Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU201101729UpriorityCriticalpatent/UA60332U/en
Publication of UA60332UpublicationCriticalpatent/UA60332U/en
Channel for measurement of slant range to aircrafts with use of frequencies of inter-mode beats and increased capabilities includes control element, block for control of deflectors, laser with pumping, selector of long modes with multi-frequency separation of channels, prisms for frequency of inter-mode beats Δν, block of deflectors, switch for frequencies of inter-mode beats Δνand 2Δν, transmitting optics, receiving optics, photo-detectors, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse former, trigger "1"|"0", circuit “and”, counters, filter with given pass band, detector, differential optics, amplifier, filter, differential chains, rectifiers, computer and block for representation of measuring information on slant range R to aircraft (A). After BA instead of multi-functional information block there is included an information block with increased capabilities with b – input of signal of tangent component of velocity (angular velocities) of A that is measured.
UAU201101729U2011-02-142011-02-14Channel for measurement of slant range to aircrafts with use of frequencies of inter-mode beats and increased capabilities
UA60332U
(en)
Channel for measurement of slant range distance to aircrafts with use of frequencies of inter-mode beats and feasibility of search and identification of an a
Channel for measurement of slant range to 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 slant range to aircrafts with use of frequencies of inter-mode beats and capabilityof aircraft identification for a range test complex
Channel for measurement of slant range distance to aircrafts with modified longitudinal-mode selector and advanced functionality for laser information and measuring system of range test complex
Channel for measurement of slant range to 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 slant range to aircrafts with multi-functional information block and capability of aircraft identification for laser information and measuring system of range test complex
Channel for measurement of slant range to aircrafts for local information computer networks with enlarged set of polarization signs for identification of an aircraft
Channel for measurement of slant range to aircrafts with multichannel longitudinal mode selector and additional scanning for laser information and measuring system of a launch-site test complex