Low-energy transfers to the Moon with long transfer time
From MaRDI portal
Publication:2005589
DOI10.1007/s10569-019-9883-7zbMath1448.70072OpenAlexW2913513990WikidataQ128494579 ScholiaQ128494579MaRDI QIDQ2005589
Francesco Topputo, Tomohiro Yanao, Kenta Oshima
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/s10569-019-9883-7
restricted four-body problemPareto-optimal solutionlunar gravity assistlow-energy transferdirect transcription and multiple shooting
Related Items (4)
Energy analysis of the single impulsive Earth-Moon transfer with the temporary lunar capture ⋮ Transfers from distant retrograde orbits to low lunar orbits ⋮ Spatial unstable periodic quasi-satellite orbits and their applications to spacecraft trajectories ⋮ Transits close to the Lagrangian solutions L 1, L 2 in the elliptic restricted three-body problem
Cites Work
- Unnamed Item
- Optimal capture trajectories using multiple gravity assists
- Novel spaceways for reaching the Moon: An assessment for exploration
- Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time
- Computation of low energy Earth-to-Moon transfers with moderate flight time
- Fast numerical approximation of invariant manifolds in the circular restricted three-body problem
- A Method to Design Efficient Low-Energy, Low-Thrust Transfers to the Moon
- Survey of Numerical Methods for Trajectory Optimization
- Discrete approximations to optimal trajectories using direct transcription and nonlinear programming
- Multiple Gravity Assists, Capture, and Escape in the Restricted Three-Body Problem
- On the dynamics of weak stability boundary lunar transfers
- Low energy transfer to the Moon
This page was built for publication: Low-energy transfers to the Moon with long transfer time
