Abstract
The paper deals with questions of developing the advanced unmanned aerial vehicle landing system. The article considered the existing unmanned aerial vehicle landing systems as well as proposed the unmanned aerial vehicle polarimetric landing system, which consists of two parts: the ground-based block and the on-board block. The proposed system, potentially, can increase the accuracy and sensitivity of determination the unmanned aerial vehicles deviation from the landing trajectory and its attitude. Unmanned aerial vehicle polarimetric landing system allows providing landing on non-horizontal and moving plane of landing. Also considered block diagrams of the onboard and ground polarimetric device. In article were given result of the mathematical modeling of measurement channel.
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