yatinsd / missile-simulation

Modelling and Simulation Assignment - Autonomous Vehicle Dynamics and Control, Cranfield University

This repository contains a MATLAB/Simulink simulation software for the flight dynamic simulation of an transsonic missile system.

Discription

This Software Project was created as part of the Modeling and Simulation module which was held by Dr. Chang-Hun Lee, Korean Advanced Institute of Science and Technolgy for the students of the master course Autonomous Vehicle Dynamics and Control at Cranfield University. This repository contains MATLAB/Simulink software in which the flight dynamic model of a transsonic missile has been developed and analyised.

The problem presented in this assignment was the modelling and simulation of a transsonic missile model in MATLAB/Simulink. The aerodynamic and airframe information were provided by the lecturer. This work was mainly focusing on modelling the system and to analyse the flight dynamics and response behaviour of the missile. Furthermore, a required control law was adapted for the modelled system. For that goal suitable algorithm and fitting SIMULINK models should be created and afterwards discussed.

Structure

This assignment aims to model and simulate the flight dynamic behaviour of a specified missile by using MATLAB/Simulink. This general aim can be separated into six primary objectives:

• Describing the general model conceptualisation
• Deviate the flight dynamic equations of a missile
• Establishing the Simulink model of the missile
• Verification of the created SIMULINK model
• Searching Trimming states of the missile
• Linearisation of flight dynamic equations
• Analysing the Stability behaviour of the missile
• Designing an Autopilot for the missile