Study on Landing Response Control of Planetary Exploration Spacecraft Based on Momentum Exchange Principles-Reference-Cited by-同舟云学术

Study on Landing Response Control of Planetary Exploration Spacecraft Based on Momentum Exchange Principles

Published:2012 Issue:792 Volume:78 Page:2781-2796
ISSN:0387-5024
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series C
language:en
Short-container-title:Trans.JSME(C)

Author:

HARA Susumu¹,WATANABE Tsubasa,KUSHIDA Yohei,OTSUKI Masatsugu,YAMADA Yoji,MATSUHISA Hiroshi,YAMADA Keisuke,HASHIMOTO Tatsuaki,KUBOTA Takashi

Affiliation:

1. Nagoya Univ. Dept. of Mechanical Science and Engineering, Graduate School of Engineering

Publisher

Japan Society of Mechanical Engineers

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials

Link

https://www.jstage.jst.go.jp/article/kikaic/78/792/78_2781/_pdf

Reference15 articles.

1. (1) Rogers, W. F., “Apollo Experience Report - Lunar Module Landing Gear Subsystem”, Technical Report TN D-6850, NASA (1972), pp. 6-21.

2. (5) Cadogan, D., Sandy, C. and Grahne, M., “Development and Evaluation of the Mars Pathfinder Inflatable Airbag Landing System”, Acta Astronautica, Vol. 50, No. 10 (2002), pp. 633-640.

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