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...

Täydet tiedot

Bibliografiset tiedot

Päätekijät:	Matteo Caruso, Giulio De Angelis, Edoardo Maria Leonardi, Mauro Pontani
Aineistotyyppi:	Artigo
Kieli:	Inglês
Julkaistu:	MDPI AG 2025-02-01
Sarja:	Aerospace
Aiheet:	minimum-fuel lunar descent pinpoint landing near-optimal explicit guidance low lunar orbit Lambert-based trajectory optimization powered descent guidance
Linkit:	https://www.mdpi.com/2226-4310/12/3/183
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