Synopsis

This report outlines the design of a UAV for disaster response, specifically for delivering essential items to disaster-stricken areas. The report identifies the need for a fast and effective UAV service to overcome physical barriers such as flooding. The model assumes that storm conditions have ceased and wind conditions are negligible. The report covers four main sections: payload, propulsion, navigation, and body design. The payload section outlines the calculation process for determining the maximum payload capacity and recommends the use of a winch system for delivery. The propulsion section discusses the calculations for vertical ascent and horizontal movement of the UAV, with an estimated travel distance of 2km to the rescue site. The navigation section covers the navigation system used for reconnaissance missions and how the UAV uses trilateration to determine its position. The body design section describes the mechanics and body design of a multirotor octocopter UAV, made from carbon fiber and aircraft-grade aluminum. The report concludes that the model relies on several assumptions and expects an error of approximately 10%.