次世代展開アンテナ構造の解析手法の研究

Material type: 文書・図像類

Author: 西元, 美希ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-20

Material Format: Digital

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Note (General)：: A method of a structural design has been presented to realize an ultra lightweight deployable antenna structure for next generation communication sate...

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Material Type: 文書・図像類
Title: 次世代展開アンテナ構造の解析手法の研究
Author/Editor: 西元, 美希
武市, 昇
下田, 孝幸
小澤, 悟
新舘, 恭嗣
Nishimoto, Miki
Takeichi, Noboru
Shimoda, Takayuki
Ozawa, Satoru
Shintate, Kyoji
Author Heading: 西元, 美希
武市, 昇
下田, 孝幸
小澤, 悟
新舘, 恭嗣
Nishimoto, Miki
Takeichi, Noboru
Shimoda, Takayuki
Ozawa, Satoru
Shintate, Kyoji
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-20
Publication Date (W3CDTF): 2006-01-20
Alternative Title: Buckling mode injection algorithm and its implementation for an ultra-light large deployable antenna
Periodical title: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems
No. or year of volume/issue: JAXA-SP-05-008
Volume: JAXA-SP-05-008
Pages: 25-30
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: アンテナ設計
展開アンテナ
構造設計
大型宇宙構造物
通信衛星
軽量化
数学モデル
計算機プログラム
antenna design
deployable antenna
structural design
large space structure
communication satellite
weight reduction
mathematical model
computer program
Target Audience: 一般
Note (General): A method of a structural design has been presented to realize an ultra lightweight deployable antenna structure for next generation communication satellites. To materialize this method in actual designing, it is necessary to identify the structure's buckling mode correctly in advance, and a flexible multibody analysis program is required. A buckling mode injection algorithm has been presented for the buckling mode identification in a previous study. We have added this algorithm to SPADE, which is a program to analyze flexible multibody systems, and has been developed for analyzing deployable structures. This enables a correct identification of the buckling mode of an arbitrary flexible multibody structure, which ensures the designing of an ultra lightweight deployable antenna structure.
資料番号: AA0049054006
レポート番号: JAXA-SP-05-008
Access Restrictions: 限定公開
Periodical Title (NCID): AA11984031
https://ci.nii.ac.jp/ncid/AA11984031
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ