Abstract
This article shows the complexity of the integrated modular avionics design of on-board equipment of large aircraft. A modern image of the integrated modular avionics of on-board equipment is presented on the basis of existing samples. The design process of the software and hardware of the integrated modular avionics of on-board equipment is analysed. The main tasks of its design are listed. The existing and currently used methods for solving design problems of integrated modular avionics of on-board equipment are described. The level of the design automation process is reviewed. Modern means of computer-aided design are presented and their comparative analysis is carried out. An assessment of the existing level of design automation is given. The design stage with the lowest level of automation is defined. Appropriate conclusions are given.
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