CAJ | 학술논문

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。
침대비궤부건자동제공공예수구，재구체분석자동제공말단집행기공작류정적기출지상，통과은、동태설계화공제계통건모，기우TwinCAT연PLC개발료일투말단집행기공제계통，병최종실현료PID전폐배공제。시험결과표명，해공제계통조작방편，성능은정，겁대제고료비궤부건적제공효솔화장배질량。
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.