航天嵌入式软件动力学仿真环境的通用软件架构  

Universal Software Framework for Dynamics Simulation of Aerospace Embedded Software

作　　者：蔡雨辰[1] 奚坤[1] 黎藜[1] 王振华[1] 

机构地区：[1]北京控制工程研究所,北京100094

出　　处：《空间控制技术与应用》2017年第3期66-70,共5页Aerospace Control and Application

基　　金：国防基础科研资助项目(JCKY2016203B006)

摘　　要：针对航天嵌入式软件测试环境通用化需求,提出动力学软件的通用化设计方法.基于航天动力学仿真的特点,设计灵活、通用和易于扩展的软件框架、接口数据结构和接口函数,适用于在研型号的所有接口处理方式.该方法在实际型号工作中完成应用,显著提高了动力学软件的研制速度,动力学软件运行稳定,精度满足测试要求.In order to develop the general construction of the aerospace embedded software testing environment,a general method for the aerospace dynamics software design is proposed. Based on the characteristics of aerospace dynamic simulation,a flexible generic and extensible software framework,interface data structures as well as interface functions are proposed,which are applied to all the simulation requirements of spacecraft under developing. The given method is applied in practical work. The programming progress is significantly increased,and the dynamics software is running stably and with high precision.

关 键 词：航天嵌入式软件测试 通用测试环境 动力学软件 

分 类 号：TN492[电子电信—微电子学与固体电子学]