北京星际荣耀科技有限责任公司,北京 100176
[ "江良伟 男,1982年11月出生,浙江兰溪人.硕士,高级工程师.主要从事运载火箭计算机技术、数字电源技术.E-mail:jianglw@live.com" ]
[ "彭小波(通讯作者) 男,1972年12月出生,陕西汉中人.博士,研究员.主要从事航天飞行器技术研发与项目管理.E-mail:pengxb@i-space.com.cn" ]
收稿:2020-07-13,
修回:2021-02-23,
纸质出版:2021-12-25
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江良伟,彭小波.双曲线一号运载火箭综合电子系统的设计与实现[J].电子学报,2021,49(12):2307-2314.
JAING Liang-wei,PENG Xiao-bo.Design and Implementation of Integrated Modular Avionics for Hyperbola-1 Launch Vehicle[J].ACTA ELECTRONICA SINICA,2021,49(12):2307-2314.
江良伟,彭小波.双曲线一号运载火箭综合电子系统的设计与实现[J].电子学报,2021,49(12):2307-2314. DOI: 10.12263/DZXB.20200687.
JAING Liang-wei,PENG Xiao-bo.Design and Implementation of Integrated Modular Avionics for Hyperbola-1 Launch Vehicle[J].ACTA ELECTRONICA SINICA,2021,49(12):2307-2314. DOI: 10.12263/DZXB.20200687.
针对民营商业运载火箭“双曲线一号”高可靠、低成本、快响应的要求,设计了一种自定义高速串行总线架构的高集成度箭载综合电子系统.描述了综合电子系统的任务需求、各功能模块原理组成、叠板结构设计、实时操作系统以及飞控软件等关键技术.重点阐述了基于Zynq处理器的主控模块最小系统及通讯接口设计、自定义高速串行总线架构设计.随着双曲线一号首飞试验的成功,作为控制中枢的综合电子系统工作正常,满足民营商业运载火箭强实时性、高可靠性以及高精度控制等要求.
Aiming at the requirement of high reliability
low cost and fast response of the private commercial launch vehicle "Hyperbola-1"
a high-integrated launch vehicle integrated modular avionics is designed. This paper describes the task requirements of integrated modular avionics
the principle composition of each function module
the structure design of laminated board
real-time operating system and flight control software. Emphasis is given to the design of minimum system and communication interface of the main control module based on Zynq
the design of custom high-speed serial bus architecture. With the success of the first flight test of Hyperbola-1
integrated modular avionics
as a control center
works normally and meets the requirements of high real-time
high reliability and high precision control of private commercial launch vehicles.
宋征宇 . 新一代运载火箭电气系统体系架构的研究 [J]. 载人航天 , 2016 , 22 ( 3 ): 317 - 322 .
Song Z Y . Research on avionics system configuration of next generation launch vehicle [J]. Manned Spaceflight , 2016 , 22 ( 3 ): 317 - 322 . (in Chinese)
胡海峰 , 宋征宇 , 孙海峰 . 新型中型运载火箭控制系统架构及发展 [J]. 导弹与航天运载技术 , 2019 , ( 2 ): 49 - 53 .
Hu H F , Song Z Y , Sun H F . Review of avionics architecture of new medium launch vehicle and development [J]. Missiles and Space Vehicles , 2019 , ( 2 ): 49 - 53 . (in Chinese)
彭越 , 牟宇 , 宋敬群 . 中国下一代运载火箭电气系统技术发展研究 [J]. 宇航总体技术 , 2020 , 4 ( 2 ): 13 - 24 .
Peng Y , Mou Y , Song J Q . Research on the development of avionics and electrical system in Chinese next generation launch vehicle [J]. Astronautical Systems Engineering Technology , 2020 , 4 ( 2 ): 13 - 24 . (in Chinese)
李孝同 , 施思寒 , 李冠群 . 微小卫星综合电子系统设计 [J]. 航天器工程 , 2008 , 17 ( 1 ): 30 - 35 .
Li X T , Shi S H , Li G Q . Integrated electronics system of micro-satellite [J]. Spacecraft Engineering , 2008 , 17 ( 1 ): 30 - 35 . (in Chinese)
孙海峰 , 刘俊阳 , 程胜 , 等 . 面向下一代运载火箭的综合电子系统集成技术 [J]. 宇航学报 , 2019 , 40 ( 3 ): 334 - 344 .
Sun H F , Liu J Y , Cheng S , et al . Integration technology of avionics for next-generation launch vehicle [J]. Journal of Astronautics , 2019 , 40 ( 3 ): 334 - 344 . (in Chinese)
周虎 , 段然 , 凌震 , 等 . 基于综合电子的某型运载器电气系统方案设计 [J]. 宇航总体技术 , 2019 , 3 ( 3 ): 19 - 25 .
Zhou H , Duan R , Ling Z , et al . Research on electronic system of launch vehicle by integrated electronics [J]. Astronautical Systems Engineering Technology , 2019 , 3 ( 3 ): 19 - 25 . (in Chinese)
苏晓东 , 苏峰 , 宋蔚阳 , 等 . 基于VNX总线的航天飞行器综合控制系统设计 [J]. 计算机测量与控制 , 2019 , 27 ( 3 ): 117 - 120 .
Su X D , Su F , Song W Y , et al . Design of spacecraft integrated electronic system based on VNX [J]. Computer Measurement & Control , 2019 , 27 ( 3 ): 117 - 120 . (in Chinese)
苏晓东 , 宋蔚阳 , 鞠晓燕 , 等 . 基于Zynq平台的弹载计算机设计 [J]. 航天控制 , 2019 , 37 ( 6 ): 48 - 53 .
Su X D , Song W Y , Ju X Y , et al . Design of missile-borne computer based on zynq [J]. Aerospace Control , 2019 , 37 ( 6 ): 48 - 53 . (in Chinese)
辛高波 , 王猛 , 丁秀峰 , 等 . 运载火箭冗余分级智能供配电技术研究 [J]. 计算机测量与控制 , 2018 , 26 ( 10 ): 137 - 140, 154 .
Xin G B , Wang M , Ding X F , et al . Study of a redundant intelligent power distribution system for launch vehicle [J]. Computer Measurement & Control , 2018 , 26 ( 10 ): 137 - 140, 154 . (in Chinese)
张拓 , 党小鹏 , 韩连刚 , 等 . 高可靠性小型固体动力运载火箭时序控制器设计 [J]. 计算机测量与控制 , 2019 , 27 ( 2 ): 135 - 138 .
Zhang T , Dang X P , Han L G , et al . Design of time serier controller for highly reliable small solid dynamic launch vehicle [J]. Computer Measurement & Control , 2019 , 27 ( 2 ): 135 - 138 . (in Chinese)
张宏波 , 李长森 , 李铁麟 , 等 . 一种新型多点互联高速冗余总线通信方法与实现 [J]. 航天控制 , 2018 , 36 ( 6 ): 53 - 59, 75 .
Zhang H B , Li C S , Li T L , et al . Method and implementation of a novel multi-point interconnect high-speed redundant bus communication [J]. Aerospace Control , 2018 , 36 ( 6 ): 53 - 59, 75 . (in Chinese)
黄波 , 曹帮林 , 张福鑫 , 等 . 一种三模混合冗余总线控制系统设计研究 [J]. 航天控制 , 2015 , 33 ( 6 ): 76 - 80 .
Huang B , Cao B L , Zhang F X , et al . Research on triple modular hybrid redundant bus control system [J]. Aerospace Control , 2015 , 33 ( 6 ): 76 - 80 . (in Chinese)
姚国伟 , 张凤 , 曹建文 , 等 . 基于有向图的运载火箭综合电子系统设计方法 [J]. 北京理工大学学报 , 2019 , 39 ( 6 ): 650 - 654 .
Yao G W , Zhang F , Cao J W , et al . Launch vehicle integrated electronic system design based on directed graph method [J]. Transactions of Beijing Institute of Technology , 2019 , 39 ( 6 ): 650 - 654 . (in Chinese)
王小辉 , 张涛 , 吕殿君 , 等 . 面向软件定义的飞行器综合电子系统软件架构技术 [J]. 航天控制 , 2019 , 37 ( 4 ): 66 - 71 .
Wang X H , Zhang T , Lv D J , et al . Software architecture technology of software-defined spacecraft integrated electronic system [J]. Aerospace Control , 2019 , 37 ( 4 ): 66 - 71 . (in Chinese)
陈建新 , 张志 , 王磊 , 等 . 嫦娥三号巡视器综合电子系统的设计与实现 [J]. 中国科学: 技术科学 , 2014 , 44 ( 5 ): 450 - 460 .
Chen J X , Zhang Z , Wang L , et al . Design and realization of the integrated electronic system for the <math id="M1"><mi mathvariant="normal">C</mi><mi mathvariant="normal">h</mi><mi mathvariant="normal">a</mi><mi mathvariant="normal">n</mi><msup><mrow><mi mathvariant="normal">g</mi></mrow><mrow><mi>'</mi></mrow></msup></math> http://html.publish.founderss.cn/rc-pub/api/common/picture?pictureId=39073294&type= http://html.publish.founderss.cn/rc-pub/api/common/picture?pictureId=39073289&type= 8.72066593 2.96333337 E-3 lunar rover [J]. Scientia Sinica (Technologica) , 2014 , 44 ( 5 ): 450 - 460 . (in Chinese)
仇公望 , 詹景坤 , 吕殿君 , 等 . 基于边缘计算的航天器电气系统设计 [J]. 电子测试 , 2019 ( 13 ): 12 - 15 .
Qiu G W , Zhan J K , Lv D J , et al . Design of spacecraft avionics system based on edge computing [J]. Electronic Test , 2019 , 2019 ( 13 ): 12 - 15 . (in Chinese)
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