An analytical theory for avoidance collision between space debris and operating satellites in LEO

DOI10.1016/J.APM.2013.03.045zbMath1426.70031OpenAlexW2077985271MaRDI QIDQ1791471

Yehia A. Abdel-Aziz

Publication date: 10 October 2018

Published in: Applied Mathematical Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.apm.2013.03.045

zbMATH Keywords

satellite dynamicscollisionsorbital mechanicsanalytical theorygravitational forcesnon-gravitational forces

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20)

Cites Work

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• An efficient algorithm for orbital evolution of artificial satellite
• A second order analytical atmospheric drag theory based on the TD88 thermospheric density model
• On analytic modeling of Lunar perturbations of artificial satellites of the Earth
• Virtual singularities in the artificial satellite theory

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