基于双DSP的某弹载计算机的设计与实现

Design and Implement of the Double DSPs Missile-born Computer

弹载计算机是精确制导武器的核心单元,本文介绍了一种弹载计算机,采用双DSP的设计结构,且集导航和飞控一体。文章详细介绍了该弹载计算机的整体结构和详细的功能电路硬件设计方法及结构设计,通过单台计算机实现了独立的导航任务处理和飞行控制任务处理平台,并成功实现了产品的小型化、轻量化。

This paper introduces a Navigation/Flight-control Integrative Missile-born Computer, which introduces hardware design method and structure design of the whole structure and the particular function circuitry of the missile-born computer based on double DSPs. The department navigation task process and flight-control task process are realized via single computer. Miniaturization and lightweight are successfully realized.