中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Inverse Calculation and Regularization Process for the Solar Aspect System (SAS) of HXI Payload on ASO-S Spacecraft

文献类型:期刊论文

作者Yu, Ji-Rui3,4; Ruan, Ping4; Su, Yang1,2; He, Ying-Hong4; Tao, Jin-You4; Zhang, Zhe2; Guo, Song3,4; Xue, Bin4; Yang, Jian-Feng4
刊名RESEARCH IN ASTRONOMY AND ASTROPHYSICS
出版日期2024-04-01
卷号24期号:4
关键词methods: data analysis Sun: flares Sun: X-rays gamma rays
ISSN号1674-4527;2397-6209
DOI10.1088/1674-4527/ad283b
产权排序1
英文摘要

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

语种英语
WOS记录号WOS:001188032600001
出版者NATL ASTRONOMICAL OBSERVATORIES, CHIN ACAD SCIENCES
源URL[http://ir.opt.ac.cn/handle/181661/97298]  
专题西安光学精密机械研究所_光电测量技术实验室
通讯作者Yu, Ji-Rui
作者单位1.Univ Sci & Technol China, Sch Astron & Space Sci, Hefei 230026, Peoples R China
2.Chinese Acad Sci, Key Lab Dark Matter & Space Astron, Purple Mt Observ, Nanjing 210034, Peoples R China
3.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
4.Chinese Acad Sci, Xian Inst Opt & Precis Mech, Xian 710119, 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).

入库方式: OAI收割

来源:西安光学精密机械研究所

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