Design and Fabrication of a Solar Power Unmanned Aerial Vehicle
Fundamentals of unmanned aerial vehicle has been designed and runs for quite a while. An approach that involving
in designing aircraft to meet emission constraints while minimizing cost. These include the definition of the mission of the
aircraft and various requirements, such as performance, handling, manufacturing, certifiability, upgradability,
maintainability, and many others. Experiments have been carried out to assess the performance of the unmanned aerial vehicle
which runs on solar power. The main objective of this paper is releasing mechanism where we can attach a load in the
unmanned aerial vehicle and by the help of a remote controlled device we can drop the load anywhere. In addition to
developing concepts, another objective is used in this aircraft as a surveying purpose. A high power lens (live steaming
camera) is attached to capture images and videos of the survey field. This can help to detect the enemy in the defence purpose.
A wireless remote control is used to fly the aircraft and a feedback battery indicator mechanics is also developed. A lithium 3
cell battery is incorporated with the system.