| タイトル | Sensitivity of Space Station Alpha Joint robust controller to structural modal parameter variations |
| 著者（英） | Cooper, Paul A.; Lim, Tae W.; Kumar, Renjith R. |
| 著者所属（英） | Lockheed Engineering and Sciences Co.|NASA Langley Research Center|Analytical Mechanics Associates, Inc. |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | The baseline design of the photovoltaic-array sun-tracking control system is presented with special attention given to the optimization of design variables related to stability and performance. The procedures utilized to attenuate control/structure interaction are described, and controller sensitivity to variations in structural modal parameters is examined. Constrained optimization techniques determine the stability margin and tracking capability, which are then tested for sensitivity to variations in natural frequency, mode-shape amplitudes, and modal-damping ratios. The effect of variations in the modal parameters of the dominant modes on performance indicators is also examined to optimize tracking-performance responsiveness and satisfy the design requirements. It is concluded that accurate on-orbit modal data are necessary to make the reoptimization procedure effective in improving the performance of the control system. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 91A49636
AIAA PAPER 91-2665 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/346167 |
