タイトル | Guidance and control system research for improved terminal area operations |
本文(外部サイト) | http://hdl.handle.net/2060/19810010512 |
著者(英) | Young, J. C.; Hueschen, R. M.; Bundick, W. T.; Creedon, J. F. |
著者所属(英) | Analytical Mechanics Associates, Inc.; Boeing Co.; Information and Control Systems, Inc.; NASA Langley Research Center |
発行日 | 1981-03-01 |
言語 | eng |
内容記述 | Several guidance and control system research and development activities aimed at improving the operational capabilities of commercial aircraft in the terminal area are described. The guidance and control systems were designed to improve the capacity and efficiency of terminal area operations, enhance the approach and landing capability of aircraft in adverse weather conditions, and reduce the impact of aircraft noise perceived on the ground. Specific performance features include the ability to capture and track steep glideslopes, use short final approaches, perform flares with reduced longitudinal touchdown dispersion and execute high speed runway rollout and turnoff. Results obtained from simulation studies or flight tests are shown for each of the algorithms. |
NASA分類 | AIR TRANSPORTATION AND SAFETY |
レポートNO | 81N19038 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/568209 |