The purpose of this thesis is to analyse and subsystem integration of Unmanned Aerial Vehicle (UAV). The analysis part of the thesis is divided into two section: numerical and software analysis. The numerical analysis is done by using Matlab program as the platform to perform the analysis for the aerodynamic and static stability. The Matlab program for the static stability is wrote based on the book Introduction to Flight by John D. Anderson Jr. The software analysis is use the Computerised Environment for Aircraft Synthesis and Integrated Optimisation Methods (CEASIOM). The CEASIOM analysis go through several module to obtain the result for the thesis: AcBuilder, Weight and Balance, Aerodynamics Model Builder, Propulsion, and Simulation and Dynamic Stability Analyser. The second part of the thesis is about the subsystem integration of the UAV. The subsystem integration is divided into two section: the control system and the FPV system. Basically, the control system section is done by integrate the subsystems: battery, servo, esc and motor to function properly. The second section is the First Person View (FPV) system, the integration of the video camera with the video transmitter for the on-board system and video receiver with the personal computer for the ground system.
Analysis and Subsystem Integration_Mohamed Affanzi Abdullah_A2_2014_NI