可快速配置的多轴装配系统控制软件设计
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摘要
针对飞机装配系统控制软件重用性低、开发难度高等问题,对装配系统控制软件的架构、系统的组织方式、数据的存储和处理等方面进行了研究。提出了一种基于组件和配置文件技术的装配系统控制软件开发方法,设计了开放式的软件架构、基于组件化和配置文件的功能模块,以及基于XML配置技术的系统配置方法。研究结果表明:该软件平台具有很强的伸缩性和可复用性,利用系统配置文件更替部分组件,可以快速配置出面向不同装配系统的控制软件,后续开发者只需要遵循组件接口的标准,所开发的组件就能为系统所加载。
Aiming at the problems of low reusability and high difficulty in the development of control software for aircraft assembly systems,the architecture and organization of the control software and the storage and processing of data were studied. A method of developing control software for multi-axis assembly system based on component and configuration file was proposed. An open software architecture,functional modules based on componentization and configuration files,and a system configuration method based on XML configuration technology were designed. The results indicate that the software platform is highly scalable and reusable. Utilizing the system configuration file to replace some components can quickly configure the control software for different assembly systems. Subsequent developers only need to follow the standard of component interfaces,then the components can be loaded by the system.
Aiming at the problems of low reusability and high difficulty in the development of control software for aircraft assembly systems,the architecture and organization of the control software and the storage and processing of data were studied. A method of developing control software for multi-axis assembly system based on component and configuration file was proposed. An open software architecture,functional modules based on componentization and configuration files,and a system configuration method based on XML configuration technology were designed. The results indicate that the software platform is highly scalable and reusable. Utilizing the system configuration file to replace some components can quickly configure the control software for different assembly systems. Subsequent developers only need to follow the standard of component interfaces,then the components can be loaded by the system.
引文
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[2]许国康.大型飞机自动化装配技术[J].航空学报,2008,29(3):13-13.
[3]高明辉,张杨,张少擎,等.工业机器人自动钻铆集成控制技术[J].航空制造技术,2013,440(20):74-76.
[4]刘宇平,杨宏毅.打造航空工业自动钻铆设备先锋[J].航空制造技术,2006(12):60-61.
[5] ATKINSON J,HARTMANN J,JONES S,et al. Robotic drilling system for 737 aileron[C]. SAE 2007AeroTech Congress&Exhibition. Los Angeles:SAE,2007.
[6]邓锋. MPAC自动钻铆机[J].航空制造技术,2010(6):26-29.
[7] HOGAN S,HARTMANN J,THAYER B,et al. Automated wing drilling system for the A380-GRAWDE[C]. Proceedings of the Autom ated Fastening Conference and Exposition,Montreal:SAE,2003.
[8]沈建新,田威.基于工业机器人的飞机柔性装配技术[J].南京航空航天大学学报,2014,46(2):181-189.
[9]甘露,姚艳彬,魏超.爬行机器人制孔系统在飞机装配中的应用研究[J].航空制造技术,2013,440(20):80-82.
[10]赵辉.基于UMAC的自动钻铆机控制系统研究与开发[D].南京:南京航空航天大学机电工程学院,2014.
[11]门昌华,关学锋,胡明,等.基于PMAC的六自由度机器人开放式控制系统开发[J].机电产品开发与创新,2008,21(4):4-5.
[12]吴琳,谭营,唐建.运动控制技术发展与展望[J].机床与液压,2007,35(7):231-233.
[13] BALDWIN C Y,CLARK K B. Design rules,the power of modularity[M]. Cambridge:MIT Press,2000
[14]谢峰,肖晓明,蔡自兴.移动机器人的可重构控制系统[J].控制工程,2007,14(5):535-539.
[15]柳建飞,张伟中.新型二自由度移动并联机构设计[J].轻工机械,2017,35(2):63-65.
[16]阎思达,陈雁,陈文卓.六自由度加油机器人运动特性分析[J].液压气动与密封,2017(11):26-29.
[17] STEWART D B,KHOSLA P K. The Chimera Methodology:designing dynamically reconfigurable and reusable realtime software using port-based object[J]. International Journal of Software Engineering&Knowledge Engineering,1996,6(2):249-277
[18] WILLS L,KANNAN S,SANDER S,et al. An open platform for reconfigurable control[J]. Control Systems IEEE,2001,21(3):49-64.