| タイトル | The 727 approach energy management system avionics specification (preliminary) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770012122 |
| 著者（英） | Lambregts, A. A.; Jackson, D. O. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1976-08-01 |
| 言語 | eng |
| 内容記述 | Hardware and software requirements for an Approach Energy Management System (AEMS) consisting of an airborne digital computer and cockpit displays are presented. The displays provide the pilot with a visual indication of when to manually operate the gear, flaps, and throttles during a delayed flap approach so as to reduce approach time, fuel consumption, and community noise. The AEMS is an independent system that does not interact with other navigation or control systems, and is compatible with manually flown or autopilot coupled approaches. Operational use of the AEMS requires a DME ground station colocated with the flight path reference. |
| NASA分類 | AIRCRAFT INSTRUMENTATION |
| レポートNO | 77N19066
NASA-CR-137906
D6-44119 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/182981 |
