Integrated sensor system for controlling altitude–velocity parameters of unmanned aircraft plane based on the vortex method

Abstract

The paper considers the original scheme, algorithms for the formation and processing of time–frequency primary informative signals, and determination of the altitude–velocity parameters of unmanned aircraft planes in channels of integrated sensor system with one receiver of primary information. The competitive advantages of the offering sensor system for controlling the altitude–velocity parameters are provided, which determine the prospects for its use on unmanned aircraft planes of various classes.