Description: The multifunction laser informatively-measuring system (LIMS) for a ground proof-of-concept complex, that is built on the use of frequency-sentinel method (FSM) of search, recognition and measuring of parameters of motion of aircraft (А) and optician-electronic module, is offered. Multifunction LIMS carries out angular autoaccompaniment of А in the wide range of distances at the simultaneous goniometry of azimuth and place sloping distance, radial and tangential (angular) speeds and has in the composition a televisional channel for realization of objective control real-time. Presented results of estimation of точностних descriptions of measuring channels and chart-technical decisions of construction of LIMS. Exposed essence of angular autoaccompaniment of А, measuring of him six parameters of motion, realizations of objective control and, after a necessity, search of А, recognition and delivery of commands of management of LIMS.
Keywords: multifunction laser informatively-measuring system, frequency-temporal method of measuring, aircraft