Attitude Control of Rocket via Thrust Vector Control Technique

Abstract

Rocket control was primarily complex and aimed at one objective which is maintaining flight path directory and an advanced one which is an automotive flight mission flexible to different delivered inputs from communication guidance navigation and changing orbits. Thus, making a control model of rockets will impact industrial sectors in many ways from satellite emplacement to helping researchers internet connection and military purposes; thrust vector control TVC is the general technique of rocket control thus in this thesis we are willing to demonstrate the attitude control of small scaled rocket with linear control and this work will be in 3 chapters. Chapter 1 dedicated for rocket history and the TVC in general. Chapter 2 about the mathematical model for the rocket dynamics and will be on implementing a linear control method for our dynamical model. Chapter 3 will be about experimentation controlling two degree of freedom “pitch and yaw”.