摘要
A study adopts the disturbance-observer-based control scheme to enhance the flight control performance. This method is known as an active anti-disturbance strategy where the lumped disturbances from various sources are estimated by a disturbance observer (DO) and then incorporated into a nominal controller to compensate for their adverse effects. A preliminary study has demonstrated the disturbance rejection ability of this control strategy on a small-scale helicopter. The study proposes a novel disturbance-observer design that extends the scope of the classical one to a partial-state unmeasurable system.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 2235-2240 |
| 页数 | 6 |
| 期刊 | Journal of Guidance, Control, and Dynamics |
| 卷 | 38 |
| 期 | 11 |
| DOI | |
| 出版状态 | 已出版 - 2015 |
学术指纹
探究 'Flight control design for small-scale helicopter using disturbance- observer-based backstepping' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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