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Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design

Grover, Piyush and Andersson, Christian LU (2012) 22nd AAS/AIAA Space Flight Mechanics Meeting 143 (2012). p.1189-1203
Abstract
We describe a modular optimization framework for GTO-to-moon mission design using the planar circular restricted three-body problem (PCR3BP) model. The three-body resonant gravity assists and invariant manifolds in the planar restricted three-body problem are used as basic building blocks of this mission design. The mission is optimized by appropriately timed delta-Vs, which are obtained by a shooting method and a Gauss-Pseudospectral collocation method for different phases of the mission. Depending upon the initial and final orbits, the optimized missions consume between 10-15 % less fuel compared to a Hohmann transfer, while taking around 4 to 5 months of travel time.
Please use this url to cite or link to this publication:
author
and
organization
publishing date
type
Chapter in Book/Report/Conference proceeding
publication status
published
subject
keywords
Optimization, Space Travel, Fuel Minimization, JModelica.org, Optimica, CasADi
host publication
Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting)
editor
McAdams, James V. ; McKinley, David P. ; Berry, Matthew M. and Jenkins, Keith L.
volume
143 (2012)
pages
15 pages
publisher
American Astronautical Society
conference name
22nd AAS/AIAA Space Flight Mechanics Meeting
conference location
Charleston, South Carolina, United States
conference dates
2012-01-29 - 2012-02-02
external identifiers
  • scopus:84879389135
ISSN
1081-6003
0065-3438
ISBN
978-0-87703-581-7 (print)
978-0-87703-582-4 (CD-ROM)
project
LCCC
language
English
LU publication?
yes
additional info
Abstracts of all the papers presented at the conference may be found at: http://www.univelt.com/linkedfiles/SFM2012.pdf The information about affiliations in this record was updated in December 2015. The record was previously connected to the following departments: Numerical Analysis (011015004)
id
fcd8e9ee-4b52-46ca-9d38-4a72d06550b1 (old id 4350250)
date added to LUP
2016-04-01 11:16:19
date last changed
2020-01-12 08:03:53
@inproceedings{fcd8e9ee-4b52-46ca-9d38-4a72d06550b1,
  abstract     = {We describe a modular optimization framework for GTO-to-moon mission design using the planar circular restricted three-body problem (PCR3BP) model. The three-body resonant gravity assists and invariant manifolds in the planar restricted three-body problem are used as basic building blocks of this mission design. The mission is optimized by appropriately timed delta-Vs, which are obtained by a shooting method and a Gauss-Pseudospectral collocation method for different phases of the mission. Depending upon the initial and final orbits, the optimized missions consume between 10-15 % less fuel compared to a Hohmann transfer, while taking around 4 to 5 months of travel time.},
  author       = {Grover, Piyush and Andersson, Christian},
  booktitle    = {Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting)},
  editor       = {McAdams, James V. and McKinley, David P. and Berry, Matthew M. and Jenkins, Keith L.},
  isbn         = {978-0-87703-581-7 (print)},
  issn         = {1081-6003},
  language     = {eng},
  pages        = {1189--1203},
  publisher    = {American Astronautical Society},
  title        = {Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design},
  volume       = {143 (2012)},
  year         = {2012},
}