基于LabVIEW与DSP的机载电源模拟测试系统的设计与研究
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摘要
论文介绍了基于LabVIEW与DSP的机载电源模拟测试系统的设计方案,通过控制直流电源的正常、低压、高压和断电输出,模拟GJB181A—2003中所规定的用电设备耐电压试验,完成用电设备的欠压、过压、瞬时断电试验。实验表明:该系统符合GJB181A要求,具有自动化成度高、测试稳定、使用方便、界面友好等优点。
This paper introduces the in airborne power supply based on DSP and LabVIEW simulation test system design scheme,By controlled the DC power supply is normal,low pressure and high pressure and power output,the simulation GJB181A-2003 in the specified for electrical equipment voltage withstanding test,complete with electrical equipment under voltage,over voltage,instantaneous power test.The experiment shows that the system has high degree of automation,self calibration,test stability,voltage waveform display,convenient use and verification.
This paper introduces the in airborne power supply based on DSP and LabVIEW simulation test system design scheme,By controlled the DC power supply is normal,low pressure and high pressure and power output,the simulation GJB181A-2003 in the specified for electrical equipment voltage withstanding test,complete with electrical equipment under voltage,over voltage,instantaneous power test.The experiment shows that the system has high degree of automation,self calibration,test stability,voltage waveform display,convenient use and verification.
引文
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[3]夏国清,冯建朝,任仁良.基于虚拟仪器的航空逆变电源输出特性测量研究[J].仪器仪表学报,2010,31(11):2555-2560.XIA Guoqing,FENG Jianchao,REN Renliang.Study on the measurement of aircraft inventor Output characteristics based on virtual instrument[J].Chinese Journal of Scientific Instrument,2010,31(11):2555-2560.
[4]杨乐.飞机电源系统的建模方法研究[J].科学技术与工程,2013(9):2611-2615.YANG Le.Research on Modeling Approach of Aircraft Electrical Power Systems[J].Science Technology and Engineering,2013(9):2611-2615.
[5]高红红.机载电源检测系统的设计[J].西安工业大学学报,2009(12):534-538.GAO Honghong.Design of Detection System for Airborne Power Supply[J].Journal of Xian Technological University,2009(12):534-538.
[6]李俭川,秦国军,陶利民.虚拟仪器系统构建策略及其在飞机二次电源维修中的应用[J].计算机自动测量与控制,2001(3):49-52.LI Jianchuan,QIN Guojun,TAO Limin.Construction Strategy of Virtual Test System and Its Application in Airplane Convertor Maintain[J].Computer Automated Measurement&Control,2001(3):49-52.
[7]刘少军,王瑜瑜.基于LabWindows/CVI的飞机电负载系统设计[J].电子技术应用,2014,40(11):92-94.LIU Shaojun,WANG Yuyu.Design of plane electric load based on the LabWindows/CVI[J].Application of Electronic Technique,2014,40(11):92-94.
[8]袁旭猛,郭晓义.一种新型无人机机载电源浪涌保护器的设计[J].计算机测量与控制,2011,19(6):1487-1489.YUAN Xumeng,GUO Xiaoyi.Research on a New Kind of DC-DC Power Surge Protective Device in Unmanned Aerial Vehicle[J].Computer Measurement&Control,2011,19(6):1487-1489.
[9]霍峰,戴小氏,田丹.综合化航电智能电源控制软件设计与实现[J].航空计算技术,2011,41(5):91-94.HUO Feng,DAI Xiaoshi,TIAN Dan.Design and Realization of Intelligence Power Supply Software in Integrated Module Avionics[J].Aeronautical Computing Technique,2011,41(5):91-94.
[10]庄旭岩,徐亚军,包勇.飞机电院系统故障诊断专家系统研究[J].现代电子技术,2014(8):177-180.ZHUANG Xuyan,XU Yajun,BAO Yong.Study on fault diagnosis expert system for aircraft power-supply system[J].Modern Electronics Technique,2014(8):177-180.