| 基于Simulink的无人机六自由度仿真 |
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| 引用本文： | 李文强,彭学锋,郑志强. 基于Simulink的无人机六自由度仿真[J]. 系统仿真学报, 2007, 19(19): 4604-4606 |
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| 作者姓名： | 李文强 彭学锋 郑志强 |
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| 作者单位： | 国防科大机电工程与自动化学院,湖南,长沙,410073 |
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| 摘 要： | 加装滑翔增程组件的炸弹气动外形和无人机类似,研究无人机的运动特性将对研究滑翔增程组件起到重要作用。利用Simulink对无人机进行六自由度建模,分析无人机在滑翔过程当中的运动姿态特性,副翼对无人机运动的影响,无人机在风干扰的环境中的运动姿态特性,通过这些分析,可以对炸弹的滑翔增程组件的设计起到至关重要的作用,可为后续的控制、制导、导航研究打下基础。
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| 关 键 词： | 滑翔增程 无人机 六自度 副翼 |
| 文章编号： | 1004-731X（2007）19-4604-03 |
| 收稿时间： | 2006-08-09 |
| 修稿时间： | 2007-01-25 |
UAV 6 DOF Simulation Based on Simulink |
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| LI Wen-qiang,PENG Xue-feng,ZHENG Zhi-qiang. UAV 6 DOF Simulation Based on Simulink[J]. Journal of System Simulation, 2007, 19(19): 4604-4606 |
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| Authors: | LI Wen-qiang PENG Xue-feng ZHENG Zhi-qiang |
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| Affiliation: | School of Mechatronics and Automation,National University of Defense Technology, Changsha 410073, China |
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| Abstract: | It is true that researching kinetic characteristic of UAV can help researching gliding extended range module,because the ammunition with gliding extended range module has similar aerodynamic configuration to UAV. The six DOF of UAV was modeled using Simulink,and the kinetic attitude characteristic of UAV was analyzed when gliding,and the impact of aileron was analyzed,and the kinetic attitude characteristic of UAV was analyzed which was in wind interference environment. The gliding extended range module could be designed with these analyses,which benefited the later research of control,guidance and navigation. |
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| Keywords: | Simulink |
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