Low-Thrust Many-Revolution Transfer between Near Rectilinear Halo Orbit and Low Lunar Orbit Using Hybrid Differential Dynamic Programming

Fuente: arXiv

Saved in:

Bibliographic Details
Main Authors:	Oue, Kohei, Ozaki, Naoya, Chujo, Toshihiro
Format:	Preprint
Published:	2025
Subjects:	Earth and Planetary Astrophysics Instrumentation and Methods for Astrophysics Optimization and Control
Online Access:	Acceder al recurso
Tags:	Add Tag No Tags, Be the first to tag this record!

Internet

https://arxiv.org/abs/2504.07723