Modelling and simulation of surface-to-surface missile general platform

Abstract

In this paper, a general platform of a surface‐to‐surface missile model is presented. An accurate missile system model was made with consideration of the rigid body dynamics in space with six degrees of freedom and equation of motion starting from Newton second law to the non‐linear state space model of the missile. Computer simulations have been executed using the MATLAB / Simulink software. Verification of the system model has been made.