Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Харьковский Университет Воздушных Сил Имени Ивана КожедубаfiledCriticalХарьковский Университет Воздушных Сил Имени Ивана Кожедуба
Priority to UAU201101994UpriorityCriticalpatent/UA60347U/en
Publication of UA60347UpublicationCriticalpatent/UA60347U/en
Channel for measurement of angular velocities of aircrafts with BSPM and capability of identification of A includes control element, block for control of deflectors, laser with pumping, multi-functional selector of longitudinal modes, 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 Δv- input of support signals with frequencies of inter-mode beats (Δv, 2 Δv3Δv, 6 Δv) from transmission laser. After BA in place of information block multi-functional information block is included, with b – input of signal of tangent component of velocity (angular velocities) of A that is measured.
UAU201101994U2011-02-212011-02-21Channel for measurement of angular velocities of aircrafts with bspm and capability of identification of a
UA60347U
(en)
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 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 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 increased capabilities for laser information and measuring system of a launch-site test complex
Channel for measurement of aircraft attitude rate with use of intermodal frequencies and capability of aircraft identification for a range test complex
Channel for measurement of angular velocities of AIRCRAFTS WITH MODIFIED LONGITUDINAL-MODE SELECTOR 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 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 use of frequencies of inter-mode beats and capability of search, formation and processing the aircraft image for 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 use of frequencies of inter-mode beats and additional scanning for a range test complex