| タイトル | Attitude Control for an Aero-Vehicle Using Vector Thrusting and Variable Speed Control Moment Gyros |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050232878 |
| 著者（英） | Lim, K. B.; Moerder, D. D.; Shin, Jong-Yeob |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2005-01-01 |
| 言語 | eng |
| 内容記述 | Stabilization of passively unstable thrust-levitated vehicles can require significant control inputs. Although thrust vectoring is a straightforward choice for realizing these inputs, this may lead to difficulties discussed in the paper. This paper examines supplementing thrust vectoring with Variable-Speed Control Moment Gyroscopes (VSCMGs). The paper describes how to allocate VSCMGs and the vectored thrust mechanism for attitude stabilization in frequency domain and also shows trade-off between vectored thrust and VSCMGs. Using an H2 control synthesis methodology in LMI optimization, a feedback control law is designed for a thrust-levitated research vehicle and is simulated with the full nonlinear model. It is demonstrated that VSCMGs can reduce the use of vectored thrust variation for stabilizing the hovering platform in the presence of strong wind gusts. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | AIAA Paper 2005-5972 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
