Research on Design Method of Missile-borne Guidance Computer
Ying Zhou · Aeronautical Computing Technique · 2009
Missile-borne guidance computer is the core component of missile-borne guidance system.Design method of missile-borne guidance computer has been researched in two aspects-system structure and main technology in this paper.induction and summarization of missile-borne guidance computer system structure has been proposed by combined with missile guidance system and allocation model of guidance system.Main design method of missile-borne guidance computer has been explained from aspects of CPU and memory selection,bus technology,power technology.Design of integrated missile-borne guidance computer has been showed through an engineering example in the end.