Study of UAV Flight Control Software Test Method

被引：0
|
作者：
Sun, Ting [1 ]
Wang, Jiasi [1 ]
Zhang, Ying [1 ]
Xiang, Liang [1 ]
机构：
[1] Beijing Special Vehicles Inst, Beijing, Peoples R China
来源：
INTERNATIONAL CONFERENCE ON ELECTRONIC INFORMATION TECHNOLOGY AND INTELLECTUALIZATION (ICEITI 2016) | 2016年
关键词：
D O I：
暂无
中图分类号：
C93 [管理学]; O22 [运筹学];
学科分类号：
070105 ; 12 ; 1201 ; 1202 ; 120202 ;
摘要：
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.
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页码：407 / 415
页数：9
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