| タイトル | Flight testing and simulation of an F-15 airplane using throttles for flight control |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920023620 |
| 著者（英） | Wolf, Thomas; Burcham, Frank W., Jr.; Maine, Trindel |
| 著者所属（英） | NASA Dryden Flight Research Facility |
| 発行日 | 1992-08-01 |
| 言語 | eng |
| 内容記述 | Flight tests and simulation studies using the throttles of an F-15 airplane for emergency flight control have been conducted at the NASA Dryden Flight Research Facility. The airplane and the simulation are capable of extended up-and-away flight, using only throttles for flight path control. Initial simulation results showed that runway landings using manual throttles-only control were difficult, but possible with practice. Manual approaches flown in the airplane were much more difficult, indicating a significant discrepancy between flight and simulation. Analysis of flight data and development of improved simulation models that resolve the discrepancy are discussed. An augmented throttle-only control system that controls bank angle and flight path with appropriate feedback parameters has also been developed, evaluated in simulations, and is planned for flight in the F-15. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 92N32864
H-1826
AIAA PAPER 92-4109
NAS 1.15:104255
NASA-TM-104255 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/126163 |
