Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control-Reference-Cited by-同舟云学术

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Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control

Published:2023-11 Issue: Volume:212 Page:672-685
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Pontani Mauro^ORCID,Celani Fabio^ORCID,Carletta Stefano

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Apollo Guidance, Navigation and Control: Apollo Lunar Descent Guidance;Klumpp,1971

2. E-Guidance – A General Explicit, Optimizing Guidance Law for Rocket-Propelled Spacecraft;Cherry,1964

3. "Revisiting Apollo: Lunar Landing Guidance,";Nemeth,2006

4. Enhanced apollo-class real-time targeting and guidance for powered descent and precision landing;Azimov,2013

5. Analytical lunar descent guidance algorithm;Chomel;J. Guid. Control Dynam.,2009

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Trajectory/propulsion integrated design optimization of the manned lunar lander propelled by hybrid rocket motors using analytical target cascading;Acta Astronautica;2024-09

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