A special perturbation method in orbital dynamics

DOI10.1007/S10569-006-9056-3zbMath1162.70022OpenAlexW1964268975WikidataQ59650363 ScholiaQ59650363MaRDI QIDQ861363

Jesús Peláez, Pedro Rodríguez de Andrés, José Manuel Hedo

Publication date: 29 January 2007

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: http://oa.upm.es/9819/

zbMATH Keywords

Numerical methodsOrbital dynamicsPropagation of orbitsSpecial perturbations

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (14)

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Cites Work

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• Motion of artificial satellites in the set of Eulerian redundant parameters. III
• Analytical solution to the perturbed \(J_ 2\) motion of artificial satellite in terms of Euler parameters
• Fundamentals of astrodynamics and applications. With technical contributions by Wayne D. McClain.
• The uniform, regular differential equations of the KS transformed perturbed two-body problem

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