Modified Chebyshev-Picard iteration methods for station-keeping of translunar halo orbits

DOI10.1155/2012/926158zbMath1264.70032OpenAlexW2089730637WikidataQ58912679 ScholiaQ58912679MaRDI QIDQ1955351

John L. Junkins, Xiao-Li Bai

Publication date: 11 June 2013

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2012/926158

Mathematics Subject Classification ID

Three-body problems (70F07) Celestial mechanics (70F15)

Related Items (2)

Numerical solution of two-point nonlinear boundary value problems via Legendre-Picard iteration method ⋮ Bandlimited implicit Runge-Kutta integration for astrodynamics

Cites Work

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• The ?Halo? family of 3-dimensional periodic orbits in the Earth-Moon restricted 3-body problem
• Analytic construction of periodic orbits about the collinear points
• New approach to halo orbit determination and control
• Quasi-periodic orbits about the translunar libration point

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