| タイトル | Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140008294 |
| 著者（英） | Leonard, Michael W.; Craun, Robert W.; Acosta, Diana M.; Beard, Steven D.; Weinstein, Michael; Hardy, Gordon H. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2013-08-19 |
| 言語 | eng |
| 内容記述 | In order to advance research in the area of pilot induced oscillations, a reliable method to create PIOs in a simulated environment is necessary. Using a boundary avoidance tracking task, researchers performing an evaluation of control systems were able to create PIO events in 42% of cases using a nominal aircraft, and 91% of cases using an aircraft with reduced actuator rate limits. The simulator evaluation took place in the NASA Ames Vertical Motion Simulator, a high-fidelity motion-based simulation facility. |
| NASA分類 | Aircraft Stability and Control; Aircraft Design, Testing and Performance |
| レポートNO | ARC-E-DAA-TN10073 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/80341 |
