The method of syntheses of hardware and software complexes for unmanned aerial vehicles flight control systems development

The method of design of hardware and software complexes for unmanned aerial vehicles fl ight control systems development, used by developers during the design and testing, is presents. The results of creation of a simulation model of short-range type unmanned aircraft flight dynamics, means of interfacing simulation models and flight control hardware and specialized software development, is considered. The recommendations on the use of the developed models and programs in the problems of the synthesis of unmanned aerial vehicles fl ight control systems are given.