A design and simulation of aircraft drilling end-effector based on bionics

Peijiang Yuan, Tianmiao Wang, Fucun Ma, Maozhen Gong
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引用次数: 2

Abstract

This paper describes a design and simulation device for the aircraft drilling end-effector based on bionics which is mainly for robotic drilling on the aircraft surface and inner structures. The whole system is composed of six modules which are controlled by master-slave architecture. Automation studio programming software provides a programming pattern to control hardware system. Experiments show that the ADEE can greatly enhance the quality and precision of drilling holes comparing with manual drilling. We use Matlab and simulink to simulate the process of drilling and test the drilling results with non-PID drilling system (UPDS) and PID drilling system (PDS). Experiments demonstrate that the drilling results of PDS are obvious better than UPDS. At last, we apply pulsed thermography to investigate drilling defects.
基于仿生学的飞机钻孔末端执行器设计与仿真
本文介绍了一种基于仿生学的飞机钻孔末端执行器的设计与仿真装置,主要用于在飞机表面和内部结构上进行机器人钻孔。整个系统由6个模块组成,采用主从结构控制。自动化工作室编程软件为控制硬件系统提供了一种编程模式。实验表明,与手工钻孔相比,该方法能显著提高钻孔质量和精度。利用Matlab和simulink对钻井过程进行仿真,并采用非PID钻井系统(UPDS)和PID钻井系统(PDS)对钻井结果进行测试。实验表明,PDS的钻井效果明显优于UPDS。最后,应用脉冲热成像技术对钻孔缺陷进行了研究。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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