#TITLE_ALTERNATIVE#

• Main Author: JAMALLUBIS (NIM : 13613008), FATUH
• Format: Final Project
• Language: Indonesia
• Online Access: https://digilib.itb.ac.id/gdl/view/27223
• Institution: Institut Teknologi Bandung

Currently, the use of Unmanned Aerial Vehicle or UAV is prevalent in the field of military with a variety of flying missions including surveillance. Therefore, it is neccesary to develop an automatic control system and guidance to operate the UAV in accordance with its flight mission. <br /> <br /> <br /> <br /> XFW01 is one of the fixed wing UAV currently being developed in Indonesia that is designed to conduct surveillance missions. For the operation of XFW01, an autonomous flight control and guidance system is needed to manage the attitude, maneuver, and movement of both the longitudinal and the lateral-directional dimensions. <br /> <br /> <br /> <br /> In this final project, the design of automatic control system and guidance for XFW01 rides includes stability augmentation system, basic autopilot and flight path control. The control system is developed using a linear method that includes flying conditions at a speed range of 30 to 60 m / s and an altitude of 2000 to 5000 m. The designed control system is then evaluated by performing numerical simulations on varying flying conditions. The simulation results show that the built control system can improve the stability (with settling time 57 - 98.5% of the open-loop system settling time), keep the flying variable at a certain value (with steady state error 0.12-2%) and can manage the cross-flight rides (with 0-28.75% overshoot).