[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 4: 176 - 180

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.04.022

CORRELATION TECHNOLOGY

Implementation and Evaluation of Operating System for Integrated Missile System

  • TANG Xiaoming ,
  • LI Yinjuan ,
  • CHENG Nong
Expand
  • 1 School of Automation, Northwestern Polytechnical University, Xi'an 710072, China
    2 Flight Automatic Control Research Institute, Xi'an 710065, China
    3 School of Information Science and Technology, Tsinghua University, Beijing 100084, China

Received date: 2011-11-02

  Online published: 2025-05-29

Fold

Abstract

The new missile task computer system employs the architecture of integrated modular avionics. Based on this architecture, the traditional sub-systems will be integrated into a single hardware platform. In this paper, a strong partitioned operating system model was proposed. With this model, the software platform can guarantee that every partition is completely independent and isolated from others. The strong partitioned operating system kernel FCOS was discussed in detail, including system architecture, partition scheduling, inter-partition communication and memory management. Besides, the analysis and evaluation of this kernel FCOS base on different benchmark were conducted. In terms of results, an optimized memory management was mentioned as well. As a real case, an integrated missile task system with three traditional systems integrated into one platform was illustrated.

Key words： integrated missile task system; strong partitioning; operating system; integrated modular avionics

Cite this article

TANG Xiaoming , LI Yinjuan , CHENG Nong . Implementation and Evaluation of Operating System for Integrated Missile System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(4) : 176 -180 . DOI: 10.15892/j.cnki.djzdxb.2012.04.022

[an error occurred while processing this directive]

References

[1]
Jose Rufino, Sergio Filipe, Manuel Coutinho, et al. ARINC653interfaces in RTEMS[C] //Proceedings of Data Systems inAerospace, DASIA'07, 2007.
[2]
SC-200 RTCA, Inc. Integrated Modular Avionics (IMA) De-velopment Guidance and Certification Considerations DO297 [Z]. RTCA, Inc, 2005.
[3]
L Lamport. Avionics Application Standard Software Inter-face [Z]. 2009: 207 – 220.
[4]
Windriver Inc. Vxworks 653 user guide [Z]. Windriver Inc, 2005.
[5]
OSEK. OSEK/VDX Operating system [Z]. OSEK. 2005.
[6]
David kleidernacher, Green Hills Softeare. ARINC 653 andIMA-compliant high robustness file systems [C] //Proceed-ings of IEEE/AIAA 27th Digital Avionics Systems Confer-ence, DASC'08, 2008.
[7]
Richard L Alena, John P Ossenfort Iv, Kenneth I Laws, et al. Communication for integrate modular avionics [C] // 2007 IEEE Aerospace Conference. 2007:1-18.
[8]
Saznuk P J. ARINC 653 role in integrated modular avionics(IMA) [C]//Proceedings of IEEE/AIAA 27 th Digital A-vionics Systems Conference, DASC'08, 2008.
[9]
Peter H Feiler. Challenges in validating safety-critical em-bedded systems [Z]. SAE International. 2009.
[10]
SC Vestal, P Binns, A Larson, et al. Safe partition sched-uling on multi-core processors: US, 20100199280A1[P]. 2010.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]