| タイトル | Variable-Structure Control of a Model Glider Airplane |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090011278 |
| 著者（英） | Anderson, Mark R.; Waszak, Martin R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2008-07-01 |
| 言語 | eng |
| 内容記述 | A variable-structure control system designed to enable a fuselage-heavy airplane to recover from spin has been demonstrated in a hand-launched, instrumented model glider airplane. Variable-structure control is a high-speed switching feedback control technique that has been developed for control of nonlinear dynamic systems. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | LAR-17106-1 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
