| 基于DWILS的无人机着陆导引与控制仿真 |
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| 引用本文： | 王鹏,马松辉,段晓军,陈怀民.基于DWILS的无人机着陆导引与控制仿真[J].计算机仿真,2010,27(1):110-113. |
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| 作者姓名： | 王鹏 马松辉 段晓军 陈怀民 |
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| 作者单位： | 西北工业大学无人机特种技术围防科技重点实验窒,陕西,西安,710065 |
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| 摘 要： | 导引和控制技术是大型无人机实现自动着陆的两项关键技术。针对分米波仪表着陆系统（DWILS）的无人机着陆导引与控制技术的仿真验证,为了提高导引的可靠性,给出了基于DWILS的无人机着陆地面仿真系统的结构,着陆导引仿真设备,根据DWILS的工作原理给出了导引信号的计算公式,同时设计了着陆控制器。根据导引设备的原理建立了基于DWILS的无人机着陆导引与控制仿真系统模型,并进行仿真验证。仿真结果表明,基于DWILS的导引方式满足无人机着陆导引的需要,设计的着陆控制器具有较好的控制效果。
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| 关 键 词： | 无人机 分米波仪表着陆系统 着陆导引 飞行仿真 |
Simulation of Landing Guidance and Control for UAV Guided by Decimeter Wave Instrument Landing System |
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| WANG Peng,MA Song-hui,DUAN Xiao-jun,CHEN Huai-min.Simulation of Landing Guidance and Control for UAV Guided by Decimeter Wave Instrument Landing System[J].Computer Simulation,2010,27(1):110-113. |
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| Authors: | WANG Peng MA Song-hui DUAN Xiao-jun CHEN Huai-min |
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| Affiliation: | National Key Laboratory of Special Science and Technology on UAV/a>;Northwestern Polytechnical University/a>;Xi'an Shanxi 710065/a>;China |
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| Abstract: | Guidance and control are two key technologies of automatic landing for large UAVs.Decimeter wave instrument landing system(DWILS) is a method may be used in guidance for UAV during landing.How to testify the DWILS based landing guidance and control technologies in laboratory is studied in this paper.Firstly the architecture of a hardware-in-loop simulation system is given to testify the feasibility of DWILS for UAV landing guidance.Secondly,the simulator of guidance signal and calculation of guidance signal... |
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| Keywords: | UAV Decimeter wave instrument landing system(DWILS) Landing guidance Flight simulation |
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