利用监督学习进行卫星间链路预测:极轨应用

Estel Ferrer, J. A. Ruiz-de-Azua, Francesc Betorz, Josep Escrig
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引用次数: 0

摘要

分布式空间系统通过多颗异构卫星之间的协作和资源共享提高了任务性能,因此在航天工业中日益受到重视。此外,通过卫星间链路(ISL)实现自主和实时的卫星对卫星通信,可以进一步提高整体性能,无需依赖地面链路和不同利益攸关方之间的广泛协调努力即可开展合作。鉴于卫星上的可用资源有限,实现具有成本效益的自主合作的一个关键因素是尽量减少因通信不成功或不必要而造成的能源浪费。为应对这一挑战,卫星必须以最小的资源利用率预测其 ISL 机会或遭遇。在之前发表的论文基础上,这项工作进一步深入探讨了如何利用监督学习,使卫星能够在不依赖轨道传播的情况下预测其相遇情况。特别是,对卫星相遇进行了更现实的定义,并实施了适用于所有极地低地轨道卫星的通用解决方案。结果表明,训练有素的模型可以预测来自现有数据源的现实数据和未见数据的相遇情况,平衡精度约为 90%,与著名的简化一般扰动 4 轨道模型相比,速度快六倍。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Inter-Satellite Link Prediction with Supervised Learning: An Application in Polar Orbits
Distributed space systems are increasingly valued in the space industry, as they enhance mission performance through collaborative efforts and resource sharing among multiple heterogeneous satellites. Additionally, enabling autonomous and real-time satellite-to-satellite communications through Inter-Satellite Links (ISLs) can further increase the overall performance by allowing cooperation without relying on ground links and extensive coordination efforts among diverse stakeholders. Given the constrained resources available onboard satellites, a crucial element of achieving cost-effective and autonomous cooperation involves minimizing energy wastage resulting from unsuccessful or unnecessary communication. To address this challenge, satellites must anticipate their ISL opportunities or encounters with minimal resource utilization. Building upon prior publications, this work presents further insights into the use of supervised learning to enable satellites to forecast their encounters without relying on orbit propagation. In particular, a more realistic definition of satellite encounters, along with a versatile solution applicable to all polar low-Earth orbit satellites is implemented. Results show that the trained model can anticipate encounters for realistic and unseen data from an available data source with a balance accuracy of around 90% and six times faster when compared with the well-known Simplified General Perturbation 4 orbital model.
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