Selective Tensorized Multi-layer LSTM for Orbit Prediction

Youjin Shin, Eun-Ju Park, Simon S. Woo, Ok-Cheol Jung, D. Chung
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Abstract

Although the collision of space objects not only incurs a high cost but also threatens human life, the risk of collision between satellites has increased, as the number of satellites has rapidly grown due to the significant interests in many space applications. However, it is not trivial to monitor the behavior of the satellite in real-time since the communication between the ground station and spacecraft is dynamic and sparse, and there is an increased latency due to the long distance. Accordingly, it is strongly required to predict the orbit of a satellite to prevent unexpected contingencies such as a collision. Therefore, the real-time monitoring and accurate orbit prediction are required. Furthermore, it is necessary to compress the prediction model, while achieving a high prediction performance in order to be deployable in the real systems. Although several machine learning and deep learning-based prediction approaches have been studied to address such issues, most of them have applied only basic machine learning models for orbit prediction without considering the size, running time, and complexity of the prediction model. In this research, we propose Selective Tensorized multi-layer LSTM (ST-LSTM) for orbit prediction, which not only improves the orbit prediction performance but also compresses the size of the model that can be applied in practical deployable scenarios. To evaluate our model, we use the real orbit dataset collected from the Korea Multi-Purpose Satellites (KOMPSAT-3 and KOMPSAT-3A) of the Korea Aerospace Research Institute (KARI) for 5 years. In addition, we compare our ST-LSTM to other machine learning-based regression models, LSTM, and basic tensorized LSTM models with regard to the prediction performance, model compression rate, and running time.
轨道预测的选择性张拉多层LSTM
虽然空间物体的碰撞不仅造成高昂的成本,而且还威胁到人类的生命,但随着许多空间应用的重大利益使卫星数量迅速增加,卫星间碰撞的风险也增加了。然而,由于地面站与航天器之间的通信是动态的、稀疏的,并且由于距离较远,延迟会增加,因此实时监测卫星的行为并非易事。因此,预测卫星的轨道是防止碰撞等意外事件发生的必要条件。因此,需要对卫星进行实时监测和准确的轨道预测。此外,有必要对预测模型进行压缩,同时达到较高的预测性能,以便在实际系统中部署。虽然已经研究了几种基于机器学习和深度学习的预测方法来解决这些问题,但大多数方法只应用基本的机器学习模型进行轨道预测,而没有考虑预测模型的大小、运行时间和复杂性。在本研究中,我们提出了用于轨道预测的选择性张紧化多层LSTM (ST-LSTM),不仅提高了轨道预测性能,而且压缩了可应用于实际部署场景的模型大小。为了评估我们的模型,我们使用了韩国航空航天研究所(KARI)的韩国多用途卫星(KOMPSAT-3和KOMPSAT-3A) 5年来收集的真实轨道数据集。此外,我们将ST-LSTM与其他基于机器学习的回归模型、LSTM和基本张紧LSTM模型在预测性能、模型压缩率和运行时间方面进行了比较。
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