Abstract
The deployment of battery powered Unmanned Aerial Vehicle (UAV) is constrained mainly due to its lack of range per single charge. In this paper, load modelling of an UAV at different stages like take-off, level flight and landing at different conditions like constant altitude - variable speed, constant speed - variable altitude, constant altitude and speed - variable take-off and landing angle; has been derived. Analysis of Thrust and Power requirement of UAV at different stages has been discussed in the paper. This analysis can be used for the selection of components and battery required for the UAV, depending upon the particular application. This can also be used in power estimation and flight planning accordingly.
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