Minimum-Fuel Trajectories and Near-Optimal Explicit Guidance for Pinpoint Landing from Low Lunar Orbit

This research addresses minimum-fuel pinpoint lunar landing at the South Pole, focusing on trajectory design and near-optimal guidance aimed at driving a spacecraft from a circular low lunar orbit (LLO) to an instantaneous hovering state above the lunar surface. Orbit dynamics is propagated in a hig...

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Bibliografische Detailangaben

Hauptverfasser:	Matteo Caruso, Giulio De Angelis, Edoardo Maria Leonardi, Mauro Pontani
Format:	Artigo
Sprache:	Inglês
Veröffentlicht:	MDPI AG 2025-02-01
Schriftenreihe:	Aerospace
Schlagworte:	minimum-fuel lunar descent pinpoint landing near-optimal explicit guidance low lunar orbit Lambert-based trajectory optimization powered descent guidance
Online-Zugang:	https://www.mdpi.com/2226-4310/12/3/183
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