Calculation and design of several scale models of a drone

Abstract

This thesis presents a detailed investigation into the design and analysis of multi-scale drones using MATLAB. The study is structured into three full chapters. The first chapter provides an in-depth overview of the history, background, and several types of drones. This exploration lays the foundation for understanding the evolution of drone technology and the principles that guide their design and operation. Chapter ? delves into the mathematical underpinnings of drone design. This chapter is divided into two parts: structural and performance parameters. It presents a thorough review of the equations and formulas used in the design process, providing a theoretical framework for the practical application in the subsequent chapter. Chapter ?, applies the theoretical knowledge from chapter two to a practical scenario. Using MATLAB, the structural and performance parameters of a chosen drone, the SKYEYE SIERRA, are calculated. Following this, MATLAB is used to recalculate these parameters for a drone with a different mass, noting the changes in performance and structure. The chapter also includes a study on the effect of the taper ratio on wing design and aerodynamics. The thesis concludes with the use of SolidWorks for a 3D design of a fixed-wing drone, bringing the theoretical calculations to life. This practical application validates the theoretical calculations and provides a tangible output of the design process. This research contributes to the field of mechanical engineering by providing a systematic and practical approach to drone design. The methodologies and findings presented in this thesis could guide future research and development in the field of UAVs, particularly in the design of multi-scale drones