Optimal Low-Thrust Transfers Between Relative Planar and Spatial Quasi-Satellite Orbits in the Earth–Moon System

This paper investigates the design of optimal low-thrust transfers between relative planar and spatial quasi-satellite orbits (QSOs) in the Earth–Moon system under the Circular Restricted Three-Body Problem (CR3BP). A key contribution is the adaptation of a trajectory optimization framework, previou...

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Bibliographic Details
Published in:Aerospace
Main Authors: Nishanth Pushparaj, Naoki Hiraiwa, Yuta Hayashi, Mai Bando
Format: Article
Language:English
Published: MDPI AG 2025-06-01
Subjects:
CRTBP
periodic orbits
QSO
optimization
Online Access:https://www.mdpi.com/2226-4310/12/6/524

Internet

https://www.mdpi.com/2226-4310/12/6/524

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