航天器工程2019，Vol.28Issue(6)：46-51,6.DOI:10.3969/.j issn.1 673-8748.2019.06.007
航天器遥测信息传递通用接口设计
Design of Spacecraft Telemetry Transfer Universal Interface
摘要
Abstract
In order to solve the telemetry processing and transferring problem,such as the design disunity,structural irregularities,long processing time and difficult interaction,between the spacecraft manufacturers and control center,a hierarchical model for telemetry processing is taken and the telemetry transfer universal interface is proposed based on XTCE (XML telemetric and command exchange)standard with CCSDS.The telemetry detailed design is made from the top to the bottom and from the overall structure to the single element.Firstly,a general and ca-nonical spacecraft telemetry model is established,and the subsystem nodes are defined;after-wards,the telemetry elements are defined,including the attribute,optional attribute,subordi-nates’attributes,etc.Finally,the telemetry transfer universal interface software is made.Design verification results show that the universal interface can transfer the telemetry from spacecraft manufacturers to control center nondestructively and quickly,and it is important for the space-craft design and manufacture,control and management,and application efficiency.关键词
航天器遥测/通用接口/分层模型Key words
spacecraft telemetry/universal interface/hierarchical model分类
航空航天引用本文复制引用
张海威,郭江,匡冬梅,张江,任登高..航天器遥测信息传递通用接口设计[J].航天器工程,2019,28(6):46-51,6.基金项目
国家自然科学基金(61502523) （61502523）
