Abstract:
The article is devoted to the description of the information model of the weight profile of an aircraft. The weight profile of an aircraft is understood as a set of interconnected information objects containing a description of the structure, parameters, and characteristics of the aircraft sufficient for weight calculations, weight analysis, and weight control at all stages of the product life cycle. The described information model can serve as the basis for a scheme of a database in the development of automated weight design systems. In the article, the weight model of an aircraft is described in terms of network data structures.