Inverse Calculation and Regularization Process for the Solar Aspect System (SAS) of HXI Payload on ASO-S Spacecraft | |
Yu, Ji-Rui1,2; Ruan, Ping1![]() ![]() ![]() ![]() | |
作者部门 | 光电跟踪与测量技术研究室 |
2024-04-01 | |
发表期刊 | RESEARCH IN ASTRONOMY AND ASTROPHYSICS
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ISSN | 1674-4527;2397-6209 |
卷号 | 24期号:4 |
产权排序 | 1 |
摘要 | For the ASO-S/HXI payload, the accuracy of the flare reconstruction is reliant on important factors such as the alignment of the dual grating and the precise measurement of observation orientation. To guarantee optimal functionality of the instrument throughout its life cycle, the Solar Aspect System (SAS) is imperative to ensure that measurements are accurate and reliable. This is achieved by capturing the target motion and utilizing a physical model-based inversion algorithm. However, the SAS optical system's inversion model is a typical ill-posed inverse problem due to its optical parameters, which results in small target sampling errors triggering unacceptable shifts in the solution. To enhance inversion accuracy and make it more robust against observation errors, we suggest dividing the inversion operation into two stages based on the SAS spot motion model. First, the as-rigid-as-possible (ARAP) transformation algorithm calculates the relative rotations and an intermediate variable between the substrates. Second, we solve an inversion linear equation for the relative translation of the substrates, the offset of the optical axes, and the observation orientation. To address the ill-posed challenge, the Tikhonov method grounded on the discrepancy criterion and the maximum a posteriori (MAP) method founded on the Bayesian framework are utilized. The simulation results exhibit that the ARAP method achieves a solution with a rotational error of roughly +/- 3.'' 5 (1/2-quantile); both regularization techniques are successful in enhancing the stability of the solution, the variance of error in the MAP method is even smaller-it achieves a translational error of approximately +/- 18 mu m (1/2-quantile) in comparison to the Tikhonov method's error of around +/- 24 mu m (1/2-quantile). Furthermore, the SAS practical application data indicates the method's usability in this study. Lastly, this paper discusses the intrinsic interconnections between the regularization methods. 35 |
关键词 | methods: data analysis Sun: flares Sun: X-rays gamma rays |
DOI | 10.1088/1674-4527/ad283b |
收录类别 | SCI |
语种 | 英语 |
WOS记录号 | WOS:001188032600001 |
出版者 | NATL ASTRONOMICAL OBSERVATORIES, CHIN ACAD SCIENCES |
引用统计 | |
文献类型 | 期刊论文 |
条目标识符 | http://ir.opt.ac.cn/handle/181661/97298 |
专题 | 光电跟踪与测量技术研究室 |
通讯作者 | Yu, Ji-Rui |
作者单位 | 1.Chinese Acad Sci, Xian Inst Opt & Precis Mech, Xian 710119, Peoples R China 2.Univ Chinese Acad Sci, Beijing 100049, Peoples R China 3.Chinese Acad Sci, Key Lab Dark Matter & Space Astron, Purple Mt Observ, Nanjing 210034, Peoples R China 4.Univ Sci & Technol China, Sch Astron & Space Sci, Hefei 230026, Peoples R China |
推荐引用方式 GB/T 7714 | Yu, Ji-Rui,Ruan, Ping,Su, Yang,et al. Inverse Calculation and Regularization Process for the Solar Aspect System (SAS) of HXI Payload on ASO-S Spacecraft[J]. RESEARCH IN ASTRONOMY AND ASTROPHYSICS,2024,24(4). |
APA | Yu, Ji-Rui.,Ruan, Ping.,Su, Yang.,He, Ying-Hong.,Tao, Jin-You.,...&Yang, Jian-Feng.(2024).Inverse Calculation and Regularization Process for the Solar Aspect System (SAS) of HXI Payload on ASO-S Spacecraft.RESEARCH IN ASTRONOMY AND ASTROPHYSICS,24(4). |
MLA | Yu, Ji-Rui,et al."Inverse Calculation and Regularization Process for the Solar Aspect System (SAS) of HXI Payload on ASO-S Spacecraft".RESEARCH IN ASTRONOMY AND ASTROPHYSICS 24.4(2024). |
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