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Automation of the inner design of the aircraft
Author(s) -
Mikhail Yu. Kuprikov,
Leonid Markin
Publication year - 2019
Publication title -
incas buletin
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.282
H-Index - 10
eISSN - 2247-4528
pISSN - 2066-8201
DOI - 10.13111/2066-8201.2019.11.s.13
Subject(s) - computer aided design , computer science , automation , interface (matter) , software , cad , graphics , computer graphics , visualization , task (project management) , electronic design automation , geometric modeling , engineering drawing , systems engineering , software engineering , computer graphics (images) , engineering , embedded system , programming language , artificial intelligence , mechanical engineering , operating system , bubble , maximum bubble pressure method
The task of forming the wind-swept surface according to the results of the aircraft’s inner design is described. The approach of the integration of natural and virtual prototyping in the design of equipment compartments is substantiated. Such approaches open up new possibilities for creating intelligent composition algorithms that eliminate the "blind search". For the practical implementation of these approaches, it is necessary to link the appropriate software to standard geometric modeling systems in the form of additional computational modules. Preparing the aircraft for design automation complicates the mathematical description of geometric models of placed objects, increases the complexity of their visualization in modern computer graphics systems and the need to create an additional interface between new geometric models and common CAD systems (SolidWorks, AutoCAD, COMPAS, etc.).

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