| タイトル | Application of the concept of dynamic trim control to automatic landing of carrier aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800010849 |
| 著者（英） | Meyer, G.; Smith, G. A. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1980-04-01 |
| 言語 | eng |
| 内容記述 | The results of a simulation study of an alternative design concept for an automatic landing control system are presented. The alternative design concept for an automatic landing control system is described. The design concept is the total aircraft flight control system (TAFCOS). TAFCOS is an open loop, feed forward system that commands the proper instantaneous thrust, angle of attack, and roll angle to achieve the forces required to follow the desired trajector. These dynamic trim conditions are determined by an inversion of the aircraft nonlinear force characteristics. The concept was applied to an A-7E aircraft approaching an aircraft carrier. The implementation details with an airborne digital computer are discussed. The automatic carrier landing situation is described. The simulation results are presented for a carrier approach with atmospheric disturbances, an approach with no disturbances, and for tailwind and headwind gusts. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 80N19126
NASA-TP-1512
A-7801 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173152 |
