一种面向航天器综合电子的ASIC芯片设计

周莉; 安军社; 方青文; 蔡飞

doi:10.11728/cjss2014.04.497

一种面向航天器综合电子的ASIC芯片设计

doi: 10.11728/cjss2014.04.497

周莉^1,2, ,,
安军社¹,
方青文^1,2,
蔡飞³

1.
中国科学院空间科学与应用研究中心北京 100190
2.
中国科学院大学北京 100049
3.
中国科学院计算技术研究所北京 100190

基金项目: 国家重大科技专项（TY3-201106）和中国科学院空间科学战略性先导科技专项（XDA04070000）共同资助

详细信息

通讯作者:
周莉,E-mail:zhouli@nssc.ac.cn

中图分类号: V443
计量
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- 被引次数: 0
出版历程
- 收稿日期: 2013-04-22
- 修回日期: 2013-09-26
- 刊出日期: 2014-07-15

Design of an ASIC Chip for Spacecraft Integrated Avionics

Zhou Li^{1,2
, ,},
An Junshe¹,
Fang Qingwen^1,2,
Cai Fei³

1.
Center for Space Science and Applied Research, Chinese Academy of Sciences, Beijing 100190
2.
University of Chinese Academy of Sciences, Beijing 100049
3.
Institute of Computing Technology, Chinese Academy of Sciences, Beijing 100190

摘要

摘要: 航天器综合电子系统通用功能集成并芯片化是目前航天器电子系统的发展趋势. 针对中国航天器电子系统小型化、综合化的应用需求，提出一种面向航天器综合电子的ASIC芯片设计方案，分析了ASIC芯片设计中的关键技术，包括芯片系统工作模式、IP核的开发应用、可靠性和低功耗设计，1553B简易终端控制模式是芯片的技术特色和典型应用. ASIC芯片的功能设计、系统仿真验证、FPGA验证和物理设计均已完成，进入流片状态. 芯片的FPGA验证结果证明了芯片设计的有效性和可靠性. ASIC芯片旨在达到国军标548S的要求，应用场景是航天器内数据总线接口单元和遥测遥控.
- 航天器综合电子系统 /
- 数据管理系统 /
- ASIC芯片 /
- MIL-STD-1553B总线 /
- 遥测遥控
Abstract: It is a trend to put the common spacecraft engineering requirements into one chip, which can miniaturize spacecraft avionics and reduce the repeated work for spacecraft engineers. Based on the analysis of space application requirements, the system design of an ASIC (Application Specific Integrated Circuit) chip for spacecraft telemetry and command system is proposed. Firstly, the chip system architecture is described. Secondly, four key techniques of the ASIC chip design are presented in detail, including design of the chip working modes, design of onchip IP cores, design of reliability, and the design of low power consumption technology. 1553B RT working mode of this ASIC is different and special from other space chips. The system test results based on FPGA show the validity and reliability of the ASIC system design. Finally, some promising applications of the ASIC chip are described.
- Spacecraft integrated avionics /
- Onboard data handling system /
- ASIC chip /
- MIL-STD-1553B /
- Telemetry and Command

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参考文献(13)

[1]	Luo Zhiqiang. Avionics Integrated Systems[M]. Beijing: Beijing Aerospace University Press, 1990:3-10. In Chinese (罗志强. 航空电子综合化系统[M]. 北京: 北京航空航天大学出版社, 1990: 3-10)
[2]	Caffrey R, Cuviello M, Phyllis H, et al. A standard spacecraft data system on a chip: NASA Goddard Space Flight Center's Essential Services Node (ESN)[C]// IEEE Aerospace Applications Conference Proceedings. Snowmass, Aspen: IEEE, 1997: 505-521
[3]	Tan Weizhi, Gu Yingqi. Space Data System[M]. Beijing: China Science and Technology Press, 2008: 5-12. In Chinese (谭维炽, 顾莹琦. 空间数据系统[M]. 北京: 中国科学技术出版社, 2008: 5-12)
[4]	Vladimirova T. A novel autonomous low-cost on-board data handling architecture for a pin-point planetary lander[J]. Acta Astron., 2011, 68:811-829
[5]	Elias M. Development of a low cost, fault tolerant, and highly reliable command and data handling computer (pulse)[C]//60th International Astronautical Congress. Daejeon: IAC, 2009: 3904-3909
[6]	Ibrahim bin S A, Sabri S F, Salleh N A. Preliminary hardware design and development of on-board data handling for pico-satellite in national space agency[J]. Appl. Mech. Mater., 2012, 225: 492-496
[7]	Zhang Weigong, Duan Qingya, Wang Jianfeng, et al. The method and study of SOC for managing system of spacecraft bus[J]. J. Astron., 2005(03):373-376. In Chinese (张伟功, 段青亚, 王剑峰, 等. 航天器总线管理系统的SOC设计与研究[J]. 宇航学报, 2005(03):373-376)
[8]	Xu Liqing. Research on the 1553B Bus Interface Technologies and FPGA Implement[D]. Xi'an: Northwestern Polytechnical University, 2006. In Chinese (徐丽清. 1553B 总线接口技术研究及FPGA 实现[D]. 西安: 西北工业大学, 2006)
[9]	Yuan Ziyang. Research on Space Irradiation Environment Adaptability of Rad-hard Godson Processor and an Design of Aerospace Computer Based on it[D]. Beijing: University of Chinese Academy of Sciences, 2009. In Chinese (袁子阳. 抗辐射加固''龙芯''处理器的空间辐射环境适应性研究及航天计算机设计[D]. 北京: 中国科学院大学, 2009)
[10]	Yang Ye. Software Design and System Verification on Anti-radiation Godson SOC for Space Application[D]. Beijing: University of Chinese Academy of Sciences, 2010. In Chinese(杨晔. 抗辐照加固''龙芯''SOC的航天应用研究软件设计与系统验证[D]. 北京: 中国科学院大学, 2010)
[11]	Zhou Li, An Junshe, Xie Yan, et al. Design of a 1553B IP core based on ASIC technology[J]. Chin. J. Space Sci., 2014, 34(01):127-136. In Chinese (周莉, 安军社, 谢彦, 等. 基于ASIC技术的1553B IP核的设计[J]. 空间科学学报, 2014, 34(01):127-136)
[12]	Sturesson F, Gaisler J, Ginosar R. Radiation characterization of a dual core LEON3-FT processor[C]//12th Proceedings of the European Conference on Radiation and its Effects on Components and Systems. Sevilla, Spain: IEEE, 2011:938-944
[13]	Chinese Academy of Sciences Space Strategic Studies Group. Space Science & Technology in China: A Roadmap to 2050[M]. Beijing: Science Publishing Company, 2009: 67-70. In Chinese (中国科学院空间领域战略研究组. 中国至2050年空间科技发展路线图[M]. 北京: 科学出版社, 2009: 67-70)