Optimal capture trajectories using multiple gravity assists

Details Optimal capture trajectories using multiple gravity assists Optimal capture trajectories using multiple gravity assists

Dec 2009

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2009cnsns..14.4168j&link_type=abstract

Communications in Nonlinear Science and Numerical Simulation, Volume 14, Issue 12, p. 4168-4175.

Mathematics

Combinatorics

Control Theory, Control Theory And Feedback, Numerical Optimization, Optimization, Combinatorics, Graph Theory, Jupiter, Callisto

Scientific paper

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.

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