A Study on the Development of HWIL Simulation Control System for High Maneuver Guided Missile System 


Vol. 35,  No. 11, pp. 1659-1666, Nov.  2010


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  Abstract

The High maneuver missiles use various interfaces and high speed guidance and control loop. Hardware-in-the-Loop(HWIL) simulation control system, therefore, should have high performance computing power and hardware interface capabilities, and should be developed using IT technology with which real time operating system, embedded system, data communication technology, and real time hardware control are integrated. This paper suggests the control system design techniques, such as a system hardware configuration, a job distribution algorithm for high performance multi-processors, a real time calculation and control mechanism, inter-processor communication mechanism, and a real time data acquisition technique, to perform the HWIL simulation for high maneuver missile system.

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  Cite this article

[IEEE Style]

W. Kim, B. Lee, S. Kim, "A Study on the Development of HWIL Simulation Control System for High Maneuver Guided Missile System," The Journal of Korean Institute of Communications and Information Sciences, vol. 35, no. 11, pp. 1659-1666, 2010. DOI: .

[ACM Style]

WoonSik Kim, ByungSun Lee, and SangHa Kim. 2010. A Study on the Development of HWIL Simulation Control System for High Maneuver Guided Missile System. The Journal of Korean Institute of Communications and Information Sciences, 35, 11, (2010), 1659-1666. DOI: .

[KICS Style]

WoonSik Kim, ByungSun Lee, SangHa Kim, "A Study on the Development of HWIL Simulation Control System for High Maneuver Guided Missile System," The Journal of Korean Institute of Communications and Information Sciences, vol. 35, no. 11, pp. 1659-1666, 11. 2010.

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pISSN : 1226 - 4717
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