[D-5] Orbital Dynamics 2

[2022-d-21] A Dynamics-leveraging Guidance and Control Architecture for Autonomous Rendezvous and Docking in the Restricted Three-Body Problem

*Sergio Cuevas del Valle¹, Hodei Urrutxua Cereijo¹, Pablo Solano López¹ (1. Aerospace Systems and Transport Research Group (GISAT-ASTRG) | Universidad Rey Juan Carlos)

キーワード：GNC, Restricted Three-Body Problem, Rendezvous, Relative Dynamics, Manifolds