Synthesis of Electronic Tracking Systems Considering Aircraft Movement Dynamics
The paper describes the ranging channel algorithm of information measurement system, using the dynamic characteristics of the aircraft. The authors justify the choice of state models based on kinematic and dynamic characteristics of the flying aircraft (AC), and observation models given the radiolocation information from ground radar stations and non-radar information from the on-board measuring instruments. A distance-measuring device is modelled on a computer, tracking the AC performing a fragment of a “small box” maneuver. The results of the study of the algorithm of information-measuring system are given.