| abstract |
An exemplary embodiment includes a landing platform having a housing and a power terminal adapted to extract electrical power from a power source. The landing platform further comprises an electroconductive landing terminal which is dorsal to the housing and configured such that, in a landing state of an aerial vehicle, the landing terminal contacts a plurality of electrical contacts disposed ventrally with respect to a fuselage of the aerial vehicle. The landing terminal is adapted to transfer electrical energy drawn from the power supply terminal to the air vehicle through the electrical contacts in the landing state of the air vehicle. |