@inproceedings{529572cf2ebd40b194fd80a86be84d14,
title = "Endgame design for europa lander: Ganymede to europa approach",
abstract = "The endgame scenario that was explored in this analysis consisted of the part of the trajectory starting at the last Ganymede flyby and ending at the final Europa approach. The basic design components included computing the phasing for the final Ganymede encounter, computing the required intermediate Europa flybys, determining the required maneuvers to transition between the intermediate resonances, and interfacing with a computed portal prior to the final approach. The JPL optimization software, COSMIC, was used in the ephemeris model to optimize solutions computed in the circular restricted three-body problem and compute bounds on the attainable set of solutions by sweeping various design parameters.",
author = "Anderson, {Rodney L.} and Stefano Campagnola and Dayung Koh and McElrath, {Timothy P.} and Woollands, {Robyn M.}",
note = "Publisher Copyright: {\textcopyright} 2020, Univelt Inc. All rights reserved. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; AAS/AIAA Astrodynamics Specialist Conference, 2019 ; Conference date: 11-08-2019 Through 15-08-2019",
year = "2020",
language = "English (US)",
isbn = "9780877036654",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "1427--1446",
editor = "Horneman, {Kenneth R.} and Christopher Scott and Hansen, {Brian W.} and Hussein, {Islam I.}",
booktitle = "AAS/AIAA Astrodynamics Specialist Conference, 2019",
address = "United States",
}