Optimal capture trajectories using multiple gravity Assists

Stefan Jerg; Oliver Junge; Shane D. Ross

doi:10.1007/978-90-481-9884-9_16

Optimal capture trajectories using multiple gravity Assists

Stefan Jerg
, Oliver Junge
, Shane D. Ross

Professur für Numerik komplexer Systeme

Technische Universität München
Virginia Polytechnic Institute and State University

Publikation: Beitrag in Buch/Bericht/Konferenzband › Kapitel › Begutachtung

Abstract

Graph theoretic methods of optimal control in the presence of uncertainty are applied to a celestial mechanics problem. We find a fuel-efficient spacecraft trajectory which starts at infinity and is captured by the smaller member of a binary system, e.g., a moon of Jupiter, using multiple gravity assists.

Originalsprache	Englisch
Titel	Nonlinear Science and Complexity
Herausgeber (Verlag)	Springer Netherlands
Seiten	125-130
Seitenumfang	6
ISBN (Print)	9789048198832
DOIs	https://doi.org/10.1007/978-90-481-9884-9_16
Publikationsstatus	Veröffentlicht - 2011

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10.1007/978-90-481-9884-9_16

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title = "Optimal capture trajectories using multiple gravity Assists",

abstract = "Graph theoretic methods of optimal control in the presence of uncertainty are applied to a celestial mechanics problem. We find a fuel-efficient spacecraft trajectory which starts at infinity and is captured by the smaller member of a binary system, e.g., a moon of Jupiter, using multiple gravity assists.",

keywords = "Celestial mechanics, Graph partitioning, Gravity assist, Optimal control, Periapsis map, Shortest path, Symplectic map, Three-body problem",

author = "Stefan Jerg and Oliver Junge and Ross, \{Shane D.\}",

year = "2011",

doi = "10.1007/978-90-481-9884-9\_16",

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T1 - Optimal capture trajectories using multiple gravity Assists

AU - Jerg, Stefan

AU - Junge, Oliver

AU - Ross, Shane D.

PY - 2011

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N2 - Graph theoretic methods of optimal control in the presence of uncertainty are applied to a celestial mechanics problem. We find a fuel-efficient spacecraft trajectory which starts at infinity and is captured by the smaller member of a binary system, e.g., a moon of Jupiter, using multiple gravity assists.

AB - Graph theoretic methods of optimal control in the presence of uncertainty are applied to a celestial mechanics problem. We find a fuel-efficient spacecraft trajectory which starts at infinity and is captured by the smaller member of a binary system, e.g., a moon of Jupiter, using multiple gravity assists.

KW - Celestial mechanics

KW - Graph partitioning

KW - Gravity assist

KW - Optimal control

KW - Periapsis map

KW - Shortest path

KW - Symplectic map

KW - Three-body problem

UR - https://www.scopus.com/pages/publications/84895202216

U2 - 10.1007/978-90-481-9884-9_16

DO - 10.1007/978-90-481-9884-9_16

M3 - Chapter

AN - SCOPUS:84895202216

SN - 9789048198832

SP - 125

EP - 130

BT - Nonlinear Science and Complexity

PB - Springer Netherlands

ER -

Optimal capture trajectories using multiple gravity Assists

Abstract

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