Review of Present Systems and Costs of Conceptual Designs of UAV:s for Humanitarian Relief Missions.

Abstract: A study of the viabliness of a UAV for humanitarian relief missions has been done. With an aeronautical model fulfilling humanitarian logistics has then the manufacture and operational life-cycle costs as well as the present air jurisdiction. In contrast to this has also an evaluation of the empty weight conceptual estimation equation been reviewed and what conditions fairly describes the sizing of a UAV. The study finds there’s a technical possibility, economic plausibility but a need for legal development. The coefficients which are sufficient to estimate the empty weight ratio are the Home built aircrafts and powered sailplane. The study concludes what present off-the-shelf systems that might be suitable to sustain humanitarian relief missions.