Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems
type: Item
instance of: scholarly article
title: Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems
zbMATH Open document ID: 1447.70020
author: Y. Aharonov
published in: Celestial Mechanics and Dynamical Astronomy
publication date: 2018-06-14T00:00:00Z
Mathematics Subject Classification ID: 70M20
Mathematics Subject Classification ID: 70F05
Mathematics Subject Classification ID: 70F07
zbMATH DE Number: 6889346
zbMATH Keywords: non-Keplerian orbits
zbMATH Keywords: continuous low thrust
zbMATH Keywords: relative spacecraft motion
zbMATH Keywords: orbit period modulation
zbMATH Keywords: Hill-clohessy-wiltshire equations
zbMATH Keywords: restricted three-body problem
MaRDI profile type: Publication
full work available at URL: s10569-017-9807-3
OpenAlex ID: W2770141559
Wikidata QID: Q102054126
cites work: Artificial equilibrium points for a generalized sail in the circular restricted three-body problem
cites work: Artificial halo orbits for low-thrust propulsion spacecraft
cites work: On the stability of artificial equilibrium points in the circular restricted three-body problem
cites work: New approach to halo orbit determination and control
cites work: Q5532317
cites work: The existence and stability of families of displaced two-body orbits
cites work: Q3273009
cites work: Nonlinear dynamical analysis for displaced orbits above a planet
DOI: 10.1007/S10569-017-9807-3
description: scientific article; zbMATH DE number 6889346