DESIGN AND IMPLEMENTATION OF DIGITAL PID CONTROL SYSTEM FOR ROCKET MODEL YAW CONTROL FIN (RUDDER) AND PITCH CONTROL FIN(ELEVATOR)

• Main Author: AGUSTIAN (NIM 13202084), ERIC
• Format: Final Project
• Language: Indonesia
• Online Access: https://digilib.itb.ac.id/gdl/view/10353
• Institution: Institut Teknologi Bandung

<p align="justify">PID controller is a control technique which frequently used in rocket movement control because its ability to improve system response characteristic and fast computation process time.<p align="justify"><p>This final project report will discuss about design and implementation of digital PID control system for rocket movement. Rocket movement is determined only by yaw control fin (rudder) and pitch control fin (elevator). Main objective for this system control is rocket can make an automatic movement in order to have a same position with target object.<p align="justify"><p>Control system input are target position and velocity that measured from camera center point which taken from target identification system. This input then compared with rocket position and velocity that realizing closed loop control system. Testing stage for whole system uses a rocket model that placed on wind tunnel. The testing result show that rocket succesfully following moving target with average error rate 1,52 degrees for yaw movement and 0,97 degrees for pitch movement. <br />