| タイトル | Modified independent modal space control method for active control of flexible systems |
| 著者（英） | Baz, A.; Poh, S.; Studer, P. |
| 著者所属（英） | Catholic Univ. of America|NASA Goddard Space Flight Center |
| 発行日 | 1988-01-01 |
| 言語 | eng |
| 内容記述 | A modified independent modal space control (MIMSC) method is developed for designing active vibration control systems for large flexible structures. The method accounts for the interaction between the controlled and residual modes. It incorporates also optimal placement procedures for selecting the optimal locations of the actuators in the structure in order to minimize the structural vibrations as well as the actuation energy. The MIMSC method relies on an important feature which is based on time sharing of a small number of actuators, in the modal space, to control effectively a large number of modes. Numerical examples are presented to illustrate the application of the method to generic flexible systems. The results obtained suggest the potential of the devised method in designing efficient active control systems for large flexible structures. |
| NASA分類 | CYBERNETICS |
| レポートNO | 89A11681 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/367530 |
