| 引用本文: | 樊鹏辉,王新华,蔡开元.可垂直起降、高速前飞的飞行器设计与控制[J].控制理论与应用,2010,27(9):1171~1177.[点击复制] |
| FAN Peng-hui,WANG Xin-hua,CAI Kai-yuan.Design and control of aircraft of vertical take-off-and-landing and high-speed forward flight[J].Control Theory and Technology,2010,27(9):1171~1177.[点击复制] |
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| 可垂直起降、高速前飞的飞行器设计与控制 |
| Design and control of aircraft of vertical take-off-and-landing and high-speed forward flight |
| 摘要点击 2695 全文点击 2087 投稿时间：2009-04-16 修订日期：2009-10-13 |
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| DOI编号 10.7641/j.issn.1000-8152.2010.9.CCTA090443 |
| 2010,27(9):1171-1177 |
| 中文关键词 垂直起降 高速前飞 模态转换 四轴飞行器 固定翼 |
| 英文关键词 VTOL high-speed forward flight flight-mode transition four-rotor aircraft fixed-wings |
| 基金项目 国家自然科学基金资助项目(60774008). |
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| 中文摘要 |
| 本文设计了一种具有垂直起降、悬停和高速前飞能力的飞行器. 这种飞行器通过模态转换, 既能够实现类似传统四轴飞行器的垂直起降, 又能够实现类似固定翼飞行器的高速前飞. 同时本文针对这种飞行器设计了模态转换控制律; 仿真试验验证了设计方案和控制律的有效性. |
| 英文摘要 |
| We design a new aircraft with the ability of vertical take-off-and-landing(VTOL), like a four-rotor aircraft; and the ability of flying forward with high speed, like an aircraft with fixed-wings. The flight-mode transition from hovering to forward flight and the reverse process are achieved. A flight-mode transition control law is designed. Both the designscheme and the proposed control law are verified by simulation. |