检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:钟文琦 刘达 管斌 付宇[2] ZHONG Wenqi;LIU Da;GUAN Bin;FU Yu(College of Electronic Information and Automation,Civil Aviation University,Tianjin 300300,China;College of Aeronautical Engineering,Civil Aviation University,Tianjin 300300,China)
机构地区:[1]中国民航大学电子信息与自动化学院,天津300300 [2]中国民航大学航空工程学院,天津300300
出 处:《计算机应用》2020年第S01期279-283,共5页journal of Computer Applications
基 金:航空科学基金资助项目(20183367013)。
摘 要:针对无人机无线充电平台的感应耦合电能传输(ICPT)系统要求,对其补偿网络工作模式及参数设计进行了研究,提出了一种实现原边线圈励磁电流恒定、负载端恒流输出的参数设计方法。通过发射端励磁电流恒定特性、接收端恒压输出特性、接受端恒流输出特性等约束条件,分析双LCCL谐振补偿电路原边恒流副边恒压与原边恒流副边恒流两种模式的工作特性,得出在产生横向偏移时原边恒流副边恒流模式能够保持其工作模式。根据无人机降落在无线充电平台易产生横向偏移的特点,选择原边恒流副边恒流的工作模式进行Simulink仿真与样机开发,证明了不同无人机或无人机降落产生横向偏移导致互感的改变不影响系统工作状态,验证了此参数设计方法在无人机无线充电平台应用的准确性与有效性。For the requirement of Induction Coupled Power Transmission(ICPT)system on wireless charging platform of Unmanned Aerial Vehicle(UAV),the working mode and parameter design of compensation network were studied,moreover,a parameter design method was proposed to realize constant excitation current of the primary side coil and constant current output of the load side. Based on the constraints of constant excitation current at the transmitter,constant voltage output at the receiver and constant current output at the receiver,the working characteristics of two modes of double Inductance-Capacitance-Capacitance-Inductance(LCCL)resonant compensation circuit,including constant current at the primary side constant voltage at the secondary side mode;and constant current at the primary side-constant current at the secondary side mode,were analyzed. It was concluded that the constant current at the primary side and constant current at the secondary side mode can maintain its working condition when lateral offset occurs. According to the lateral offset of UAV landing on the wireless charging platform,Simulink simulation and prototype development were carried out by choosing the working mode of constant current at the primary side and constant current at the secondary side. It was proved that the change of mutual inductance caused by the lateral offset of different UAV or UAV landing did not affect the working state of the system,and the accuracy and effectiveness of this parameter design method in the application of UAV wireless charging platform was verified.
分 类 号:TP391.9[自动化与计算机技术—计算机应用技术]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.222