Designing rendezvous missions with mini-moons using geometric optimal control

DOI10.3934/jimo.2014.10.477zbMath1276.49017OpenAlexW2321839020MaRDI QIDQ380585

Monique Chyba, Jeremie Vaubaillon, Gautier Picot, Robert Jedicke, Mikael Granvik, Geoff Patterson

Publication date: 14 November 2013

Published in: Journal of Industrial and Management Optimization (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3934/jimo.2014.10.477

zbMATH Keywords

optimal controlnatural earth satellitesorbital transfertemporarily captured orbiters

Mathematics Subject Classification ID

Numerical methods based on necessary conditions (49M05) Variable mass, rockets (70P05) Orbital mechanics (70M20) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (1)

Indirect methods for fuel-minimal rendezvous with a large population of temporarily captured orbiters

Cites Work

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