摘要
依照某无人机机电综合管理构型,针对该无人机的液冷系统,通过研究其控制功能和接口需求,运用机电综合控制技术对其进行控制构型设计、控制逻辑及故障诊断逻辑设计,利用综合管理计算机实现对液冷系统的控制与管理;在此基础上进行了该控制系统的半物理仿真试验平台设计,在该平台上运行Windows7、Linux、Vxworks5.5等多个操作系统、利用LabVIEW和Matlab/Simulink搭建并运行实时仿真模型,模拟液冷系统的实时控制及信息传输,验证控制逻辑的正确性和接口的正确性。
The article describes the requirements of function and interface for controlling a UAV liquid-cooling system,and then design the control logic to control it by using a real-time integration computer on-vehicle.Based on that,the article describes a hardware-in-loop test system for this control system.The computer of the test system have three operating systems,such asWindows7、Linux and Vxworks5.5.The LabVIEW and Simulink are used to develop a series of models to simulate this control system.In the end,the interface of the control system is tested by this test system,and the control logic is verified too.
作者
艾素霄
梁世哲
任杰
晏涛
Ai Suxiao;Liang Shizhe;Ren Jie;Yan Tao(AVIC Chengdu Aircraft Industrial(Group)Co,Ltd,Chengdu 610092,China)
出处
《计算机测量与控制》
2020年第2期136-139,168,共5页
Computer Measurement &Control
关键词
无人机
液冷
机电综合
半物理仿真
UAV
liquid-cooling
electro-mechanical integration
half physical simulation