Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU201101747UpriorityCriticalpatent/UA60335U/en
Publication of UA60335UpublicationCriticalpatent/UA60335U/en
Channel for measurement of angular velocities of aircrafts with increased capabilities includes control element, block for control of deflectors, laser with pumping, modified selector of longitudinal modes, modified block of deflectors, transmitting 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 ∆ν– input of support signals with frequencies of inter-mode beasts (∆ν, 2∆ν, 3∆ν, 6∆ν) from transmitting laser. After BA in place of multifunctional information block information block with increased capabilities is included, with b - support of signal of tangent component of velocity (angular velocities) of aircraft that is measured.
UAU201101747U2011-02-142011-02-14Channel for measurement of angular velocities of aircrafts with increased capabilities
UA60335U
(en)
Channel for measurement of angular velocities 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 angular velocities of aircrafts with multifunctional information block 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 search and identification of aircrafts
Channel for measurement of angular velocities of aircrafts with multichannel longitudinal mode selector and additional scanning for laser information and measuring system of a launch-site test complex
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 to aircrafts with multifunctional longitudinal mode selector and capability of formation and processing of an aircraft image for laser information and measuring system of a launch-site 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
Channel for measurement of angular velocities of aircrafts for local information computer networks with enlarged set of polarization signs for identification of an aircraft
Channel for measurement of angular velocities of aircrafts with modified longitudinal mode selector and multifunctional information block for laser information and measuring system of a range test complex