Study of rocket launcher trajectories

Design and simulation of a rocket launcher trajectory, from launch platform to NEO. The present project consist in the development of a code to simulate the flight dynamics of a rocket launcher. Firstly, a mathematical model is made and then the equations of motion are integrated through a series of iterative algorithms in order to obtain the flight characteristics of the launcher. Special attention is paid to the computation of the flight path of the launcher, in an effort to retrieve the flight path presented in the launcher official documentation