GPS卫星箱形翼太阳辐射压力模型及其对精确点定位的影响

IF 3.4 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE
Yi-Hsuan Tsai , Tzu-Pang Tseng , Kun-Lin Chen , Cheng-Yung Huang , Wen-Hao Yeh , Tung-Yuan Hsiao
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引用次数: 0

摘要

本文主要提出了一种处理太阳辐射压力(SRP)对GPS卫星影响的盒翼模型EBOXW。这个EBOXW模型假设了太阳能电池板和卫星总线上不同的辐射效应。我们使用20年(2001 - 2020年)的GPS轨道作为伪观测,使用所谓的轨道拟合技术来检验EBOXW的性能。轨道拟合的GPS轨道残差呈现周期性变化,这种变化与SRP模型和GPS块类型有关。在这项工作中,ECOM1和ECOM2 SRP模型都被用来验证EBOXW模型的有效性。总的来说,所有GPS块类型的轨道残差在−5 cm到+5 cm之间。仔细观察就会发现,与EBOXW模式相比,基于ec的模式在IIR-M和IIF卫星的沿轨道和交叉轨道方向上都引起了更明显的周期性变化。这可以归因于在基于ec的模型的eD方向上引入的周期项。相比之下,EBOXW模型只估计卫星X面和Z面以及太阳能板上的D0加速度。此外,三种模型都在径向上引入了显著的周期变化。总的来说,这三种模式在II和IIA卫星上工作相似。与基于ecomm的模型相比,EBOXW模型相对较好地拟合了IIR-M和IIF卫星的IGS轨道。最后,我们使用精确点定位(PPP)作为评估SRP模型对定位的影响的外部验证。尽管PPP解决方案在EBOXW情况下的改进并不显著,但所提出的EBOXW模型有效地最小化了所有块类型的基于ec的模型中发现的轨道残差。本文主要为轨道拟合技术及相关应用提供了一种备选的SRP模型。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A box-wing-like solar radiation pressure model for GPS satellites and its impact on precise point positioning
This study is mainly to propose a box-wing-like model, termed EBOXW, for handling the solar radiation pressure (SRP) effect on GPS satellite. This EBOXW model assumes the different radiation effects on both the solar panel and satellite bus. We use 20 years (from 2001 to 2020) of GPS orbits as pseudo observations to check the EBOXW performance using the so-called orbit fitting technique. We find that the GPS orbit residuals from the orbit fitting show the periodic variations, which are associated with the SRP model and the GPS Block types. In this work, both the ECOM1 and the ECOM2 SRP models are used to validate the EBOXW model for the effectiveness. Overall, the orbit residuals range from −5 cm to +5 cm for all GPS Block types. In a closer inspection, the ECOM-based model induces more pronounced periodic variation in both the along-track and cross-track directions of IIR-M and IIF satellites than the EBOXW model does. This can be attributed to the periodic terms introduced in the eD direction of the ECOM-based model. In comparison, the EBOXW model estimates the D0 acceleration only on the satellite X and Z sides, as well as the solar panel. Besides, the three models commonly introduce the significant periodic variation in the radial direction for all block types. Overall, the three models work similarly for the II and IIA satellites. The EBOXW presents the relatively well fitting to the IGS orbit for the IIR-M and IIF satellites, as compared to the ECOM-based model. In the end, we use the precise point positioning (PPP) as an external validation for assessing the impact of the SRP models on positioning. Although the improvement of the PPP solution is insignificant in the EBOXW case, the proposed EBOXW model effectively minimizes the orbital residual bias found in the ECOM-based models for all Block types. This work mainly provides an alternative SRP model for the orbit fitting technique and the related applications.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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