A6 高速マヌーバを受ける非対称柔軟衛星の振動特性
スポンサーリンク
概要
- 論文の詳細を見る
This paper describes dynamic behavior of an asymmetric satellite with flexible appendages under agile maneuvers. Four dynamic models are used, and they differ in the eigen frequencies of the two flexible appendages. The results of the dynamic response simulation show that increasing one appendage rigidity decreases the frequency range of the total system main response.
- 2008-01-24