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International Standard Serial Number:
ISSN 1001-4551
Sponsor:
Zhejiang University;
Zhejiang Machinery and Electrical Group
Edited by:
Editorial of Journal of Mechanical & Electrical Engineering
Chief Editor:
ZHAO Qun
Vice Chief Editor:
TANG ren-zhong,
LUO Xiang-yang
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HUANG Can, BU Linsen, WANG Min, CHEN Wenliang
(College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)
Abstract: 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 multiaxis 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.
Key words: assembly system; component; configuration file; control system