| タイトル | Flexible body stability analysis of Space Shuttle ascent flight control system by using lambda matrix solution techniques |
| 著者（英） | Bown, R. L.; Lardas, M.; Flanders, H.; Christofferson, A. |
| 著者所属（英） | Houston Univ.|Martin Marietta Aerospace|Lockheed Engineering and Management Services Co., Inc. |
| 発行日 | 1980-01-01 |
| 言語 | eng |
| 内容記述 | A lambda matrix solution technique is being developed to perform an open loop frequency analysis of a high order dynamic system. The procedure evaluates the right and left latent vectors corresponding to the respective latent roots. The latent vectors are used to evaluate the partial fraction expansion formulation required to compute the flexible body open loop feedback gains for the Space Shuttle Digital Ascent Flight Control System. The algorithm is in the final stages of development and will be used to insure that the feedback gains meet the design specification. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 80A45906
AIAA PAPER 80-1616 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/420750 |
