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

Piyush Grover; Christian Andersson

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

Piyush Grover, Christian Andersson

Matematik LTH

Forskningsoutput: Kapitel i bok/rapport/Conference proceeding › Konferenspaper i proceeding › Peer review

Sammanfattning

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.

Originalspråk	engelska
Titel på värdpublikation	Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting)
Redaktörer	James V. McAdams, David P. McKinley, Matthew M. Berry, Keith L. Jenkins
Förlag	American Astronautical Society
Sidor	1189-1203
Antal sidor	15
Volym	143 (2012)
ISBN (tryckt)	978-0-87703-581-7 (print), 978-0-87703-582-4 (CD-ROM)
Status	Published - 2012
Evenemang	22nd AAS/AIAA Space Flight Mechanics Meeting - Charleston, South Carolina, USA Varaktighet: 2012 jan. 29 → 2012 feb. 2

Publikationsserier

Namn
Volym	143 (2012)
ISSN (tryckt)	1081-6003
ISSN (elektroniskt)	0065-3438

Konferens

Konferens	22nd AAS/AIAA Space Flight Mechanics Meeting
Land/Territorium	USA
Ort	Charleston, South Carolina
Period	2012/01/29 → 2012/02/02

Bibliografisk information

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)

Ämnesklassifikation (UKÄ)

Matematik

LCCC
Holmqvist, A. (Forskare), Andersson, N. (Forskare), Cervin, A. (Forskare), Mannesson, A. (Forskare), Gattami, A. (Forskare), Ghulchak, A. (Forskare), Papadopoulos, A. V. (Forskare), Rantzer, A. (Forskare), Robertsson, A. (Forskare), Sootla, A. (Forskare), THEORIN, A. (Forskare), Bernhardsson, B. (Forskare), Olofsson, B. (Forskare), Wittenmark, B. (Forskare), Grussler, C. (Forskare), Johnsson, C. (Forskare), MADJIDIAN, D. (Forskare), Johannesson, E. (Forskare), Magnusson, F. (Forskare), Ståhl, F. (Forskare), Como, G. (Forskare), Chasparis, G. (Forskare), Turesson, G. (Forskare), Dressler, I. (Forskare), Åkesson, J. (Forskare), Cho, J. H. (Forskare), Årzén, K.-E. (Forskare), Åström, K. J. (Forskare), Sou, K. C. (Forskare), Mårtensson, K. (Forskare), Berntorp, K. (Forskare), Soltesz, K. (Forskare), Lessard, L. (Forskare), Hast, M. (Forskare), Rönn, M. (Forskare), Ansbjerg Kjær, M. (Forskare), Maggio, M. (Forskare), Kristalny, M. (Forskare), Garpinger, O. (Forskare), From, P. J. (Forskare), Larsson, P.-O. (Forskare), Giselsson, P. (Forskare), Johansson, R. (Forskare), Hägglund, T. (Forskare), Vladimerou, V. (Forskare), Romero Segovia, V. (Forskare), Aurelius, A. (Forskare), Cedersjö, G. (Forskare), Bür, K. (Forskare), Dellkrantz, M. (Forskare), Du, M. (Forskare), Amani, P. (Forskare), Larsson, R. (Forskare), Tärneberg, W. (Forskarstuderande), Li, Z. (Forskare), Yin, L. (Forskare), Tufvesson, F. (Forskare), Höst, S. (Forskare), Nilsson, B. (Forskare), Stenström, S. (Forskare), Andersson, J. A. (Forskare), Diehl, S. (Forskare), Dürango, J. (Forskare), Ghazaei Ardakani, M. (Forskare), Forsberg, P.-O. (Forskare), Bengtsson, F. (Forskare), Jörntell, H. (Forskare), Arévalo, C. (Forskare), Führer, C. (Forskare), Andersson, C. (Forskare), Mohammadi, F. (Forskare), Ödling, P. (Forskare), Andersson, M. (Forskare), Kihl, M. (Forskare) & Tunestål, P. (Forskare)
2008/07/01 → 2018/06/30
Projekt: Forskning

Citera det här

Grover, P., & Andersson, C. (2012). Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design. I J. V. McAdams, D. P. McKinley, M. M. Berry, & K. L. Jenkins (Red.), Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting) (Vol. 143 (2012), s. 1189-1203). American Astronautical Society.

Grover, Piyush ; Andersson, Christian. / Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design. Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting). redaktör / James V. McAdams ; David P. McKinley ; Matthew M. Berry ; Keith L. Jenkins. Vol. 143 (2012) American Astronautical Society, 2012. s. 1189-1203

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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.",

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Grover, P & Andersson, C 2012, Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design. i JV McAdams, DP McKinley, MM Berry & KL Jenkins (red), Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting). vol. 143 (2012), American Astronautical Society, s. 1189-1203, 22nd AAS/AIAA Space Flight Mechanics Meeting, Charleston, South Carolina, USA, 2012/01/29.

Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design. / Grover, Piyush; Andersson, Christian.
Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting). red. / James V. McAdams; David P. McKinley; Matthew M. Berry; Keith L. Jenkins. Vol. 143 (2012) American Astronautical Society, 2012. s. 1189-1203.

Forskningsoutput: Kapitel i bok/rapport/Conference proceeding › Konferenspaper i proceeding › Peer review

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AU - Grover, Piyush

AU - Andersson, Christian

N1 - 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)

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AB - 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.

KW - Optimization

KW - Space Travel

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KW - Optimica

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SN - 978-0-87703-582-4 (CD-ROM)

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BT - Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting)

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Grover P, Andersson C. Optimized Three-Body Gravity Assists and Manifold Transfers in End-to-End Lunar Mission Design. I McAdams JV, McKinley DP, Berry MM, Jenkins KL, redaktörer, Advances in the Astronautical Sciences (Spaceflight Mechanics 2012: Proceedings of the 22nd AAS/AIAA Space Flight Mechanics Meeting). Vol. 143 (2012). American Astronautical Society. 2012. s. 1189-1203

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

Sammanfattning

Publikationsserier

Konferens

Bibliografisk information

Ämnesklassifikation (UKÄ)

Fingeravtryck

Projekt

LCCC

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