Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU201101340UpriorityCriticalpatent/UA60319U/en
Publication of UA60319UpublicationCriticalpatent/UA60319U/en
Channel for measurement of angular velocities of aircrafts for LVS with increased capabilities includes control element, block for deflector control, laser with pumping (Lp), block of deflectors, transmission optics, receiving optics, photodetector, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, triggers, circuits “and”, resonance counters, comparison circuits, computer, blocks for representation of information, ΔvMop – input of support signals with frequencies of inter-mode beats (ΔvMop, 2ΔvMop, 3ΔvMop, 6ΔvMop) from transmission laser and b – input of signal of measuring information on tangent component of velocity (angular velocities) of aircraft. After Ln instead of selector of long modes modified selector of long modes is included, and after BA instead of identification block a block with increased capabilities with input b is included.
UAU201101340U2011-02-072011-02-07Channel for measurement of angular velocities of aircrafts for lvs with increased capabilities
UA60319U
(en)
Channel for measurement of angular velocities of aircrafts with capability of aircraft identification for laser measuring system of a range test complex
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 for laser information and measuring systems with possibility of search and identification of aircrafts
Channel for measurement of angular velocities of aircrafts with capability of formation and processing the aircraft image for laser measuring system of a range 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 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 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 with modified longitudinal-mode selector and advanced functionality for laser information and measuring system of range test complex
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 multifunctional longitudinal-mode selector and possibility of aircraft identification for laser information and measuring system of a launch-site test complex