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Non-regression method of a tool for designing a monitoring system of an aircraft engine

机译:用于设计飞机发动机监控系统的工具的不回归方法

摘要

A system of non-regression tests of a designing tool including modules used to build a monitoring device of an aircraft engine is provided. The system includes a processor configured to automatically create an experience base by instrumenting behavior tests upon executing the modules, the experience base including reference input signals, sets of reference parameters, reference output signals, and collections of results of reference executions relating to the modules; start again the behavior tests on the modules depending on the corresponding reference input signals and the corresponding sets of reference parameters thus generating test output signals and collections of results of test executions; and compare the test output signals with the corresponding reference output signals and the collections of results of test execution with the corresponding collections of results of reference executions in order to test the non-regression of the designing tool.
机译:提供了一种设计工具的非回归测试系统,该设计工具包括用于构建飞机发动机的监视装置的模块。该系统包括处理器,该处理器被配置为通过在执行模块时进行行为测试来自动创建体验库,该体验库包括参考输入信号,参考参数集,参考输出信号以及与模块有关的参考执行结果的集合。再次根据相应的参考输入信号和相应的参考参数集在模块上开始行为测试,从而生成测试输出信号和测试执行结果的集合;并将测试输出信号与相应的参考输出信号以及测试执行结果的集合与参考执行结果的相应集合进行比较,以测试设计工具的不回归。

著录项

  • 公开/公告号US10094740B2

    专利类型

  • 公开/公告日2018-10-09

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号US201414506901

  • 发明设计人 JEROME HENRI NOEL LACAILLE;AURELIE GOUBY;

    申请日2014-10-06

  • 分类号A61B3/00;G02B27/01;A61B5/00;G01M15/00;G06F11/36;G06F11/277;

  • 国家 US

  • 入库时间 2022-08-21 13:03:51

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