Modeling of the Flight Trajectory of Flying Objects

Abstract

In this paper, we describe a modeling approach for simulation of motion of flying objects. Such model can be used to examine the accuracy and resistance of radio-navigation systems against interference. The design of the simulation model is based on a mathematical description of the motion of a flying object in a geocentric coordinate system (ECEF - Earth - Centered, Earth - Fixed). The flight trajectory of flying objects consists of a straight section and two turns. We present the process of transforming the coordinates of the local motion of the flying object into a geocentric coordinate system in the topocentric coordinate system. We determined the initial coordinates of the flying objects (FO) from the real flight situation from flightradar24. The computer simulation was performed in the Matlab programming environment.