Synthesis of an Algorithm for Angle Measurement Channel of the Information-Measuring System of a Maneuvering Aircraft Given its Dynamic and Kinematic Characteristics

To solve the problem of improving the accuracy of electronic tracking devices of the information-measuring system of air traffic control, it is necessary to use state and observation models that take into account not only kinematic, but also dynamic characteristics of aircraft. Kinematic and dynamic characteristics more adequately describe aircraft movement models during various maneuvers, compared with aircraft movement models where this information is not taken into account. In this paper, the algorithms for the functioning of the angle measurement channel of the radar station of the information-measuring system for air traffic control are developed taking into account the kinematic and dynamic characteristics of the aircraft.