针对空空导弹制导系统传统开发流程的弊端,提出了在制导控制系统设计中应用快速原型技术进行制导系统分析、建模、仿真和代码生成的方法,并首次在RT-LAB原型开发平台生成制导控制系统快速原型,实现数字/半实物仿真的一体化设计开发和测试环境。

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.