arXiv Open Access 2024

Computing Classical Orbital Elements with Improved Efficiency and Accuracy

Roberto Flores Elena Fantino
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Abstrak

This paper reviews the standard algorithm for converting spacecraft state vectors to Keplerian orbital elements with a focus on its computer implementation. It analyzes the shortcomings of the scheme as described in the literature, and proposes changes to the implementation to address orbits of arbitrary eccentricity and inclination in a simple and robust way. It presents two coding strategies that simplify the program structure while improving the accuracy and speed of the transformation on modern computer architectures. Comprehensive numerical benchmarks demonstrate accuracy improvements by two orders of magnitude, together with a 40% reduction of computational cost relative to the standard implementation.

Penulis (2)

R

Roberto Flores

E

Elena Fantino

Format Sitasi

Flores, R., Fantino, E. (2024). Computing Classical Orbital Elements with Improved Efficiency and Accuracy. https://arxiv.org/abs/2404.18141

Akses Cepat

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Informasi Jurnal
Tahun Terbit
2024
Bahasa
en
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arXiv
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Open Access ✓