抄録
Deployment behavior of modularized structures is numerically analyzed from the viewpoint of synchronism. Elastic panels with single and double accordion folding patterns are examined as examples of modularized structures. Through computer simulations, it is shown that asynchronous deployments are caused by inertia forces. To improve the synchronism of the deployment, autonomous distributed control method is proposed. Control rules are driven based on equations of heat conduction and wave propagation. It is confirmed that simple autonomous distributed control can improve the synchronism of the deployment.
| 本文言語 | English |
|---|---|
| ページ（範囲） | 425-432 |
| ページ数 | 8 |
| ジャーナル | American Society of Mechanical Engineers, Aerospace Division (Publication) AD |
| 巻 | 60 |
| 出版ステータス | Published - 2000 12月 1 |
| 外部発表 | はい |
ASJC Scopus subject areas
- 機械工学
- 宇宙惑星科学