Nonsingular elements in description of the motion of small eccentricity and inclination satellites

DOI10.1007/BF01230423zbMath0627.70025OpenAlexW2051282772MaRDI QIDQ3763639

Iwona Wytrzyszczak

Publication date: 1986

Published in: Celestial Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01230423

zbMATH Keywords

singularitiesgeopotentialgeopotential expansionnonsingular orbital elementszero eccentricity

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (5)

First-order accurate theory of perturbed circular motion ⋮ Third-body perturbation using a single averaged model: application in nonsingular variables ⋮ The inclination function in terms of nonsingular elements ⋮ Long-period variations of the eccentricity vector valid also for near circular orbits around a non-spherical body ⋮ An analytical solution of the Lagrange equations valid also for very low eccentricities: influence of a central potential

Cites Work

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• The geopotential in nonsingular orbital elements
• The equations of motion of an artificial satellite in nonsingular variables

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