应用FPGA实现弹载飞行控制器控制算法IP核  

The Implementation of Real-time Control Algorithmic IP Core for Missile-borne Flight Controller using FPGA

作　　者：徐铁军 丁力 黄超凡 周玉清 马强 XU Tiejun;DING li;HUANG Chaofan;ZHOU Yuqing;MA Qiang(No.203 Research Institute of China Ordnance Industries,Xi’an 710065,China;State Grid Shandong Electric Power Company,Jinan 250001,China)

机构地区：[1]中国兵器工业第203研究所,西安710065 [2]国网山东省电力公司,济南250001

出　　处：《兵器装备工程学报》2018年第3期131-134,共4页Journal of Ordnance Equipment Engineering

摘　　要：为了应用FPGA(Field Programmable Gate Array现场可编程门阵列)实现某型反坦克导弹弹载飞行控制器的设计,采用了基于模型的设计方法,实现了弹载飞行器控制器控制算法IP核,并对IP核进行了仿真验证;在Quatus Ⅱ开发环境下,进行了综合、布局,获得该IP核的相关属性。最后通过Modelsim联合仿真,表明该设计实现的有效性,为弹载飞行控制器ASIC的实现奠定技术基础。To apply the FPGA(Field Programmable Gate Array)to the implementation of a certain type of anti-tank missile-borne flight controller IP core,the method of model-based design is adopted,and the simulation verification for IP core is done;In the development environment of Quatus II,the synthesize and layout process are carried out,the related properties of this IP core are obtained.The feasibility and validity of this method are proved by associative simulation under Modelsim,and laid a technical foundation for the realization of ASIC.

关 键 词：FPGA 弹载飞行控制器 实时控制 控制算法IP核 基于模型的设计 专用控制器集成电路 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计] TP391[自动化与计算机技术—计算机应用技术]