| タイトル | Flight Test of an L(sub 1) Adaptive Controller on the NASA AirSTAR Flight Test Vehicle |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100033219 |
| 著者（英） | Gregory, Irene M.; Hovakimyan, Naira; Cao, Chengyu; Xargay, Enric |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2010-08-02 |
| 言語 | eng |
| 内容記述 | This paper presents results of a flight test of the L-1 adaptive control architecture designed to directly compensate for significant uncertain cross-coupling in nonlinear systems. The flight test was conducted on the subscale turbine powered Generic Transport Model that is an integral part of the Airborne Subscale Transport Aircraft Research system at the NASA Langley Research Center. The results presented are for piloted tasks performed during the flight test. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | NF1676L-11093 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
