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Background. One of the important tasks in the design of a quadrocopter is the development of an information- measuring and control system of a quadrocopter. Materials and methods. This system should provide quadrocopter years with the maximum reduction of external disturbances. Since the information-measuring and control system includes inertial sensors, which significantly degrade the characteristics of the control loop of the spacecraft. To solve these problems, this article considers the problem of synthesizing a control loop of one of the coordinates in the horizontal plane of an information-measuring and control system with a quadrocopter state identifier. The aim of the work is to improve the quality of control of the movement of the quadrocopter based on the introduction of state identifiers in the information-measuring and control system of the quadrocopter. Results and conclusions. This system serves for the capable monitoring of various objects of the quadrocopter and its ability to overcome disturbances in uncertain situations.