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为了确定模块计算机的结构(在导弹的整个使用范围内,这个模块结构是最适合的),须遵循图6.0—1所示的任务顺序。可以看出,一个计算机的结构综合方案必须与整个导弹系统所共有的结构设计统一起来,并且这个结构综合方案应能适应各种不同的导弹要求。计算机结构研究的输入部分列在下面,为了保证一个首尾一贯的、平衡的设计,这个输入部分包括了对设计者负有责任的,理论上的和实际上的在导弹整个使用范围内的设计限制条件。1.航空电子设备系统的接口导弹计算机系统与航空电子计算机系统的连接。
In order to determine the structure of the module computer (which is the most suitable structure throughout the missile’s use), the sequence of tasks shown in Figure 6.0-1 must be followed. It can be seen that the structural solution of a computer must be unified with the structural design that is common to the whole missile system and the integrated solution of this structure should be able to adapt to various missile requirements. The input section of the computer architecture study is listed below. To ensure a consistent and balanced design, this input section includes design restrictions on the designer, both theoretically and practically within the entire range of the missile’s use condition. 1. Interface of avionics system missile computer system and avionics computer system connection.