Optimizing rocket trajectories: advanced mathematical modeling in MATLAB/simulink

Abstract

The article presents a methodology for generating a simulation Simulink model of a rocket. The use of the MATLAB/Simulink environment for simulating the flight of a rocket and calculating its aerodynamic characteristics is described in detail. The principles of forming blocks for calculating the parameters of a standard atmosphere, aerodynamic characteristics, power plant thrust, flight angles, altitude and flight range are described. The results of numerical experiments carried out using the MATLAB/Simulink environment are presented.