摘要
以项目的控制计算机为研究背景 ,按照高性能和小型化的要求 ,设计并实现了基于DSP的新型弹载控制计算机 ,突破了基于 PC机和普通单片机的弹载计算机无法同时满足高速度、高精度和实现小型化的限制。详细给出了整体方案的设计原则和设计方案、硬件选型、接口设计、软件编制以及软件和硬件的具体调试步骤 。
In certain project a new kind of missile control computer is designed and brought to success on the demand of high performance and miniaturization,which breaks through the limit on meeting the target of high speed,high precision and miniaturization simultaneously for missile control computer based on PC ornormal micro- chip processor.The detailis given forthe design principle and scheme,the choice of hardware,the connecting design,the software programming,and the debug- ging of software and hardware.The ground performance checkout is qualified.
出处
《导弹与航天运载技术》
北大核心
2002年第1期25-30,共6页
Missiles and Space Vehicles
