| タイトル | Initial Flight Evaluation of the Army/NASA RASCAL Variable Stability Helicopter |
| 著者（英） | Hindson, William S.; Moralez, Ernesto, III; Arterburn, David R. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2000-09-18 |
| 言語 | eng |
| 内容記述 | NASA Ames Research Center and the U.S. Army Aeroflightdynamics Directorate (AFDD) [will] have performed initial flight evaluations of the Research Flight Control System (RFCS) that has been integrated into the Army/NASA Rotorcraft Aircrew Systems Concepts Airborne Laboratory (RASCAL) variable stability helicopter. The RASCAL, a highly modified JUH-60A Black Hawk helicopter, is a variable-stability, in-flight simulator that is designed to support flight research programs that leverage on the flight control and handling qualities design tools developed by the Army and NASA. These tools are used in the flight control design life cycle from initial concept definition, through simulation, and ultimately into flight on-board the RASCAL helicopter. The RASCAL will be used to validate methodologies for reducing design cycle costs for new or modified aircraft, and it will serve as a base for the investigation of new rotorcraft technology. |
| NASA分類 | Aircraft Design, Testing and Performance |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/545105 |
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