Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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Priority to UAU200904601UpriorityCriticalpatent/UA43787U/en
Publication of UA43787UpublicationCriticalpatent/UA43787U/en
Channel for automated tracking aircrafts in direction with additional scanning has control element. block for control of deflectors. Laser with pumping (Ln), transmission optics, receiving optics, photodetector, broadband amplifier, resonance amplifiers adjusted to respective frequencies of inter-mode beats, detectors, filters, pulse formers, triggers ("1"|"0"), circuits "and", delay lines, counters, digital-analog transformers, low frequency filters, amplifiers (filters) of error signal, executive mechanisms, electronic-digital computer and a – input of support signal with frequency Δνof transmission laser, b – input of signal from channel of evaluation of tangent component of velocity (angular velocities) of aircraft (A) for adjustment of error of coincidence by angle, information block for information interconnection with A. After Ln multi-channel selector of long modes and modified block of deflectors are included.
UAU200904601U2009-05-082009-05-08Channel of automated tracking of aircrafts in direction with additional scanning
UA43787U
(en)
Channel of automatic aircraft tracking by direction with multichannel longitudinal mode selector and additional scanning for laser information and measuring system of a launch-site test complex
Channel for automated tracking of aircrafts by direction for laser information and measuring systems with possibility of search and identification of a/c
Channel for automated tracking of aircrafts by direction for laser information and measuring systems with possibility of formation and processing of image of a/c
Channel for automated tracking aircrafts by direction with use of frequencies of inter-mode beats and capability of search, formation and processing the aircraft image for a range test complex
Channel of automated tracking of aircrafts by direction with multifunctional longitudinal mode selector and increased capabilities for laser information and measuring system of a launch-site test complex
Channel for automatic tracking of aircrafts by direction 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 automated tracking of aircrafts by direction with use of frequencies of inter-mode beats and feasibility of search and identification of an a