Integrated trajectory optimization for Jupiter missions with single-satellite-aided capture

DOI10.1007/S10569-023-10169-WzbMath1529.70028OpenAlexW4388480519MaRDI QIDQ6088002

Quan Jing, Ming-Tao Li

Publication date: 13 December 2023

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-023-10169-w

zbMATH Keywords

convergenceiterative numerical methodsatellite-aided capturedeep space maneuver methodGalilean moongravity assisted motioninterplanetary transfer model

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Celestial mechanics (70F15) Orbital mechanics (70M20)

Cites Work

• Multiple-satellite-aided capture trajectories at Jupiter using the Laplace resonance
• Fundamentals of astrodynamics and applications. With technical contributions by Wayne D. McClain.
• Satellite aided capture

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