| タイトル | An Adaptive Nonlinear Aircraft Maneuvering Envelope Estimation Approach for Online Applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140011464 |
| 著者（英） | Lombaerts, Thomas Jan; Acosta, Diana; Kaneshige, John; Schuet, Stefan R.; Wheeler, Kevin |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2014-01-13 |
| 言語 | eng |
| 内容記述 | A nonlinear aircraft model is presented and used to develop an overall unified robust and adaptive approach to passive trim and maneuverability envelope estimation with uncertainty quantification. The concept of time scale separation makes this method suitable for the online characterization of altered safe maneuvering limitations after impairment. The results can be used to provide pilot feedback and/or be combined with flight planning, trajectory generation, and guidance algorithms to help maintain safe aircraft operations in both nominal and off-nominal scenarios. |
| NASA分類 | Aircraft Stability and Control; Aircraft Design, Testing and Performance |
| レポートNO | ARC-E-DAA-TN11537 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/62944 |
