To the question for formation of a block-modular structure of the control system for unmanned aerial vehicles

The article discusses an approach to the formation of the basic structure of the control system for unmanned aerial vehicles, based on existing system solutions, typical specifications of the developer's boards. The characteristics of an unmanned aerial vehicle of both air and space class are given. General requirements for hardware and peripheral devices of unmanned aerial vehicles have been formed in accordance with their basic operating modes. Based on the obtained and generalized information about the developer's boards, the block-modular structure of the control system for unmanned aerial vehicles is presented. It includes all the main elements of the system and can be expanded by connecting additional boards. The advantage of this structure for debugging purposes is the presence of an FPGA on the development board.

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