飞航导弹一体化制导控制系统

针对传统飞航导弹制导控制系统可靠性低、硬件和软件的重用性低、使用维护成本高等不足,从软件一体化和功能及结构一体化方面对飞航导弹制导控制系统一体化设计技术进行初步研究。以一体化、集成化和模块化的设计思路,采用高性能微处理器+总线为基础的计算机体系结构,配置强实时的分区操作系统,整合各种硬件资源,设计出具有体积小、重量轻、成本低、基本可靠性高的一体化弹载制导控制系统。该系统已成功应用于某型飞航导弹。

Integrated Guidance-Control System for Winged Missile

The tradition guidance-control system of winged missile has many flaws, such as low basic reliability, low reusable of the software and hardware, and high cost of maintenance. This paper accomplish the elementary research with the design technology of integrated guidance-control （IGC） system for winged missile from the aspect of the software integration, function integration and structure integration. With the design idea of the integration and modularization, use the computer architecture basis of the high-powered microprocessor and data bus, collocate the high real-time partition operating system, coordinate the hardware resources, design the integrated missile-borne guidance-control system with the light weight, low cost and high basic dependability. This system has been successfully implemented in the certain type winged missile.