| タイトル | A simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath control |
| 著者（英） | Le, Jeanette; Conley, Joseph L.; Burcham, Frank W., Jr.; Gilyard, Glenn B. |
| 著者所属（英） | NASA Dryden Flight Research Facility |
| 発行日 | 1991-06-01 |
| 言語 | eng |
| 内容記述 | The use of throttle control laws to provide adequate flying qualities for flightpath control in the event of a total loss of conventional flight control surface use was evaluated. The results are based on a simulation evaluation by transport research pilots of a B-720 transport with visual display. Throttle augmentation control laws can provide flightpath control capable of landing a transport-type aircraft with up to moderate levels of turbulence. The throttle augmentation mode dramatically improves the pilots' ability to control flightpath for the approach and landing flight condition using only throttle modulation. For light turbulence, the average Cooper-Harper pilot rating improved from unacceptable to acceptable (a pilot rating improvement of 4.5) in going from manual to augmented control. The low frequency response characteristics of the engines require a considerably different piloting technique. The various techniques used by the pilots resulted in considerable scatter in the data. Many pilots readily adapted to a good piloting technique while some has difficulty. The research demonstrates a new and viable approach to providing an independent means of redundancy or increasing the redundancy capability of transport aircraft flightpath control. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 91A44162
AIAA PAPER 91-2223 |
| 権利 | Copyright |
