Formation reconfiguration in restricted three body problem

DOI10.1007/s10409-007-0074-5zbMath1202.70121OpenAlexW2053513864MaRDI QIDQ612407

He-Xi Baoyin, Jun-Feng Li, Yun-Feng Gao, Sheng-Ping Gong

Publication date: 28 December 2010

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-007-0074-5

zbMATH Keywords

three body problemformation flyinghalo orbitformation reconfiguration

Mathematics Subject Classification ID

Three-body problems (70F07) Orbital mechanics (70M20)

Related Items (2)

Multi-swingby optimization of mission to Saturn using global optimization algorithms ⋮ An improved nonlinear control strategy for deep space formation flying spacecraft

Cites Work

• Unnamed Item
• Study on relative orbital configuration in satellite formation flying
• Study of the transfer from the Earth to a halo orbit around the equilibrium point \(L_ 1\)
• Natural and non-natural spacecraft formations near the L₁and L₂libration points in the Sun–Earth/Moon ephemeris system

This page was built for publication: Formation reconfiguration in restricted three body problem