| タイトル | Quasi-optimum design of a six degree of freedom moving base simulator control system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740002186 |
| 著者（英） | Friedland, B.; Hutton, M. F.; Ling, C. |
| 著者所属（英） | Singer Co. |
| 発行日 | 1973-10-01 |
| 言語 | eng |
| 内容記述 | The design of a washout control system for a moving base simulator is treated by a quasi-optimum control technique. The broad objective of the design is to reproduce the sensed motion of a six degree of freedom simulator as accurately as possible without causing the simulator excursions to exceed specified limits. A performance criterion is established that weights magnitude and direction errors in specific force and in angular velocity and attempts to maintain the excursion within set limits by penalizing excessive excursions. A FORTRAN routine for relizing the washout law was developed and typical time histories using the washout routine were simulated for a range of parameters in the penalty- and weighting-functions. These time histories and the listing of the routine are included in the report. |
| NASA分類 | FACILITIES, RESEARCH, AND SUPPORT |
| レポートNO | 74N10299
NASA-CR-2312 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/197053 |
