Software design of distributed automatic testing system for UAV flight control system

Zhi Zhong; Xin Chen

doi:10.1117/12.521996

2 September 2003 Software design of distributed automatic testing system for UAV flight control system

Zhi Zhong, Xin Chen

Proceedings Volume 5253, Fifth International Symposium on Instrumentation and Control Technology; (2003) https://doi.org/10.1117/12.521996
Event: Fifth International Symposium on Instrumentation and Control Technology, 2003, Beijing, China

Abstract

A software design of a distributed automatic testing system is introduced in this paper, which is used for the flight control system (FCS) of unmanned air vehicle (UAV). The RS485 network is adopted for testing several FCS at the same time in the distributed structure software. In the software, two programming technologies, "multithread" and "knowledge base (KB)" are used. The implement of such key technologies, the entirety design idea and the actual design results of the software are also shown in the paper.

Citation Download Citation

Zhi Zhong and Xin Chen "Software design of distributed automatic testing system for UAV flight control system", Proc. SPIE 5253, Fifth International Symposium on Instrumentation and Control Technology, (2 September 2003); https://doi.org/10.1117/12.521996

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