Mission design through averaging of perturbed Keplerian systems: the paradigm of an Enceladus orbiter
type: Item
instance of: scholarly article
title: Mission design through averaging of perturbed Keplerian systems: the paradigm of an Enceladus orbiter
zbMATH Open document ID: 1223.70047
author: Jesús F. Palacián
author: Ryan P. Russell
author: Martín Lara
published in: Celestial Mechanics and Dynamical Astronomy
publication date: 2011-10-26T00:00:00Z
Mathematics Subject Classification ID: 70F15
Mathematics Subject Classification ID: 70M20
zbMATH DE Number: 5964095
zbMATH Keywords: restricted problems
zbMATH Keywords: Hill's problem
zbMATH Keywords: periodic orbits
zbMATH Keywords: stability
zbMATH Keywords: artificial satellites
zbMATH Keywords: perturbation methods
zbMATH Keywords: frozen orbits
zbMATH Keywords: satellite orbiter
MaRDI profile type: Publication
full work available at URL: s10569-010-9286-2
OpenAlex ID: W2027731272
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DOI: 10.1007/S10569-010-9286-2
description: scientific article; zbMATH DE number 5964095