Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU201001528UpriorityCriticalpatent/UA51060U/en
Publication of UA51060UpublicationCriticalpatent/UA51060U/en
Channel for measurement of radial velocity of aircrafts with possibility of identification of A has control element, block for control of deflectors, laser with pumping (Ln), modified block of deflectors, transmission optics, reception optics, broadband amplifier, resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, circuit “and”, counter, mixers, filter, former of measuring pulses, decoder, phase frequency auto-adjustment at frequency of inter-mode beats, control generator, support generator with support frequency, computer, block for representation of measured information on radial velocity R' of aircraft (A). After Ln modified selector of long modes (MSPM) is additionally included and- input of support frequencyfrom transmission laser (Ln + MSPM) and multi-functional information block is included, with b – input of signal of tangent component of velocity (angular velocities ) of A that is measured, for information intercommunication with A and in case if needed its identification.
UAU201001528U2010-02-152010-02-15Channel for measurement of radial velocity of aircrafts with possibility of identification of a
UA51060U
(en)
Channel for measurement of radial velocity of aircrafts with multi-functional information block and capability of identification of a for laser information and measuring system of a range test complex
Channel for measurement of radial velocities of aircrafts with use of frequencies of inter-mode beats and capability of aircraft identification for a range test complex
Channel for measurement of radial velocity of aircrafts with capability of formation and processing the aircraft image for laser measuring system of a range test complex
Channel for measurement of radial velocity of aircrafts with multifunctional longitudinal mode selector and increased capabilities for laser information and measuring system of a launch-site test complex
Channel for measurement of radial velocities of aircrafts with capability of aircraft identification for laser measuring system of a range test complex
Channel for measurement of radial velocity of aircrafts with moodified longitudinal mode selector and multifunctional information block for laser information and measuring system of a range test complex
Channel for measurement of radial velocity of aircrafts with multifunctional longitudinal mode selector and possibility of aircraft identification for laser information and measuring system of a launch-site test complex
Channel for measurement of radial velocity of aircrafts with enhanced information block and high functionality for laser information and measuring system of a range test complex
Channel for measurement of radial velocities of aircrafts with use of frequencies of inter-mode beats and capability of aircraft search and identification for a range test complex
Channel for measurement of radial velocity of aircrafts for laser information and measuring systems with possibility of formation and processing of image of a/c