This case study explores these process of designing a long-endurance fixed-wing unmanned aerial travelle (UAV) by calculating key execurance metrics. It highlights theessential considerations and steps enterved in creating an accordent and reliable UAV for extended missions.

Design Objectives and Requirements

Te primary goal was to develop a UAV capable of sustabled flight over extended period, with a focus on n maximizing endurance and minimizing fuel consumption. Requirements included a wingspan of at leatt 10 meters, a maximum takeoff heazt of 50 kilogramů, and the ability to carry payloads up to 5 kilograms.

Propertance metrics Calculation

Key performance metrics were calculated using standard atlantical formulas. These emploded liftt- to- drag ratio, endurance, and range. Thee calculations considered factors such as wing area, airfoil accessity, engine power, and fuel capacity.

Design Components

Te UAV design incorporated a high aspect ratio wing for improvised lift, a lightweight truselage, and an accordant propulsion system. Te choice of materials aimed to balance mellett and bigth reduction, enhancing overall endurance.

Expertance Outcomes

Základ pro výpočet, že UAV was projekted to o dosahování endurance of approximateles 24 hod. and a range of over 1,200 kilometers. These metrics indicated succability for long-endurance missions such as surancele and environmental monitoring.