| タイトル | STOVL Control Integration Program |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950005074 |
| 著者（英） | Watts, S.; Mcdowell, P.; Weiss, C. |
| 著者所属（英） | Pratt and Whitney Aircraft |
| 発行日 | 1994-07-01 |
| 言語 | eng |
| 内容記述 | An integrated flight/propulsion control for an advanced vector thrust supersonic STOVL aircraft, was developed by Pratt & Whitney and McDonnell Douglas Aerospace East. The IFPC design was based upon the partitioning of the global requirements into flight control and propulsion control requirements. To validate the design, aircraft and engine models were also developed for use on a NASA Ames piloted simulator. Different flight control implementations, evaluated for their handling qualities, are documented in the report along with the propulsion control, engine model, and aircraft model. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 95N11487
NASA-CR-195358
E-9023
NAS 1.26:195358 |
| 権利 | No Copyright |
