| タイトル | Description and theory of operation of the computer by-pass system for the NASA F-8 digital fly-by-wire control system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780014133 |
| 著者所属（英） | Sperry Flight Systems |
| 発行日 | 1978-05-01 |
| 言語 | eng |
| 内容記述 | A triplex digital flight control system was installed in a NASA F-8C airplane to provide fail operate, full authority control. The triplex digital computers and interface circuitry process the pilot commands and aircraft motion feedback parameters according to the selected control laws, and they output the surface commands as an analog signal to the servoelectronics for position control of the aircraft's power actuators. The system and theory of operation of the computer by pass and servoelectronics are described and an automated ground test for each axis is included. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 78N22076
NASA-CR-144865 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/179097 |
