Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU201101745UpriorityCriticalpatent/UA60333U/en
Publication of UA60333UpublicationCriticalpatent/UA60333U/en
Channel for measurement of slant range to aircrafts with increased capabilities includes control element, block for control of deflectors, laser with pumping, modified selector of long modes, prisms for frequency of inter-mode beats, modified block of deflectors, switch for frequencies of inter-mode beatsand, 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 circuits, rectifiers, computer and block for representation of measuring information on slant range R to aircraft (A). After BA instead of multi-functional information block information block is included with increased capabilities with b – input of signal of tangent component of velocity (angular velocities) of A that is measured.
UAU201101745U2011-02-142011-02-14Channel for measurement of slant range to aircrafts with increased capabilities
UA60333U
(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 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 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 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 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 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 capability of aircraft identification for laser measuring system of a range test complex
urn:schemas-microsoft-com:office:smarttagsCHANNEL FOR MEASUREMENT OF SLANTRANGETO AIRCRAFTS FOR LASER INFORMATION AND MEASURING SYSTEMS WITH POSSIBILITY OF SEARCH AND IDENTIFICATION OF A/C