Momentum-Exchange-Impact-Damper-Based Shock Response Control for Planetary Exploration Spacecraft
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
2. Nagoya University, Nagoya 464-8603, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.53786
Reference20 articles.
1. Lunar surface mechanical properties at the landing site of Surveyor 3
2. Lunar surface mechanical properties-Surveyor 1
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