| 旋翼式微型飞行器升力系统设计 |
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| 引用本文： | 翁梓华,陈智敏.旋翼式微型飞行器升力系统设计[J].厦门大学学报(自然科学版),2004,43(6):802-805. |
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| 作者姓名： | 翁梓华 陈智敏 |
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| 作者单位： | 厦门大学机电工程系,福建,厦门,361005 |
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| 摘 要： | 在综合分析多种微型飞行器升力系统方案的基础上,提出了3种旋翼式微型飞行器的升力系统布局方案.通过对其中的双电动机双旋翼微型飞行器升力系统布局方案进行的实验验证,证明了该升力系统布局方案的可行性.
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| 关 键 词： | 微型飞行器 旋翼 飞行控制 |
| 文章编号： | 0438-0479(2004)06-0802-04 |
| 修稿时间： | 2003年9月12日 |
Design of a Lift System of Rotary-wing Micro Air Vehicle |
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| WENG Zi-hua,CHEN Zhi-min.Design of a Lift System of Rotary-wing Micro Air Vehicle[J].Journal of Xiamen University(Natural Science),2004,43(6):802-805. |
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| Authors: | WENG Zi-hua CHEN Zhi-min |
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| Abstract: | In the paper,three kinds of the Lift System layout scheme of rotary-wing Micro Air Vehicle are proposed based on combining analysis of several kinds of Micro Air Vehicle.The Lift System layout scheme of rotary-wing Micro Air Vehicle of double-engine and double-rotor is designed and chosen to produce in the lab.And the test results have proved that the Lift System layout scheme of Micro Air Vehicle is feasibility. |
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| Keywords: | Micro Air Vehicle rotor flight control |
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