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80年代在军用航空电子设备中将不断增加标准设备,MIL—STD—1553B已被证明是保证航空电子分系统之间通讯的有效方法.空军标准计算机结构MIL—STD—1750A和标准程序设计语言MIL—STD—1589B的应用,将进一步降低目前正在研制的许多系统的寿命周期成本.当MIL—STD—1750A规定一种专用CPU结构,而MIL—STD—1553B规定分系统之间通讯的方法时,并无现行空军标准规定连接1750处理机和1553总线的I/0通道.为了减少软件研制成本和维护成本,通用动力公司研制了一种1553通道结构,适用于F—16多国阶段改进计划(MSIP)的所有自编程系统.
MIL-STD-1553B has been proved to be an effective way to ensure the communication between Avionics subsystems in the 1980s.Air standard computer architecture MIL-STD-1750A and standard programming language MIL The application of -STD-1589B will further reduce the life-cycle cost of many systems currently under development. When MIL-STD-1750A specifies a dedicated CPU architecture and MIL-STD-1553B specifies the method of communication between subsystems, There is no existing Air Force standard to connect I / O channels to 1750 processors and 1553. To reduce software development and maintenance costs, General Dynamics has developed a 1553-channel architecture for the F-16 multinational phase improvement program (MSIP ) Of all self-programming system.