Strategies for plane change of Earth orbits using lunar gravity and derived trajectories of family \(G\)

DOI10.1007/S10569-009-9193-6zbMath1223.70078OpenAlexW2074172907MaRDI QIDQ642264

C. F. De Melo, Othon Cabo Winter, Elbert E. N. Macau

Publication date: 26 October 2011

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

Full work available at URL: https://doi.org/10.1007/s10569-009-9193-6

zbMATH Keywords

astrodynamicsEarth-Moon systemswing-byorbital maneuversmission designgravity assisted maneuver

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (3)

Applications of celestial mechanics in natural objects and spacecrafts ⋮ Alternative transfers to the NEOs 99942 apophis, 1994 WR12, and 2007 UW1 via derived trajectories from periodic orbits of family G ⋮ Celestial mechanics, spacecrafts, and 50th years of the first humans on the Moon

Cites Work

• Fast periodic transfer orbits in the Sun-Earth-Moon quasi-bicircular problem
• Using FLI maps for preliminary spacecraft trajectory design in multi-body environments
• Extension of fast periodic transfer orbits from the Earth-Moon RTBP to the Sun-Earth-Moon quasi-bicircular problem
• Solar System Dynamics
• Control of chaos and its relevancy to spacecraft steering
• Unnamed Item

This page was built for publication: Strategies for plane change of Earth orbits using lunar gravity and derived trajectories of family \(G\)