飞机自动制孔末端执行器控制系统设计与开发  

Design and Development of Automatic Drilling End Effector Control System for Aircraft Assembly

作　　者：刘松[1] 韩锋[2] 戴家隆[2] 田威[2] 

机构地区：[1]成都飞机工业(集团)有限责任公司,成都610092 [2]南京航空航天大学,南京210016

出　　处：《航空精密制造技术》2014年第2期12-15,共4页Aviation Precision Manufacturing Technology

基　　金：航空科学基金(2013ZE52067);江苏省科技支撑计划项目(BE2012171)资助项目

摘　　要：针对飞机部件自动制孔工艺需求,在具体分析自动制孔末端执行器工作流程的基础之上,通过稳、动态设计和控制系统建模,基于TwinCAT软PLC开发了一套末端执行器控制系统,并最终实现了PID全闭环控制。试验结果表明,该控制系统操作方便,性能稳定,极大提高了飞机部件的制孔效率和装配质量。In order to meet the needs of automatic drilling technology of aircraft parts, on the basic of analyzing the workflow of the automatic drilling end effector, using the static and dynamic design and creating the control system model, developing a set of end effector control system based on soft PLC of TwinCAT, and realized the closed-loop control of PID. The experimental results indicate that the control system is not only easy to operate but also has stable performance. It improves the efficiency of aircraft parts drill and assembly quality.

关 键 词：末端执行器 控制系统 软PLC 全闭环控制 

分 类 号：TP273.2[自动化与计算机技术—检测技术与自动化装置]