Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU201006294UpriorityCriticalpatent/UA52933U/en
Publication of UA52933UpublicationCriticalpatent/UA52933U/en
Channel for automatic following of aircrafts in direction with possibility of identification of a for LVS has control element, block for control of deflectors, laser with pumping, selector of long modes, block of deflectors, transmission optics, reception optics, photodetector, broadband amplifier (SP), resonance amplifiers adjusted to respective frequencies of inter-mode beats, detectors, filters, pulse formers, triggers ("1"|"0"), circuits “and”, delay lines, counters, digital-analog transformers, low frequency filters, amplifiers (filters)( of error signal, executive mechanisms, computer and a – input of support signal with frequencyvof transmission laser, b – input of signal from channel of evaluation of tangent component of velocity (angular velocities) of aircraft for adjustment of error of coincidence by angles. After SP there is additionally included block for identification with input b.
UAU201006294U2010-05-252010-05-25Channel for automatic following of aircrafts in direction with possibility of identification of a for lvs
UA52933U
(en)
Channel for automated tracking of aircrafts by direction for laser information and measuring systems with possibility of search and identification of a/c
Channel for automated tracking of aircrafts by direction for laser information and measuring systems with possibility of formation and processing of image of a/c
Channel of automatic aircraft tracking by direction with multichannel longitudinal mode selector and additional scanning for laser information and measuring system of a launch-site test complex
Channel for automatic aircraft tracking in direction with modified longitudinal-mode selector and advanced functionality for laser information and measuring system of range test complex