The design and analysis of a fixed-wing unmanned aerial vehicle (UAV) with a primary purpose of conducting search and rescue operations are the primary focus of this study. This project begins with a careful analysis of the necessary dimensions and weight constraints. According to accepted industry standards, these criteria form the basis for the theoretical computation of a number of flight-related dimensions, such as flight length, wing length, wing profile, width, and height.The SolidWorks software is then used to generate a detailed model based on these design and dimensional specifications. The next stage involves simulating the UAV’s performance using CFD software. This project’s main objective is to evaluate the drone system’s aerodynamic characteristics, taking into account important factors like lift, drag, moment, and thrust. The study uses CFD simulations, 3D modelling, and theoretical calculations to thoroughly assess the aerodynamic performance of the UAV.
Aim
Design of a man-portable fixed-wing drone and launching system for search and rescue operations.
Objectives
- Background research on fixed wing drones and existing launch systems and product design specification for the complete system
- Detailed design on the fixed-wing drone fuselage and wing deployment mechanism
- Detailed design of the launch platform with a focus on portability and rapid deployment
- Analysis and calculations to determine to performance characteristics of the drone and launch system
- Optimisation of the launch system to meet the PDS based on analysis results
- Optimisation of the drone to improve overall aerodynamic performance and payload capacity based on analysis results
