The study introduces dSGP4, a novel differentiable version of the widely used SGP4 model for orbital propagation. By leveraging PyTorch, dSGP4 allows for various space-related applications and machine learning integration. The research explores ML-dSGP4, a paradigm combining neural networks with the orbital propagator to improve prediction accuracy while maintaining computational efficiency. The paper discusses experiments showcasing the enhanced accuracy of ML-dSGP4 compared to traditional methods in orbit determination and satellite collision avoidance.
The content delves into the historical context of simplified perturbation models like SGP4 and their limitations in accuracy compared to numerical propagators. It highlights the importance of space situational awareness in managing resident space objects and mitigating collisions. The study emphasizes the significance of accurate orbital propagation models in ensuring safe operations in space.
Key points include distinguishing between general perturbation techniques, special perturbation techniques, semianalytical techniques, and hybrid techniques for orbital propagation. The development history of SGP4 by the US Air Force is discussed along with its limitations and extensions like SDP4 for higher orbital periods.
Furthermore, the study details how TLE data is utilized by simplified perturbation models like SGP4 but faces challenges due to underlying assumptions and errors. It explores efforts by researchers to enhance SGP4 predictions using statistical methods and machine learning approaches.
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