Abstract
This article deals with developing of Windows, Icons, Menus, Pointer interfaces and model based approach to mathematical modeling process of an unmanned air vehicle flight control system. Application of modern model-based technologies for critical onboard systems development is considered. The program for unmanned air vehicle-automatic flight control system control loop simulation and visualization is developed. Use of the proposed approach allows to facilitate unmanned air vehicle onboard systems software engineering, analyze and certification process. The article concludes with a status of current research activities on the topic and a summary of the benefits provided by this approach for developing Windows, Icons, Menus, Pointer interfaces for unmanned air vehicle automatic flight control system.
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