| タイトル | Allowable response delay for large aircraft |
| 著者（英） | Meyer, R. T.; Tingas, S. A.; Grantham, W. D. |
| 著者所属（英） | NASA Langley Research Center|Lockheed-Georgia Co. |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | The degree of permissible time delay in an airliner flight control system is presently sought by means of a pilot-in-the-loop moving base flight simulator, assuming the characteristics of an advanced L-1011 aircraft variant. Test pilots and engineers from the U.S. Navy, the airliner manufacturer, and NASA Langley were used in a task which encompassed approach and landing after recovery from offsets in localizer and glide slope, during calm, turbulent, and cross-wind conditions. The data obtained in the course of 279 runs included statistics on pilot workload and performance as well as pilot opinion. Preliminary results indicate that requirements for a 0.1-sec maximum delay in aircraft response are excessively conservative for large aircraft, where an offset landing maneuver is the critical design task. Lateral axis delays appear to be more critical than longitudinal ones. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 84A43453
AIAA PAPER 84-1917 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/396892 |
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