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An Open Integrated Electronic System Software Architecture Design for Launch Vehicle

  • Feng ZhangEmail author
  • Guo-wei Yao
  • Qian Wang
  • Yun Xia
Conference paper
Part of the Lecture Notes in Electrical Engineering book series (LNEE, volume 517)

Abstract

In view of advantages and disadvantages analysis of software communication architecture (SCA), general open architecture (GOA) and avionics software system structure (ARINC653), a new type of integrated system software architecture which is suitable for launch vehicle was designed in this paper. According to the characteristics of the launch vehicle software, the new software system architecture including four layers, such as resource service layer, operating system layer, middleware layer, and application layer. Each layer is independent to each other, and all layers can integrate the functions of the traditional launch vehicle software system. The new software system architecture can support flexible functional expansion and tailoring, which enables it to quickly adapt to the requirements of different types of launch vehicles, and greatly reduce the repetitive design work.

Keywords

Launch vehicle Integrated electronic system Software architecture 

References

  1. 1.
    Chen, H.P., Luo, H., Liu, Y., et al.: Analysis and enlightenment on development trend of launch vehicle abroad. J. Aerosp. Ind. Manag. 11, 34–37 (2015)Google Scholar
  2. 2.
    Song, Z.Y.: Research on avionics system configuration of next generation launch vehicle. J. Manned Spacefl. 22(3), 317–322 (2016)Google Scholar
  3. 3.
    Wang, Y.: Design and Development of Frequency-Hopping Communication Waveform Based of SCA, D. Hangzhou Dianzi University, Hangzhou (2010)Google Scholar
  4. 4.
    Cai Z., Zhang X.Q.: Overview of SCA 4.0 specification, J. Commun. Technol. 46(7), 126–128 (2013)Google Scholar
  5. 5.
    Huang, Y.K., Xue, Q.H., Li, W.M.: A study on open systems architecture standards. J. Avion. Technol. 36(1), 34–41 (2005)Google Scholar
  6. 6.
    Cui, X.N., Hu, L.P., Ye, H., et al.: Research on software interfaces of integrated avionics system. J. Comput. Sci. 38(2), 122–126 (2011)Google Scholar
  7. 7.
    GJB: Software communications architecture for tactical radio systems, 5028–2004Google Scholar
  8. 8.
    SAE AS4893:. Generic open architecture (GOA) framework. USA (1996)Google Scholar
  9. 9.
    Huang, Y.K., Wu, J.M., Gu, T., et al.: Analysis and research on SAE AS4893 general open architecture (GOA) framework. J. Avion. Technol. 38(1), 40–46 (2007)Google Scholar
  10. 10.
    Pu, X.-B.: Modern Avionics System and Integration, 1st edn. Aviation Industry Press, Beijing (2013)Google Scholar

Copyright information

© Springer Nature Singapore Pte Ltd. 2020

Authors and Affiliations

  1. 1.Research and Development Center, Academy of Launch Vehicle Technology, ChinaBeijingChina

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