Deployment reliability predicition for large satellite antennas driven by spring mechanisms

Author:

Misawa Masayoshi1

Affiliation:

1. NTT Radio Communication Systems Laboratories, Tokyo 104, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 6 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. Reliability model of sequence motions and its solving idea;Ekspolatacja i Niezawodnosc - Maintenance and Reliability;2019-06-20

2. Dynamic Characteristics Verification of Large Space Structures by Component Tests;IFAC Proceedings Volumes;2004-07

3. A Dynamic Characteristics Prediction of Large Satellite Antennas by Component Tests;45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;2004-04-19

4. Sensitivity of the Deployment Repeatability of a Precision Telescope Mechanism;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22

5. Mode selection in stiffness design of deployed satellite antennas;19th AIAA Applied Aerodynamics Conference;2001-06-11

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