| 倾转旋翼机悬停建模与实验 |
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| 引用本文： | 邹灿东,王维军,屈香菊.倾转旋翼机悬停建模与实验[J].飞行力学,2010,28(1). |
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| 作者姓名： | 邹灿东 王维军 屈香菊 |
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| 作者单位： | 北京航空航天大学航空科学与工程学院,北京,100191 |
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| 摘 要： | 以自行设计的倾转旋翼机为研究对象,建立悬停模式下纵向动力学模型。通过悬停实验,对倾转旋翼机的分系统——舵机模型、旋翼气动力模型和悬停纵向模型进行了仿真验证。结果表明,模型能反映倾转旋翼机悬停模式的基本特性,可为飞行控制系统设计提供依据。
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| 关 键 词： | 倾转旋翼 悬停模式 纵向模型 |
Modeling and experiment of tilt-rotor aircraft in hover mode |
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| ZOU Can-dong,WANG Wei-jun,QU Xiang-ju.Modeling and experiment of tilt-rotor aircraft in hover mode[J].Flight Dynamics,2010,28(1). |
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| Authors: | ZOU Can-dong WANG Wei-jun QU Xiang-ju |
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| Institution: | College of Aeronautic Science and Engineering;BUAA;Beijing 100191;China |
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| Abstract: | The longitudinal dynamics model a tilt-rotor aircraft prototype was founded.The hovering experiment was designed and carried on to validate the actuator and rotor models,The results show that these models can perform basic characteristics of the hover mode and are valuable for flight control system design. |
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| Keywords: | tilt-rotor aircraft hover mode longitudinal model |
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