Study of UAV Flight Control Software Test Method

Ting Sun, Jiasi Wang, Ying Zhang, Liang Xiang

Abstract


UAV flight control software is the core of UAV flight control system. Sufficient test of the software is necessary to ensure safety and reliability of flight control system. According to the characteristics of some type of UAV flight control software, this paper proposed a test model based on multiple test environments and types, analyzed and applied test technique of coverage and fault injection, and developed a set of test techniques applicable to UAV flight control software.


DOI
10.12783/dtcse/iceiti2016/6166

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