| タイトル | Impact of magnetic isolation on pointing system performance in the presence of structural flexibility |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850018550 |
| 著者（英） | Seller, J. |
| 著者所属（英） | Sperry Corp. |
| 発行日 | 1985-02-01 |
| 言語 | eng |
| 内容記述 | The inertial pointing stability of a gimbal pointing system (AGS) was compared with a magnetic pointing/gimbal followup system (ASPS), under certain conditions of system structural flexibility and disturbance inputs from the gimbal support structure. Separate 3 degree-of-freedom (3DOF) linear models based on NASTRAN modal flexibility data for the gimbal and support structures were generated for the ASPS configurations. Using the models inertial pointing control loops providing 6dB of gain margin and 45 deg of phase margin were defined for each configuration. The pointing loop bandwidth obtained for the ASPS is more than twice the level achieved for the AGS configuration. The AGS limit is attributed to the gimbal and support structure flexibility. As a result of the higher ASPS pointing loop bandwidth and the disturbance rejection provided by the magnetic isolation ASPS pointing performane is significantly better than that of the AGS system. The low frequency peak of the ASPS transfer function from base disturbance to payload angular motion is almost 60dB lower than AGS low frequency peak. |
| NASA分類 | SPACECRAFT INSTRUMENTATION |
| レポートNO | 85N26861
NASA-CR-172481
NAS 1.26:172481 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/156399 |
