地球静止轨道
卫星
轨道(动力学)
计算机科学
中地球轨道
近地轨道
定轨
地球同步轨道
遥感
地面轨道
人工神经网络
大地测量学
实时计算
人工智能
地质学
航空航天工程
工程类
作者
Ri‐Na Dao,Junli Yang,Limei Qi,Xiaohui Wang
标识
DOI:10.1109/csrswtc56224.2022.10098449
摘要
The geostationary earth orbit (GEO) satellite is an important part of the space situational awareness system, undertaking communication, data relay, signal early warning and other tasks. It is necessary to predict the orbit of GEO satellites in order to confirm the state and identify abnormal behavior of GEO satellite. In this work, we present a GEO satellite orbit determination method based on deep neural network, and predict the orbit elements which includes eccentricity, inclination and longitude of ascending node by processing GEO satellite position sequence to determine GEO orbit. The preliminary experimental results show that the proposed algorithm is feasible.
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