Analytical approach using KS elements to near-Earth orbit predictions including drag
DOI10.1098/RSPA.1991.0038zbMATH Open0717.70023OpenAlexW2106228649MaRDI QIDQ5748924
Author name not available (Why is that?)
Publication date: 1991
Published in: Proceedings of the Royal Society of London. Series A: Mathematical and Physical Sciences (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1098/rspa.1991.0038
Lagrange's planetary equationsair drag effectorbital lifetimeexponential atmospheric density modelKS total-energy element equationsmotion of near-Earth satellite orbits
Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20)
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