DocumentCode :
2227021
Title :
Missile guidance processor software development-a case study
Author :
Bond, R. ; Bemrich, S. ; Connelly, J. ; Pendergrass, G. ; Hulsey, J.
Author_Institution :
LTV Missiles & Electron. Group, Dallas, TX, USA
fYear :
1988
fDate :
6-8 Dec 1988
Firstpage :
60
Lastpage :
68
Abstract :
A case study of a near-complete implementation of a real-time software system is presented. The software implements a missile guidance processor control system. The languages of implementation are C and assembler, targeted to an MC68020 central processing unit with an MC68881 floating-point coprocessor and an HD63450 direct memory access controller. Modern software engineering practices were used, including information hiding, separation of concerns, modularity, adaptability, and incremental development. Performance considerations required optimizing the use of hardware systems and minimizing run-time support
Keywords :
military computing; missiles; real-time systems; software engineering; C; HD63450 direct memory access controller; MC68020 central processing unit; MC68881 floating-point coprocessor; adaptability; assembler; incremental development; information hiding; minimizing run-time support; missile guidance processor control system; modularity; real-time software system; Assembly; Central Processing Unit; Centralized control; Control systems; Coprocessors; Missiles; Process control; Real time systems; Software engineering; Software systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Real-Time Systems Symposium, 1988., Proceedings.
Conference_Location :
Huntsville, AL
Print_ISBN :
0-8186-4894-5
Type :
conf
DOI :
10.1109/REAL.1988.51101
Filename :
51101
Link To Document :
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