Abstract
The study analyzes the functional principles and approaches to determine the main features of the software used for the aircraft operation. Theoretical aspects of creating the software architecture in the field of civil aviation based on modern approaches to the automation systems development are described. The main regulatory requirements for organizational and technological support of the process of developing software solutions in the field of civil aviation are considered. The peculiarities of the V-shaped model of aircraft operation software development are determined. The documentation for the software should consist of a description of the main blocks of the program, the order of modules integration, system architecture and other formalities that reflect the results of the source code. Based on the described approach to the development of a software package for the aircraft operation, the vision and criteria of the cycle of development of information solutions in the field of civil aviation is created. Depending on the functional characteristics of the obtained software solutions, the final documentation is compiled, which also contains the results of its testing under the conditions of pre-industrial operation. Modern avionics systems have a modular multilevel structure. At the same time, the classical approaches to the development of aircraft operation systems are inefficient, which requires the development of a specific methodology that takes into account the studied subject area. This is due to the need to integrate software for the operation of civil aircraft with third-party software and hardware used for flight control.
Highlights
Many flight control systems in civil aviation have been successfully developed with the help of special equipment and software
Substantiation of the basic principles of software in avionics is evolving as research is conducted and experience is gained in automation and software support architecture
The development process is controlled by different groups of people for different tasks and at different levels of creation and implementation of the software product and its components
Summary
Many flight control systems in civil aviation have been successfully developed with the help of special equipment and software. Functional principles of software development and operation determine the analysis and development of various solutions for improvement and innovation of aviation products and aviation enterprises in particular. Classical approaches to the development of aircraft operation systems are inefficient, which requires the development of a specific methodology that takes into account the subject area under study. This is due to the need to integrate software for the operation of civil aircraft with third-party software and hardware systems used for flight control. The following practically significant constructions and components are of great importance in this context: the software architecture and the subsequent V-shaped model, as well as the unity and integrity between the structural components
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