Natural and non-natural spacecraft formations near the L1and L2libration points in the Sun–Earth/Moon ephemeris system

DOI10.1080/1468936042000298224zbMath1062.70027OpenAlexW2064967585MaRDI QIDQ4651114

Kathleen C. Howell, B. G. Marchand

Publication date: 21 February 2005

Published in: Dynamical Systems (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/1468936042000298224

zbMATH Keywords

discrete control

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Celestial mechanics (70F15)

Related Items (3)

Describing relative motion near periodic orbits via local toroidal coordinates ⋮ Formation reconfiguration in restricted three body problem ⋮ Floquet-based design and control approach to spacecraft formation flying in libration point orbits

Cites Work

• Numerical determination of Lissajous trajectories in the restricted three-body problem
• Long-Term Formation Keeping of Satellite Constellation Using Linear-Quadratic Controller

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