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[an error occurred while processing this directive]Journal of Projectiles, Rockets, Missiles and Guidance >
Missile Guidance Control System Simulation Based on HLA and Simulink
Received date: 2009-11-21
Online published: 2025-05-28
In order to resolve issues including lack of rea-l time and interaction of missile stabilization control system based on Simulink tools,the simulation system was completed by use of Simulink and C++mixed programming technique which can combine the merits of these two language tools.The control model was transformed into a member of the federation which can interact with the other members based on HLA,so the high-level visual simulation testing system was realized based on HLA.Not only is this system suitable for digital simulation test,but also can be extended to the hardware-in-the-loop simulation test of missile’s stabilization control system.This method proposed in this paper has high engineering practice value.
Key words: missile stabilization control system; missile guidance; HLA; Simulink
CHEN Tao , ZHANG Wenhan , GUO Limin , ZHANG Guoyao . Missile Guidance Control System Simulation Based on HLA and Simulink[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(5) : 13 -16 . DOI: 10.15892/j.cnki.djzdxb.2010.05.057
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