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trajectory-design

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Bishwaswarup / cr3bp-manifoldtransfer

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Low-energy Earth–Moon transfer design via invariant manifolds of CR3BP halo orbits. Differential correction, pseudo-arclength continuation, Poincaré section intersection search, and ΔV budget. Python + LaTeX paper.

python astrodynamics scientific-computing orbital-mechanics three-body-problem cr3bp halo-orbits trajectory-design space-mission-design earth-moon-system poincare-section invariant-manifolds low-energy-transfer
  • Updated Aug 23, 2026
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