strong>Design and Fabrication of Fixed-Wing Unmanned Aerial Vehicle (UAV) With Dropping Mechanism
Authors:-Assistant Professor Mr.N.Kawin, P.Tharun, VP.Vaishnav, M.Yogesh
Abstract-Unmanned Aerial Vehicles (UAVs) which are also known as Drones are aircrafts without a human pilot on board, -usually controlled by a ground-based controller and a communication system or by the ability of being programmed with various degrees of autonomy. The reason of the rapid advancement on drone technology is the need for more precision, accessibility, safety and cost effectivity in many fields. They currently lack the flexibility and adaptability of manned aircrafts. By some measures, 80% of the global drone industry revenues are related to agriculture, in some way. (R1) Unmanned aerial vehicles (UAVs) are one of the most promising innovative technologies invented in recent years to promote precision agriculture and smart farming. UAVs can not only reduce labour requirements but also increase production output, reduce the use of pesticides, and protect the environment. The main objective of our project is to design an aircraft that is capable of lifting as much weight as possible while taking into account the available power and aircraft’s length, width, and height requirements. A special attention has been devoted to Dropping Mechanism of the payload which can help us in gaining more ways to deliver the goods we need. The following report is a synopsis of the design process, Fabrications, component selection and Fly with maximum payload.
