Mission design through averaging of perturbed Keplerian systems: the paradigm of an Enceladus orbiter

DOI10.1007/S10569-010-9286-2zbMath1223.70047OpenAlexW2027731272MaRDI QIDQ642366

Jesús F. Palacián, Ryan P. Russell, Martin Lara

Publication date: 26 October 2011

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

Full work available at URL: https://doi.org/10.1007/s10569-010-9286-2

zbMATH Keywords

stabilityperiodic orbitsperturbation methodsartificial satellitesHill's problemrestricted problemsfrozen orbitssatellite orbiter

Mathematics Subject Classification ID

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

Related Items (12)

Reduced 4D oscillators and orbital elements in Keplerian systems: Cushman-Deprit coordinates ⋮ Analytical investigations of quasi-circular frozen orbits in the martian gravity field ⋮ A Hopf variables view on the libration points dynamics ⋮ End-to-end trajectory concept for close exploration of Saturn's inner large moons ⋮ Planetary satellite orbiters: applications for the Moon ⋮ Higher order approximation to the Hill problem dynamics about the libration points ⋮ Exploring the long-term dynamics of perturbed Keplerian motion in high degree potential fields ⋮ Design and performance of low-energy orbits for the exploration of Enceladus ⋮ Mission design through averaging of perturbed Keplerian systems: the paradigm of an Enceladus orbiter ⋮ Some orbital characteristics of lunar artificial satellites ⋮ FROZEN ORBITS AROUND EUROPA ⋮ Families of frozen orbits of lunar artificial satellites

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