| 某型无人机飞控系统设计与实现 |
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| 引用本文： | 姜杨,薛艳峰,陈剑涛.某型无人机飞控系统设计与实现[J].计算机测量与控制,2009,17(5). |
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| 作者姓名： | 姜杨 薛艳峰 陈剑涛 |
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| 作者单位： | 中国人民解放军92419部队,辽宁,兴城,125106 |
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| 摘 要： | 某型无人机数字式飞控系统是以高性能PC104计算机为核心的,其控制方式有时间程序控制、遥控指令控制和按预先装订的航路实现三维自主飞行控制3种方式,以3维自主飞行方式为主;为了确保无人机在不受遥控的状态下安全坠毁,设计了无人机飞行安全控制系统;通过计算GPS数据来判断无人机是否超出安全区域,进而控制舵机离合器电源以实现安全控制功能;设计了用于验证该系统的仿真系统,通过仿真结果,验证系统的可行、正确.
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| 关 键 词： | 无人机 飞控系统 仿真 |
Design and Implementation of the UAV Flight Control System |
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| Jiang Yang,Xue Yanfeng,Chen Jiantao.Design and Implementation of the UAV Flight Control System[J].Computer Measurement & Control,2009,17(5). |
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| Authors: | Jiang Yang Xue Yanfeng Chen Jiantao |
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| Affiliation: | 92419 Unit of PLA;Xingcheng 125106;China |
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| Abstract: | The hardware of the UAV flight control system is a digital system,which is based on PC104. It has three control modes,including time program control,remote-control command control and according to beforehand bound airway achieve tridimensional freedom flight control,which give priority to tridimensional freedom flight control. A flight safe control system for UAV is introduced, to prang UAV reliably and safely when it is not under the remote control. Applying GPS data to calculate whether UAV surpasses the ... |
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| Keywords: | UAV flight control system simulation |
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