Dynamic analysis of lunar lander during soft landing using explicit finite element method-Reference-Cited by-同舟云学术

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Dynamic analysis of lunar lander during soft landing using explicit finite element method

Published:2018-07 Issue: Volume:148 Page:69-81
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zheng Guang,Nie Hong,Chen Jinbao,Chen Chuanzhi,Lee Heow Pueh^ORCID

Funder

The Innovation Planning Foundation of Graduate Student in Jiangsu Province

Nanjing University of Aeronautics and Astronautics

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. Apollo Experience Report - Lunar Module Landing Gear Subsystem;Rogers,1972

2. Dynamic Model Investigation of Touchdown Stability of Lunar-landing Vehicles;Herr,1967

3. Overview of lunar lander soft landing dynamic modeling and analysis;Dongping;Spacecraft Eng.,2011

4. Landing Buffer Mechanism of Spacecraft;Jiangzhon,2015

5. Modeling and simulation of lunar lander soft-landing using transient dynamics approach;Wan,2010

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