| タイトル | A Feasibility Study on the Control of a Generic Air Vehicle Using Control Moment Gyros |
| 本文（外部サイト） | http://hdl.handle.net/2060/20060047569 |
| 著者（英） | Moerder, Daniel D.; Lim, Kyong B. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2006-01-01 |
| 言語 | eng |
| 内容記述 | This paper examines feasibility and performance issues in using Control Moment Gyroscopes (CMGs) to control the attitude of a fixed-wing aircraft. The paper describes a control system structure that permits allocating control authority and bandwidth between a CMG system and conventional aerodynamic control surfaces to stabilize a vehicle with neutral aerodynamic stability. A simulation study explores the interplay between aerodynamic and CMG effects, and indicates desirable physical characteristics for a CMG system to be used for aircraft attitude control. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | AIAA Paper 2006-6313 |
| 権利 | No Copyright |
