| タイトル | Design and Testing of Flight Control Laws on the RASCAL Research Helicopter |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030107257 |
| 著者（英） | Dryfoos, James B.; Hindson, William S.; Moralez. Ernesto, III; Tucker, George E.; Frost, Chad R. |
| 著者所属（英） | Army Aviation Systems Command |
| 発行日 | 2001-12-20 |
| 言語 | eng |
| 内容記述 | Two unique sets of flight control laws were designed, tested and flown on the Army/NASA Rotorcraft Aircrew Systems Concepts Airborne Laboratory (RASCAL) JUH-60A Black Hawk helicopter. The first set of control laws used a simple rate feedback scheme, intended to facilitate the first flight and subsequent flight qualification of the RASCAL research flight control system. The second set of control laws comprised a more sophisticated model-following architecture. Both sets of flight control laws were developed and tested extensively using desktop-to-flight modeling, analysis, and simulation tools. Flight test data matched the model predicted responses well, providing both evidence and confidence that future flight control development for RASCAL will be efficient and accurate. |
| NASA分類 | Aircraft Design, Testing and Performance |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/222952 |
