| 基于Labview的遥控无人机操控测试系统 |
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| 引用本文： | 张昆,张铁民,廖贻泳,庄晓霖,李晟华,兰玉彬.基于Labview的遥控无人机操控测试系统[J].农业工程学报,2015,31(Z2):11-16. |
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| 作者姓名： | 张昆 张铁民 廖贻泳 庄晓霖 李晟华 兰玉彬 |
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| 作者单位： | 华南农业大学工程学院, 广州 510642,华南农业大学工程学院, 广州 510642,华南农业大学工程学院, 广州 510642,华南农业大学工程学院, 广州 510642,华南农业大学工程学院, 广州 510642,华南农业大学工程学院, 广州 510642 |
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| 基金项目： | 863 High Technology Research and Development Program(SS2013AA100303) and the State Key Labs of Robotics(RL2012-O02). |
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| 摘 要： | 该系统利用航姿参考系统IG-500N采集无人机实时飞行状态信息,通过无线数传模块传输至地面PC机。飞行状态信息包括:三轴姿态角、三轴加速度、三轴角速度、三轴速度、GPS经纬度、GPS海拔高度、温度和气压等信息。之后利用Labview设计的程序分割提取各个测试项目所对应的数据信息,并计算对应测试项目的用时、位置偏差和姿态稳定行,进而得到遥控无人机操控水平指标,导入生成测试报告。用于评估操控手在操控无人机起飞、航线飞行、定点悬停和降落过程中的操控水平。试验结果表明测试系统可靠。该研究可用于为无人机操控手的水平评估和自主飞行无人机的飞行性能优化提供参考。
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| 关 键 词： | 无人机 遥感 设计 飞行状态 操控水平 测试系统 Labview |
| 收稿时间： | 2015/10/1 0:00:00 |
Remote control unmanned aerial vehicle test system based on Labview |
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| Zhang Kun,Zhang Tiemin,Liao Yiyong,Zhuang Xiaolin,Li Shenghua and Lan Yubin.Remote control unmanned aerial vehicle test system based on Labview[J].Transactions of the Chinese Society of Agricultural Engineering,2015,31(Z2):11-16. |
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| Authors: | Zhang Kun Zhang Tiemin Liao Yiyong Zhuang Xiaolin Li Shenghua and Lan Yubin |
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| Institution: | College of Engineering, South China Agricultural University, Guangzhou 510642, China,College of Engineering, South China Agricultural University, Guangzhou 510642, China,College of Engineering, South China Agricultural University, Guangzhou 510642, China,College of Engineering, South China Agricultural University, Guangzhou 510642, China,College of Engineering, South China Agricultural University, Guangzhou 510642, China and College of Engineering, South China Agricultural University, Guangzhou 510642, China |
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| Abstract: | A remote control UAV test system was designed for assessing control level of the flight operators.During the test, the flight operator should control the UAV to take-off, flying along the scheduled flight path, spot hover and fixed-point landing.The system used IG-500N to acquire real-time UAV flight status and sent it to the ground computer by wireless data transmission module.Flight status information was consist of triaxial attitude angle, triaxial accelerometer, triaxial angular,triaxial speed, GPS latitude and longitude, GPS altitude, temperature and barometric pressure.The system software based on labview extracted the data corresponding to every test project.Then it calculated time, position deviation and attitude stability based on these data.So as to obtain control level indicators that would be imported into the test report.Experiment results showed that the system can be used to provide a reference for assessing operator level of the flight and performance improvement of autonomous UAV. |
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| Keywords: | unmanned aerial vehicles remote sensing design flight status control level test system Labview |
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