Journal of Projectiles, Rockets, Missiles and Guidance >
Rapid Prototype Technique Research on Guidance Control System
Received date: 2009-11-18
Online published: 2025-05-28
Focused on the abuses of traditional development flow of air-to-air missile guidance control system, rapid prototype tech-nique was presented to analyze, model, simulate and generate software automatically. A rapid prototype of guidance control system was designed on RT-LAB prototype development platform. An integrative development and test environment of digital/hardware-in-the-loop simulation was realized.
ZHANG Huijun , GUO Wenwen . Rapid Prototype Technique Research on Guidance Control System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(4) : 37 -40 . DOI: 10.15892/j.cnki.djzdxb.2010.04.043
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