Simultaneous and Decentralized Deployment Behavior of Flexible Space Structures.

Author:

Ishimura Kosei,Natori M. C.,Higuchi Ken

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference10 articles.

1. 2) Vaughan, D. H.: Modular Reflector Concept Study, 1981, NASA-CR-3411.

2. 4) Nakamura, K., Tsutsumi, Y., Uchimaru, K., Tsujihata, A. and Meguro, A.: Large Deployable Reflector on ETS-VIII, 17th AIAA Int’l Communications Satellite Systems Conf., Yokohama, 1998, AIAA Paper 98-1229.

3. 5) Chiu, C. W.: The Dynamics of Flexible Solar Array Panel during Deployment Motion, 44th Cong. Int’l Astronautical Fed. (IAF), Graz, Austria, Oct., 1993, ST-93-W.1.854.

Cited by 3 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. Fundamental Design of Tensioned Precision Deployable Space Structures Applied to an X-Band Phased Array;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

2. Effect of Synchronization Errors on Deployment Characteristics of Modularized Structures;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2004

3. Averaging Interaction in the Decentralized Control of Modularized Structures;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

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