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 |
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Seiten (von - bis) | 4168-4175 |
Seitenumfang | 8 |
Fachzeitschrift | Communications in Nonlinear Science and Numerical Simulation |
Jahrgang | 14 |
Ausgabenummer | 12 |
DOIs | |
Publikationsstatus | Veröffentlicht - Dez. 2009 |