Abstract In this paper, a research and development version of the computer-aided system of mass tensometry (SMT) for conduction of aircraft and rocket-space equipment vibration tests is considered. A technique of the system design and development that combines the advantages of the system and process approaches when using the modern element base around the high-performance integral microcircuits is a distinctive feature in this research and development problem solution. We describe the architecture and structure of the advanced computer-aided SMTs and present data on its basic components desigtn. Also determined are the list and functional parameters of ratio-measuring network modules as well as the scheme of their connection to the test object and the local computer network of the enterprise.
Research and development version of computer-aided system of aircraft and rocket-space equipment vibration tests
Russian Aeronautics (Iz VUZ) ; 55 , 2 ; 217-222
2012-04-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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