| タイトル | F-8 DFBW sensor failure identification using analytic redundancy |
| 著者（英） | Deyst, J. J.; Deckert, J. C.; Willsky, A. S.; Desai, M. N. |
| 著者所属（英） | Massachusetts Inst. of Tech.|Draper (Charles Stark) Lab., Inc. |
| 発行日 | 1977-10-01 |
| 言語 | eng |
| 内容記述 | The structure of a sensor failure detection and identification system designed for the NASA F-8 DFBW aircraft is outlined. The system is for use in a dual-redundant environment, and it takes maximal advantage of all functional relationships among the sensed variables. The identification logic uses the quality sequential probability ratio, which provides a useful on-line measure of confidence in the various forms of analytic redundancy. Preliminary simulation results indicate good behavior of the analytic decision statistic, based on the sequential probability ratio test. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 78A12362 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/434896 |
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