| 某型无人机俯仰角控制回路的控制律设计 |
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| 引用本文： | 苏巧,胡煦芫.某型无人机俯仰角控制回路的控制律设计[J].企业技术开发,2012(25):38-40,46. |
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| 作者姓名： | 苏巧 胡煦芫 |
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| 作者单位： | 中国人民解放军驻206所军代室;空军雷达学院五系 |
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| 摘 要： | 文章以某型无人机为研究对象,利用经典控制理论的知识,分析根轨迹,对无人机的俯仰运动的相关控制律进行了设计,并在SIMULINK软件中进行仿真验证,证明其控制律的有效性、正确性。
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| 关 键 词： | 无人机 控制律设计 仿真 |
Design for the control law of a UAV pitch angle control loop |
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| SU Qiao,HU Xu-yan.Design for the control law of a UAV pitch angle control loop[J].Technological Development of Enterprise,2012(25):38-40,46. |
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| Authors: | SU Qiao HU Xu-yan |
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| Institution: | 1.The Military Representative Office in 206 Institute,Xi’an,Shaanxi 710010,China;2.No.5 Department,Air Force Radar Academy,Wuhan,Hubei 430019,China) |
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| Abstract: | The article sets a UAV as the research object,with the knowledge of classical control theory analyzes the root locus,on the pitch movement of the UAV control law design and simulation in the SIMULINK software,to prove the effectiveness of the control law,correctness. |
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| Keywords: | unmanned aerial vehicles control law design simulation |
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