The use of vertical instability of \(L_1\) and \(L_2\) planar Lyapunov orbits for transfers from near rectilinear halo orbits to planar distant retrograde orbits in the Earth-Moon system
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Publication:2005608
DOI10.1007/S10569-019-9892-6zbMath1451.70051OpenAlexW2922210590MaRDI QIDQ2005608
Publication date: 8 October 2020
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-019-9892-6
optimizationcircular restricted three-body problemvertical instabilitynear rectilinear halo orbitsplanar distant retrograde orbitsplanar Lyapunov orbits
Related Items (3)
Transfers from distant retrograde orbits to low lunar orbits ⋮ Linking low- to high-energy dynamics of invariant manifolds, transit orbits, and singular collision orbits in the planar circular restricted three-body problem ⋮ Low-thrust transfers to southern \(L_2\) near-rectilinear halo orbits facilitated by invariant manifolds
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