#TITLE_ALTERNATIVE#

• Main Author: ERINSYAH (NIM 13600044), ZAKI
• Format: Final Project
• Language: Indonesia
• Online Access: https://digilib.itb.ac.id/gdl/view/11697
• Institution: Institut Teknologi Bandung

UAV (Unmanned Aerial Vehicle) X-1 is one of ITB's enhanced researches. The vehicle design processes were developed by the academic staff and undergraduate student from the aerospace engineering department, which consist of two stages; the preliminary design and the detailed design. Then the last stage breaks down into several design processes. One of them is the stability analysis and automatic flight control system design. This Tactical UAV is designed to meet the requirement for surveillance and target marking mission purposes as the reason why this UAV needs a reliable stability.<p> <br /> <br /> <br /> <br /> <br /> <br /> <br /> <br /> <br /> This thesis is based on an UAV X-1 stick fixed longitudinal and lateral-directional stability study. For the stability analysis, linear equations of motion were used. The automatic flight control systems design referred to the Lyapunov stability criteria. It was also include but not limited to the Altitude Hold System, the Airspeed Hold System, the Bank Hold, and the Turn Coordinator System. Optimal control with linier quadratic regulator method was used for the UAV X-1's flight control system design. Good design results were obtained that the results fulfill certain, predefined design criterion. The design results will be used as the basis of next development and implementation of the UAV X-1's flight control system. The automatic flight control system design will be simulated on a 3-dimension mode using the Virtual Reality software.