Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU201103365UpriorityCriticalpatent/UA61338U/en
Publication of UA61338UpublicationCriticalpatent/UA61338U/en
Channel for measurement of angular rate of aircrafts with additional scanning and possibility of identification of A includes control element, block for control of deflectors, laser with pumping, multi-functional selector of long modes, modified block of deflectors, transmission optics, receiving optics, photodetector, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, triggers "1"|"0", circuits “and”, reversing counters, comparison circuits, computer and Δv– input of support signals with frequencies of inter-mode beats (Δv, 2Δv, 3Δv, 6Δv) from transmission laser. After BA instead of information block multi-functional information block is included with b – input of signal of tangent component of velocity (angular velocities) of aircraft that is measured.
UAU201103365U2011-03-212011-03-21Channel for measurement of angular rate of aircrafts with additional scanning and possibility of identification of a
UA61338U
(en)
Channel for measurement of angular velocities of aircrafts for laser information and measuring systems with possibility of search and identification of aircrafts
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Channel for measurement of angular velocities of aircrafts with capability of aircraft identification for laser measuring system of a range test complex
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Channel for measurement of angular velocities of aircrafts with MODIFIED longitudinal-mode selector and capability of formation and processing the AIRCRAFT image for LASER information and measuring system of a range test complex
Channel for measurement of angular velocities of aircrafts with use of frequencies of inter-mode beats and capability of search, formation and processing the aircraft image for a range test complex
Channel for measurement of angular velocities of AIRCRAFTS WITH MODIFIED LONGITUDINAL-MODE SELECTOR AND CAPABILITY OF AIRCRAFT IDENTIFICATION FOR LASER INFORMATION AND MEASURING SYSTEM OF A RANGE TEST COMPLEX
Channel for measurement of angular velocities of aircrafts for laser information and measuring systems with possibility of formation and processing of aircraft image