Optimization of Low-Energy Transfers

DOI10.1007/978-1-4614-4469-5_16zbMath1365.70038OpenAlexW2179559621MaRDI QIDQ5270076

Edward A. Belbruno, Francesco Topputo

Publication date: 29 June 2017

Published in: Springer Optimization and Its Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-1-4614-4469-5_16

zbMATH Keywords

ballistic capturetrajectory optimizationlow-thrust propulsionlow-energy transfers

Mathematics Subject Classification ID

Three-body problems (70F07) Control of mechanical systems (70Q05) Celestial mechanics (70F15) Orbital mechanics (70M20) Discrete approximations in optimal control (49M25)

Related Items (2)

Optimal round trip lunar missions based on the patched-conic approximation ⋮ Minimum fuel trajectories for round trip lunar missions

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• Earth-Mars transfers with ballistic escape and low-thrust capture
• Efficient invariant-manifold, low-thrust planar trajectories to the Moon
• Low-energy, low-thrust transfers to the Moon
• Direct and indirect methods for trajectory optimization
• Study of the transfer from the Earth to a halo orbit around the equilibrium point \(L_ 1\)
• Sun-perturbed Earth-to-Moon transfers with low energy and moderate flight time
• Dynamics in the center manifold of the collinear points of the restricted three-body problem
• Survey of Numerical Methods for Trajectory Optimization
• Discrete approximations to optimal trajectories using direct transcription and nonlinear programming
• Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
• The dynamics around the collinear equilibrium points of the RTBP
• Low energy transfer to the Moon

This page was built for publication: Optimization of Low-Energy Transfers