基于DSP的某发射控制计算机的设计与实现  

Design and Implementation of a Launch Control Computer Based on DSP

作　　者：刘硕 吕浩 高浩[1] 

机构地区：[1]中国航空工业集团公司西安航空计算技术研究所,西安710065 [2]西北工业大学计算机学院,西安710072

出　　处：《电子技术（上海）》2017年第12期45-47,共3页Electronic Technology

摘　　要：对于与飞机研制相互独立的机载导弹,为了实现飞机与导弹之间的电气接口的统一,满足GJB1188A的要求,需要发射架进行控制转换。为了满足导弹发射架控制系统的要求,提出了一种基于DSP的发射控制计算机的软硬件设计与实现方法,完成了飞机与导弹之间数据与控制信号的转换。发射控制计算机稳定可靠,满足了发射架控制系统的要求。设计不仅用于某型机载导弹发射架,对于非惯标的飞机悬挂物都有普遍的借鉴意义。For the aircraft developed with independent airborne missiles, it is necessary to control the conversion of the launcher to meet the requirements of GJB1188 A in order to achieve the aircraft and missile electrical interface between the unity. In order to meet the requirements of missile launcher control system, a hardware and software design and implementation method of DSP-based launch control computer is proposed, and the conversion of data and control signals between aircraft and missile is completed. The launch control computer is stable and reliable, and meets the requirements of the launcher control system. Design is not only used for a kind of airborne missile launchers, for non-standard aircraft hangings have universal reference.

关 键 词：DSP 控制计算机 发射 GJB289A总线 ARINC429 

分 类 号：TP302.1[自动化与计算机技术—计算机系统结构]