A Case Study on the Effect of Atmospheric Density Calibration on Orbit Predictions with Sparse Angular Data

被引:2
作者
Chen, Junyu [1 ]
Sang, Jizhang [2 ]
Li, Zhenwei [3 ]
Liu, Chengzhi [3 ]
机构
[1] Kunming Univ Sci & Technol, Fac Land Resources Engn, Kunming 650093, Peoples R China
[2] Wuhan Univ, Sch Geodesy & Geomat, Wuhan 430079, Peoples R China
[3] Chinese Acad Sci, Changchun Observ, Natl Astron Observ, Jilin 130017, Peoples R China
关键词
space objects; space situational awareness; low-Earth orbit; atmospheric mass density model; orbit determination; SATELLITE DRAG; TRACKING;
D O I
10.3390/rs15123128
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
Accurately modeling the density of atmospheric mass is critical for orbit determination and prediction of space objects. Existing atmospheric mass density models (ADMs) have an accuracy of about 15%. Developing high-precision ADMs is a long-term goal that requires a better understanding of atmospheric density characteristics, more accurate modeling methods, and improved spatiotemporal data. This study proposes a method for calibrating ADMs using sparse angular data of space objects in low-Earth orbit over a certain period of time. Applying the corrected ADM not only improves the accuracy of orbit determination, but also enhances the accuracy of orbit prediction beyond the correction period. The study compares the impact of two calibration methods: atmospheric mass density model coefficient (ADMC) calibration and high precision satellite drag model (HASDM) calibration on the accuracy of orbit prediction of space objects. One month of ground-based telescope array angular data is used to validate the results. Space objects are classified as calibration objects, participating in ADM calibration, and verification objects, inside and outside the calibration orbit region, respectively. The results show that applying the calibrated ADM can significantly increase the accuracy of orbit prediction. For objects within the calibration orbit region, the calibration object's orbit prediction error was reduced by about 55%, while that of verification objects was reduced by about 45%. The reduction in orbit prediction error outside this region was about 30%. This proposed method contributes significantly to the development of more reliable ADMs for orbit prediction of space objects with sparse angular data and can provide significant academic value in the field of space situational awareness.
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页数:20
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