| 基于直接力控制的无人机抗侧风着陆研究 |
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| 引用本文： | 李继广,董彦非.基于直接力控制的无人机抗侧风着陆研究[J].指挥控制与仿真,2014,36(2):44-47. |
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| 作者姓名： | 李继广 董彦非 |
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| 作者单位： | 南昌航空大学,南昌航空航天大学飞行器工程学院 |
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| 基金项目： | 某国防预研基金资助项目 |
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| 摘 要： | 摘 要：分析了无人机采用大展弦比、短机身、小垂尾的气动布局对着陆和操纵性的影响。建立了侧风存在时的无人机横向着陆模型；依据主动控制思想，提出了前垂直鸭翼和方向舵组合的直接力控制无人机抗侧风着陆的方案，并通过仿真实验验证了该方法的有效性。
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| 关 键 词： | 气动特性 侧风着陆 直接力控制 |
Counteracting Sidewind Control System By Directforce Control For UAV Landing |
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| lijiguang and dong yan fei.Counteracting Sidewind Control System By Directforce Control For UAV Landing[J].Command Control & Simulation,2014,36(2):44-47. |
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| Authors: | lijiguang and dong yan fei |
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| Institution: | School of Aircraft Engineering, NanChang HangKong University,,College of Aircraft Engineering of Nanchang hangkong University |
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| Abstract: | Abstract:This paper analyzes the large aspect ratio , small tail , short body aerodynamic layout of unmanned aircraft to the landing and maneuverability impact . Established a model of crosswind landing UAV . Based on Active control ideas ,a scheme of vertical front canards and rudder combination of direct control of the UAV force anti crosswind landing was put forward. And the simulation results show the effectiveness of this method. |
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| Keywords: | Aerodynamic Characteristics Crosswind Landings Directforce Control |
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