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Vol. 190, Issue 7, July 2015, pp. 58-62




The Development of Synchronization Function for Triple Redundancy System Based on SCADE

1 Moupeng, 2 Duan Xiaojun

1 AVIC Chengdu Aircraft Industry Company Chengdu, Chen Fei Road Qingyang District, Chengdu, 610000, China
2 National Laboratory of UAV Special Technology, Northwestern Polytechnical University, West Youyi Road 127, Xi’an, 710072, China
1 Tel.: +86-29-88451175, fax: +86-29-88451175

1 E-mail: dxj_nwpu@sina.com


Received: 20 June 2015 /Accepted: 21 July 2015 /Published: 31 July 2015

Digital Sensors and Sensor Sysstems


Abstract: Redundancy technique is an effective approach to improve the reliability and security of flight control system, synchronization function of redundancy system is the key technology of redundancy management. The flight control computer synchronization model is developed by graphical modeling method in the SCADE development environment, the automatic code generation technology is used to generate high level reliable embedded real-time code for synchronization function, omitting the code test process, shorten the development cycle. In the practical application, the program can accomplish the functional synchronization, and lay a well foundation for the redundancy system.


Keywords: SCADE, Triple redundancy, Flight control computer, Synchronization.


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