Eight-shaped Lissajous orbits in the Earth-Moon system
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Publication:420301
DOI10.5802/msia.5zbMath1238.70023OpenAlexW2313667691MaRDI QIDQ420301
Grégory Archambeau, Philippe Augros, Emmanuel Trélat
Publication date: 21 May 2012
Published in: MathematicS In Action (Search for Journal in Brave)
Full work available at URL: https://eudml.org/doc/219789
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Cites Work
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- Computation of heteroclinic orbits between normally hyperbolic invariant 3-spheres foliated by 2-dimensional invariant tori in hill's problem
- Determining Lyapunov exponents from a time series
- Lyapunov characteristic exponents for smooth dynamical systems and for Hamiltonian systems; a method for computing all of them. I: Theory
- Variation of Lyapunov exponents on a strange attractor
- Dynamics in the center manifold of the collinear points of the restricted three-body problem
- Local Lyapunov exponents in chaotic systems
- Celestial mechanics and control of space vehicles
- A lunar exploration architecture using lunar libration point one
- The ?Halo? family of 3-dimensional periodic orbits in the Earth-Moon restricted 3-body problem
- On the Compuation of Lyapunov Exponents for Continuous Dynamical Systems
- On the generalization of a theorem of A. Liapounoff
- Numerical determination of Lissajous trajectories in the restricted three-body problem
- Analytic construction of periodic orbits about the collinear points
- Dynamics and Mission Design Near Libration Points
- High-order expansions of invariant manifolds of libration point orbits with applications to mission design
- Connecting orbits and invariant manifolds in the spatial restricted three-body problem
- Dynamics and Mission Design Near Libration Points
- Introduction to Hamiltonian dynamical systems and the \(N\)-body problem
- Low energy transfer to the Moon
