| タイトル | Integrated Autopilot/Autothrottle Based on a Total Energy Control Concept: Design and Evaluation of Additional Autopilot Modes |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880010924 |
| 著者（英） | Bruce, Kevin R. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1988-04-01 |
| 言語 | eng |
| 内容記述 | An integrated autopilot/autothrottle system was designed using a total energy control design philosophy. This design ensures that the system can differentiate between maneuvers requiring a change in thrust to accomplish a net energy change, and those maneuvers which only require elevator control to redistribute energy. The system design, the development of the system, and a summary of simulation results are defined. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 88N20308
NAS 1.26:4131
NASA-CR-4131 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146775 |
