首页 | 本学科首页   官方微博 | 高级检索  
     

运载火箭测发控技术未来发展与展望
引用本文:任月慧,张宏德,彭越,徐利杰,刘洋,马小龙. 运载火箭测发控技术未来发展与展望[J]. 计算机测量与控制, 2021, 29(6): 1-4. DOI: 10.16526/j.cnki.11-4762/tp.2021.06.001
作者姓名:任月慧  张宏德  彭越  徐利杰  刘洋  马小龙
作者单位:北京宇航系统工程研究所,北京 100076
摘    要:工业电子、测试、测控、仪表、大数据、云平台等技术的发展,为运载火箭测发控技术的发展提供了先进的技术途径;运载火箭箭上电气系统一体化设计,火箭快速测发、健康管理、子级独立测试、异地远程测试发射支持等需求,给测发控系统研制及更新换代提出更高的要求;通过对运载火箭地面测控系统供配电、有线测控、无线测控、数传通信、测发控软件5个组成部分的演变及发展方向进行了论证分析,并提出了后续测发控系统技术发展的规划路线;同时结合未来运载火箭的发展需求和目前测发控系统现状提出了测发控系统后续发展的可实施途径;最后提出顶层规范技术路径;从型号牵引转变为装备化研制;规范型谱产品研制、箭上地面同步发展的测发控系统设计新思路;为未来运载火箭测发控系统研制提供方向。

关 键 词:测发控系统  发展
收稿时间:2021-02-19
修稿时间:2021-05-05

Optimization for Commanding Mode of Unified Test and Launch Control
Ren Yuehui,Zhang Hongde,Peng Yue,Xu Lijie,Liu Yang,Ma Xiaolong. Optimization for Commanding Mode of Unified Test and Launch Control[J]. Computer Measurement & Control, 2021, 29(6): 1-4. DOI: 10.16526/j.cnki.11-4762/tp.2021.06.001
Authors:Ren Yuehui  Zhang Hongde  Peng Yue  Xu Lijie  Liu Yang  Ma Xiaolong
Abstract:With the development of industrial electronics, testing, measurement and control, instrumentation, big data, cloud platform and other technologies, it provides an advanced technical way for the development of launch vehicle test and launch control technology; the integrated design of launch vehicle electrical system, the requirements of rapid launch test, health management, sub level independent test, remote test launch support and so on, provide a reference for the development and upgrading of launch vehicle test and launch control system Higher requirements. This paper demonstrates and analyzes the evolution and development direction of the five components of the launch vehicle ground measurement and control system, including power supply and distribution, wired measurement and control, wireless measurement and control, data communication and measurement launch control software, and puts forward the planning route of the follow-up measurement launch control system technology development. At the same time, combined with the development needs of future launch vehicles and the current situation of the test launch control system, the feasible way of the follow-up development of the test launch control system is proposed. Finally, a new design idea of launch control system is put forward, which includes top-level standard technology path, transformation from model traction to equipment development, standard spectrum product development and synchronous development on the ground. It provides a direction for the development of launch test and control system of launch vehicle in the future.
Keywords:Test and launch control system   development
本文献已被 维普 万方数据 等数据库收录!
点击此处可从《计算机测量与控制》浏览原始摘要信息
点击此处可从《计算机测量与控制》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号