1. Research and development version of computer-aided system of aircraft and rocket-space equipment vibration tests
- Author
-
V. A. Komkov, Yu. V. Mozgovoi, V. F. Korolev, and V. V. Vasilevskii
- Subjects
Scheme (programming language) ,Structure (mathematical logic) ,Engineering ,business.product_category ,business.industry ,Process (computing) ,Aerospace Engineering ,Control engineering ,Vibration ,Development (topology) ,Rocket ,Computer-aided ,Systems design ,business ,computer ,computer.programming_language - 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.
- Published
- 2012