低成本高集成一体化测发控系统设计研究  

Research of Low Cost and High Integration for Launch Control System

作　　者：王旭[1] 荣刚[1] 常曦 姜悦[1] 麦吉[2] WANG Xu;RONG Gang;CHANG Xi;JIANG Yue;MAI Ji(China Academy of Launch Vehicle Technology,Beijing 100076,China;Beijing Aerospace Institute for Metrology and Measurement Technology,Beijing 100076,China)

机构地区：[1]中国运载火箭技术研究院,北京100076 [2]北京航天计量测试技术研究所,北京100076

出　　处：《宇航计测技术》2023年第6期76-82,共7页Journal of Astronautic Metrology and Measurement

摘　　要：运载器的测发控系统设计直接关系到地面数据传输的效率和可靠性。文中提出了一种通用性的低成本高集成一体化测发控系统,可以在保证远距离高效传输试验供配电等时序指令和遥测数据的同时,高效实现实时和事后对试验数据的解析和判读,地面软件接收器上数据完成飞行器的故障检测、健康状态评估及寿命和数据管理,将各系统功能及软件实现方法融为一体,简化了系统架构,降低了系统研制和维护成本,提高了系统集成性、可靠性及维护性。The design of the measuring,launching and control system of the vehicle is directly related to the efficiency and reliability of ground data transmission.A general low cost,high integration,integration system is proposed,which can realize real-time and post-hoc analysis and interpretation of test data while ensuring efficient transmission of time sequence instructions and telemetry data such as test power supply and distribution over long distances.Receiving the data on the aircraft,the fault detection,health status assessment,life and data management of the aircraft are completed by the ground measurement and control software.The system functions and software implementation methods are integrated to simplify the system architecture.The system development and maintenance costs are reduced,and the integration,reliability and maintenance of the system are improved.

关 键 词：低成本 高集成 一体化 测发控系统 

分 类 号：TN248[电子电信—物理电子学]