| タイトル | Configuration management and automatic control of an augmentor wing aircraft with vectored thrust |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790009701 |
| 著者（英） | Sridhar, B.; Meyer, G.; Cicolani, L. S. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1979-03-01 |
| 言語 | eng |
| 内容記述 | An advanced structure for automatic flight control logic for powered-lift aircraft operating in terminal areas is under investigation at Ames Research Center. This structure is based on acceleration control; acceleration commands are constructed as the sum of acceleration on the reference trajectory and a corrective feedback acceleration to regulate path tracking errors. The central element of the structure, termed a Trimmap, uses a model of the aircraft aerodynamic and engine forces to calculate the control settings required to generate the acceleration commands. This report describes the design criteria for the Trimmap and derives a Trimmap for Ames experimental augmentor wing jet STOL research aircraft. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 79N17872
NASA-TP-1222
A-7099 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/176414 |
