Onboard System for Correcting the Flight Range of an Unguided Missile
The purpose of this work is to obtain the simplest mathematical description that adequately predicts the reaction of a physical system to all input data. Within the framework of this work, a system of ordinary equations of the trajectory of a rocket projectile relative to the Earth is established, taking into account the aerodynamic drag and changes in body mass. The simulation of the flight of a rocket projectile in the Matlab Simulink environment is carried out. The simulation allows you to configure the parameters of the flight correction system without conducting a test with a real object. A full-size mathematical model of the flight of a rocket projectile equipped with a range correction system is presented. The correction of the flight range allows us to solve the problem of the dispersion of projectiles of rocket artillery systems