Orbital maneuvers to reach and explore a triple asteroid

DOI10.1007/S40314-016-0307-YzbMath1348.70024OpenAlexW2301403193MaRDI QIDQ338291

Jorge Kennety Silva Formiga, Denilson Paulo Souza dos Santos

Publication date: 4 November 2016

Published in: Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s40314-016-0307-y

zbMATH Keywords

genetic algorithmrestricted three-body problemclose approachorbital maneuversspace trajectories

Mathematics Subject Classification ID

Three-body problems (70F07) Two-body problems (70F05) Celestial mechanics (70F15)

Related Items (2)

Study of collision probability considering a non-uniform cloud of space debris ⋮ Orbital effects in a cloud of space debris making a close approach with the earth

Cites Work

• Lambert problem solution in the Hill model of motion
• Optimal multiple-impulse time-fixed rendezvous between circular orbits
• Transfer orbits in the Earth-moon system using a regularized model
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