| タイトル | MAST flight system dynamic performance |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870006599 |
| 著者（英） | Otten, T.; Davis, L.; Ham, F.; Hyland, D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1986-11-01 |
| 言語 | eng |
| 内容記述 | The MAST Flight System as a test bed for large space structure control algorithms is discussed. An overview is given of the control system architecture. The actuators, the sensors, the control computer, and the baseline damping algorithm are discussed. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 87N16032 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/152408 |
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