Development of the information-logical scheme for Earth remote sensing small spacecraft

The paper considers a modern approach to the design process of the Earth remote sensing small spacecraft using information technologies. The onboard composition is considered and a block diagram of the Earth remote sensing small spacecraft is developed in order to develop an information-logical diagram of internal interaction. The developed scheme allows, already at the design stage, by setting the necessary characteristics, to quickly form the onboard composition of any spacecraft, taking into account the efficiency of the joint operation of certain devices, as well as significantly reduce the time for design work on the development of small spacecraft.