ANALISIS KESTABILAN DAN SIMULASI GERAK UAV FIXED WING

• Main Author: Nedhio Wibowo, Aqil
• Format: Final Project
• Language: Indonesia
• Online Access: https://digilib.itb.ac.id/gdl/view/43136
• Institution: Institut Teknologi Bandung

UAV (Unmanned Aerial Vehicle) MiniBe is one of ITB’s innovation strengthening research program. UAV MiniBe is small UAV that is designed for surveillance mission in the nation border and remote area. UAV MiniBe is a unique UAV because has only elevon (combined of elevator and aileron) as its control surface. In this final project, the stability of UAV MiniBe will be analyzed for motion on longitudinal dimension and lateral-directional dimension. The motion model that used to be analyzed is the motion model that resulted from linearization. After the stability have already analyzed, the automatic control systems will be designed. Those automatic control systems are Pitch Attitude Hold, Altitude Hold, Airspeed Hold, Yaw Damper dan Turn Coordinator. The automatic control systems could be stated succeed if it meets the MIL-STD-1797A standard design criteria. All automatic control systems that have been designed meet the design criteria and give satisfactory results.