4 m×3 m风洞大迎角机构上位机软件  

Upper Computer Software for High Angle of Attack Mechanism in 4 m×3 m Wind Tunnel

作　　者：刘赟[1] 黄心跃 张苗苗 陈陆军[1] Liu Yun;Huang Xinyue;Zhang Miaomiao;Chen Lujun(Low Speed Institute,China Aerodynamics Research and Development Center,Mianyang 621000,China)

机构地区：[1]中国空气动力研究与发展中心低速所,四川绵阳621000

出　　处：《兵工自动化》2024年第7期79-81,96,共4页Ordnance Industry Automation

摘　　要：针对大迎角机构机械装置、控制硬件的改造升级,基于Labview框架平台设计编写上位机控制软件。优化更新基于TCP/IP协议的Socket通信,增设虚拟支杆设定、模型防碰撞识别等功能。编制的控制软件已成功应用于气动中心4 m×3 m低速风洞大迎角试验。结果表明,该软件有效提升了试验质量效率和设备运行安全。In order to upgrade the mechanical device and control hardware of high angle of attack mechanism,the upper computer control software is designed and compiled based on Labview framework platform.The Socket communication based on TCP/IP protocol is optimized and updated,and the functions of virtual pole setting and model anti-collision identification are added.The developed control software has been successfully applied to the high angle-of-attack test in the 4 m×3 m low speed wind tunnel of the aerodynamic center.The results show that the software can effectively improve the efficiency of test quality and the safety of equipment operation.

关 键 词：4 m×3 m低速风洞 大迎角试验 上位机控制软件 

分 类 号：TJ430.2[兵器科学与技术—火炮、自动武器与弹药工程] V211.74[航空宇航科学与技术—航空宇航推进理论与工程]