Abstract:
The entire design and development process of a small fixed-wing Unmanned Aerial
Vehicle (UAV) made especially for Search and Rescue (SAR) missions is presented in this
thesis. Because of its adaptability, agility, and capacity to reach difficult or isolated areas,
unmanned aerial vehicle (UAV) technology has become a potentially useful instrument for
improving search and rescue (SAR) operations in recent years. Nevertheless, the
specialized elements required for successful SAR flights are frequently absent from current
commercial UAVs such as telemetry, radio transmitters etc. The primary objective of this
research is to bridge this gap by designing and building a custom UAV optimized for SAR
applications. The design process involves a systematic approach encompassing
aerodynamic analysis, structural design, payload integration. Furthermore, the integration
of sensors, including GPS and cameras, enables the UAV to effectively detect and locate
individuals or objects in challenging terrain and environmental conditions. To ensure that
the planned UAV prototype performs well and is reliable for real-world applications, it is
put through testing and assessment in our MIST field.
