Pages that link to "Item:Q2656792"
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The following pages link to High-order resonant orbit manifold expansions for mission design in the planar circular restricted 3-body problem (Q2656792):
Displaying 14 items.
- A novel method of periodic orbit computation in circular restricted three-body problem (Q413094) (← links)
- Stretching in phase space and applications in general nonautonomous multi-body problems (Q748254) (← links)
- Using FLI maps for preliminary spacecraft trajectory design in multi-body environments (Q1003189) (← links)
- High-order polynomial continuation method for trajectory design in non-Keplerian environments (Q2052954) (← links)
- Rapid and accurate methods for computing whiskered tori and their manifolds in periodically perturbed planar circular restricted 3-body problems (Q2073335) (← links)
- Fast numerical approximation of invariant manifolds in the circular restricted three-body problem (Q2199529) (← links)
- Transfer design between neighborhoods of planetary moons in the circular restricted three-body problem: the moon-to-moon analytical transfer method (Q2241837) (← links)
- High-order expansions of invariant manifolds of libration point orbits with applications to mission design (Q4651111) (← links)
- Numerical Computation of High-Order Expansions of Invariant Manifolds of High-Dimensional Tori (Q5095751) (← links)
- End-to-end trajectory concept for close exploration of Saturn's inner large moons (Q6058720) (← links)
- Fully numerical computation of heteroclinic connection families in the spatial three-body problem (Q6143078) (← links)
- Computer assisted proofs for transverse collision and near collision orbits in the restricted three body problem (Q6155309) (← links)
- Weighted Birkhoff averages and the parameterization method (Q6598399) (← links)
- Computational methods in perturbation theory (Q6599390) (← links)
