Tentative Solutions for Indirect Optimization of Spacecraft Trajectories

DOI10.1007/978-3-319-41508-6_3zbMath1394.70061OpenAlexW2571148372MaRDI QIDQ3133906

Lorenzo Casalino, Guido Colasurdo

Publication date: 8 February 2018

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

Full work available at URL: https://doi.org/10.1007/978-3-319-41508-6_3

zbMATH Keywords

trajectory optimizationoptimal control theoryindirect methods

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Cites Work

• Minimum fuel control of the planar circular restricted three-body problem
• Continuation from a flat to a round Earth model in the coplanar orbit transfer problem
• Survey of Numerical Methods for Trajectory Optimization
• Reformulation of Edelbaum's Low-Thrust Transfer Problem Using Optimal Control Theory
• Indirect Methods for the Optimization of Spacecraft Trajectories
• New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Tentative Solutions for Indirect Optimization of Spacecraft Trajectories