Optimal capture trajectories using multiple gravity assists

Stefan Jerg; Oliver Junge; Shane D. Ross

doi:10.1016/j.cnsns.2008.12.009

Optimal capture trajectories using multiple gravity assists

Stefan Jerg, Oliver Junge, Shane D. Ross

Professur für Numerik komplexer Systeme

Publikation: Beitrag in Fachzeitschrift › Artikel › Begutachtung

15 Zitate (Scopus)

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
Seiten (von - bis)	4168-4175
Seitenumfang	8
Fachzeitschrift	Communications in Nonlinear Science and Numerical Simulation
Jahrgang	14
Ausgabenummer	12
DOIs	https://doi.org/10.1016/j.cnsns.2008.12.009
Publikationsstatus	Veröffentlicht - Dez. 2009

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10.1016/j.cnsns.2008.12.009

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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, Optimal control, Three-body problem",

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

year = "2009",

month = dec,

doi = "10.1016/j.cnsns.2008.12.009",

language = "English",

volume = "14",

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journal = "Communications in Nonlinear Science and Numerical Simulation",

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T1 - Optimal capture trajectories using multiple gravity assists

AU - Jerg, Stefan

AU - Junge, Oliver

AU - Ross, Shane D.

PY - 2009/12

Y1 - 2009/12

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 - Optimal control

KW - Three-body problem

UR - https://www.scopus.com/pages/publications/67249113839

U2 - 10.1016/j.cnsns.2008.12.009

DO - 10.1016/j.cnsns.2008.12.009

M3 - Article

AN - SCOPUS:67249113839

SN - 1007-5704

VL - 14

SP - 4168

EP - 4175

JO - Communications in Nonlinear Science and Numerical Simulation

JF - Communications in Nonlinear Science and Numerical Simulation

IS - 12

ER -

Optimal capture trajectories using multiple gravity assists

Abstract

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