Uniform formulation for orbit computation: the intermediate elements
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Publication:2004678
DOI10.1007/s10569-020-9952-yzbMath1448.70063arXiv1912.00795OpenAlexW2990000950MaRDI QIDQ2004678
Publication date: 7 October 2020
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://arxiv.org/abs/1912.00795
Related Items (2)
Quaternion methods and models of regular celestial mechanics and astrodynamics ⋮ Quaternion methods and regular models of celestial mechanics and space flight mechanics: the use of Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. I: Review and analysis of methods and models and their applications
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