惯性/卫星组合导航系统软件测试  

Software Testing for Inertail/Satellite Integrated Navigation System

作　　者：李萍[1] 王海明 郭伟全[1] LI Ping;WANG Haiming;GUO Weiquan(CEPREI,Guangzhou 510610,China)

机构地区：[1]工业和信息化部电子第五研究所,广东广州510610

出　　处：《电子产品可靠性与环境试验》2018年第3期37-40,共4页Electronic Product Reliability and Environmental Testing

摘　　要：给出了一种惯性/卫星组合导航系统软件测试的解决方案,可以广泛地应用于工程实践中来提高和保障惯性/卫星组合导航系统软件的可靠性。通过对惯性/卫星组合导航系统的软件用途和功能进行总结,提炼出了惯性/卫星组合导航系统软件通用的测试需求,包括导航参数计算、卡尔曼滤波测试、时间性能和导航性能计算,并分别给出了各个软件需求的测试方法,测试方法切实可行,具有较强的工程实践性。A solution for software testing of inertial/satellite integrated navigation system is given, which can be widely used in engineering practice to improve and guarantee the reliability of the software of inertial/satellite integrated navigation system. By summarizing the application and function of the software of inertial/satellite integrated navigation system, the common testing requirements of the software of inertial/satellite integrated navigation system are extracted,including navigation parameter calculation, kalman filter test, time and navigation performance calculation. Besides, the testing methods for each software requirement are given respectively,and the testing methods are feasible and have strong engineering practicability.

关 键 词：惯性/卫星组合导航 软件测试 黑盒测试 

分 类 号：TN671[电子电信—电路与系统] TP311.55[自动化与计算机技术—计算机软件与理论]