基于pu的航空航天应用嵌入式关键软件测试

R. P. Pontes, E. Martins, A. Ambrosio, E. Villani
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引用次数: 3

摘要

本文讨论了在INPE使用CoFI测试方法验证将用于未来卫星应用的机载数据处理(OBDH)软件的实践经验。该技术基于将被测系统建模为有限状态机,适用于航空航天应用。测试用例是从开发的模型中自动生成的。本文考虑的OBDH软件遵循欧洲空间标准化合作组织的PUS标准,该标准正在巴西采用。通过这个实践经验分析的重要问题包括发现的错误、建模活动所需的时间、测试所需的时间、测试用例的可重用性等等。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Embedded Critical Software Testing for Aerospace Applications based on PUS
This paper discusses the practical experience of verifying an On-Board Data Handling (OBDH) software to be used in a future satellite application at INPE using the CoFI testing methodology. This technique is proper for aerospace applications and is based on modeling the system under test as finite state machines. The test cases are automatically generated from the developed models. The OBDH software considered in this paper follows the PUS standard from European Cooperation for Space Standardization, which is being adopted in Brazil. Among the important issues analyzed by this practical experience are the errors found, the time required for the modeling activity, the time required for testing, the reusability of the test cases, among others.
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