrence of a single tone amplitude on either 1, 2, or 3 CPR are considered to analyze the effects on gravity field retrieval. Simulation results show, that for instrument-only scenarios, tone errors significantly affect single polar pair solutions over the complete SH spectrum by amplifying resonance orders, whereas double pair solutions are less affected. Since the tone amplitudes and occurrences are known, the applied stochastic modeling based on the instrumental behavior is extended by additional notch filters to mitigate the impact of tone errors. This approach has been selected to identify its performance and applicability for gravity field determination. Applying the adapted stochastic model, we can conclude that for both satellite constellations, the erroneous effect of tone errors in the higher SH spectrum can be mitigated at the cost of increased errors in the low degrees. The behavior, as seen in the instrument-only scenarios, cannot be confirmed in additional, more realistic simulations, including temporal gravity field contributions, called full-noise scenarios. Temporal gravity field signals are, in general, larger than the erroneous signal caused by tone errors. The under-sampling of high-frequency mass signals from atmosphere, ocean and ocean tides, causing temporal aliasing, dominates the gravity field solution errors for single and double pair constellations and is up to one order of magnitude larger than the tone errors impact considering low and moderate tone amplitudes. Only with large tone amplitudes the tone error effect exceeds temporal aliasing in the case of a single polar pair. In the presence of temporal aliasing applying the adapted stochastic modeling is disadvantageous since the down-weighting of specific frequencies via notch filters also affects the temporal gravity field solutions, in particular the single polar pair. Other suitable mitigation approaches to be applied for real data processing are identified as possible options.
音调误差对未来卫星重力测量任务的影响
GRACE和GRACE- fo等卫星重力测量任务观测地球重力场球面谐波谱(SH)极低度和阶数变化的主要限制因素之一是所谓的音调误差。它们是在航天器轨道频率(每转一圈,1次CPR)及其倍数上周期性发生的确定性错误。音调误差是由作用于卫星的外部扰动和航天器内部过程产生的。在本研究中,我们通过对选定的任务概念进行数值模拟,研究音调误差对产生的重力场模型的影响及其缓解措施。我们从GRACE/GRACE- fo类单极对任务概念开始,并通过添加倾斜(70°)卫星对将模拟扩展到所谓的Bender双对星座。在我们的重力场模拟方法中,我们考虑了加速度计和卫星间测距仪器的现实仪器噪声假设,从而导致仅仪器的模拟场景。音调误差的贡献是在所谓的1、2和3 CPR的轨道谐波上建模的,并纳入仪器噪声时间序列。选取三组低、中、大音调幅值,以及在1、2、3次CPR中出现单一音调幅值,分析对重力场反演的影响。仿真结果表明,在仅使用仪器的情况下,音调误差通过放大共振阶数显著影响整个SH谱的单极对解,而双极对解的影响较小。由于音调振幅和频率是已知的,基于仪器行为的应用随机建模被额外的陷波滤波器扩展,以减轻音调误差的影响。选择这种方法是为了确定其在重力场测定中的性能和适用性。应用自适应随机模型,我们可以得出结论,对于两个卫星星座来说,高SH谱的音调误差的错误影响可以减轻,但代价是低SH谱的误差增加。仅在仪器场景中看到的行为,不能在其他更真实的模拟中得到证实,包括时间重力场贡献,称为全噪声场景。一般情况下,时间重力场信号大于音调误差引起的误差信号。大气、海洋和海潮高频质量信号的欠采样导致时间混叠,在单对和双对星座的重力场解误差中占主导地位,考虑到低频和中频振幅,重力场解误差的影响比音调误差的影响大一个数量级。只有在音调振幅较大的情况下,音调误差效应才会超过单极性对的时间混叠效应。在存在时间混叠的情况下,应用自适应随机建模是不利的,因为通过陷波滤波器降低特定频率的权重也会影响时间重力场解,特别是单极对。确定了可用于实际数据处理的其他适当缓解办法。
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来源期刊
Advances in Space Research
Advances in Space Research 地学天文-地球科学综合
CiteScore
5.20
自引率
11.50%
发文量
800
审稿时长
5.8 months
期刊介绍: The COSPAR publication Advances in Space Research (ASR) is an open journal covering all areas of space research including: space studies of the Earth''s surface, meteorology, climate, the Earth-Moon system, planets and small bodies of the solar system, upper atmospheres, ionospheres and magnetospheres of the Earth and planets including reference atmospheres, space plasmas in the solar system, astrophysics from space, materials sciences in space, fundamental physics in space, space debris, space weather, Earth observations of space phenomena, etc. NB: Please note that manuscripts related to life sciences as related to space are no more accepted for submission to Advances in Space Research. Such manuscripts should now be submitted to the new COSPAR Journal Life Sciences in Space Research (LSSR). All submissions are reviewed by two scientists in the field. COSPAR is an interdisciplinary scientific organization concerned with the progress of space research on an international scale. Operating under the rules of ICSU, COSPAR ignores political considerations and considers all questions solely from the scientific viewpoint.
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