| タイトル | The 4D-TECS integration for NASA TSRV airplane |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890014100 |
| 著者（英） | Kaminer, I.; Oshaughnessy, P. R. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1989-06-01 |
| 言語 | eng |
| 内容記述 | The integration of the Total Energy Control System (TECS) concept with 4D navigation is described. This integration was made to increase the operational capacity of modern aircraft and encourage incorporation of this increased capability with the evolving National Airspace System (NAS). Described herein is: 4D smoothing, the basic concepts of TECS, the spoiler integration concept, an algorithm for nulling out time error, speed and altitude profile modes, manual spoiler implementation, 4D logic, and the results of linear and nonlinear analysis. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 89N23471
NAS 1.26:4231
NASA-CR-4231 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/142062 |
