Informatics and Applications
2018, Volume 12, Issue 1, pp 18-30
COMPUTER-AIDED SYSTEM OF AIRCRAFT WEIGHT DESIGN
- L. L. Vyshinsky
- Yu. A. Flerov
- N. I. Shirokov
Abstract
The article is devoted to the problems of computer-aided weight design of aircraft. Weight and
mass-inertial parameters are one of the basic values that affect the performance characteristics of aircraft. The
informational basis of the system is the weight model of the aircraft. The paper describes the structure of the weight
model and its individual components. The program implementation of the system, which is executed within the
framework of the client-server architecture, is shown. The automated system of weight design is implemented using
the software tool complex "Project Generator" (GP technology), which was developed at the Computing Centre
of the Russian Academy of Sciences. The creation of information and computing systems within the framework
of the GP technology is based on the so-called "project approach," when the formal description of the system
automatically generates code for the client and server components of the system.
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[+] About this article
Title
COMPUTER-AIDED SYSTEM OF AIRCRAFT WEIGHT DESIGN
Journal
Informatics and Applications
2018, Volume 12, Issue 1, pp 18-30
Cover Date
2018-03-30
DOI
10.14357/19922264180103
Print ISSN
1992-2264
Publisher
Institute of Informatics Problems, Russian Academy of Sciences
Additional Links
Key words
math modeling; design automation; aircraft; weight design; weighting model; design tree; project
generator; code generation; client-server architecture
Authors
L. L. Vyshinsky  , Yu. A. Flerov , and N. I. Shirokov
Author Affiliations
A. A. Dorodnicyn Computing Center, Federal Research Center "Computer Science and Control" of the Russian Academy of Sciences, 40 Vavilov Str., Moscow 119333, Russian Federation
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