Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design
(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:
https://lup.lub.lu.se/record/4350250
- author
- Grover, Piyush and Andersson, Christian LU
- organization
- publishing date
- 2012
- 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
- 0065-3438
- 1081-6003
- 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
- 2024-01-07 11:48:12
@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 = {{0065-3438}}, keywords = {{Optimization; Space Travel; Fuel Minimization; JModelica.org; Optimica; CasADi}}, 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}}, }