UA83640U - Channel for measurement of aircraft attitude rate with use of intermodal frequencies and capability of aircraft identification for a range test complex
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Channel for measurement of aircraft attitude rate with use of intermodal frequencies and capability of aircraft identification for a range test complex
Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
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A channel for measurement of aircraft attitude rate with use of intermodal frequencies and capability of aircraft identification for a range test complex includes a control element, block for control of deflectors, pumped laser, longitudinal mode selector with frequency-division multiplexing, block of deflectors, transmitting optics, receiving optics, photo-detector, broadband amplifier, multi-functional information block with b – input of the signal of tangent component of the measured velocity (angular velocities) of the aircraft, resonance amplifiers adjusted to respective of intermodal frequencies, pulse formers, flip-flops "1"|"0", "AND" circuits, reversible counters, comparison circuits (CC) and- input of reference signals with frequencies of inter-mode beats () from transmitting laser. After the CC instead of electronic-digital computing machine an electronic computer is inctroduced.
UAU201302316U2013-02-252013-02-25Channel for measurement of aircraft attitude rate with use of intermodal frequencies and capability of aircraft identification for a range test complex
UA83640U
(en)
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 aircraft attitude rate with use of intermodal frequencies and capability of aircraft identification for a range 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 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 use of frequencies of inter-mode beats and capability of aircraft search and identification for a range test complex
Channel for measurement of angular velocities of aircrafts with enhanced information block 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 AIRCRAFT IDENTIFICATION FOR LASER INFORMATION AND MEASURING SYSTEM OF A RANGE TEST COMPLEX
Enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range 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 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 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 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 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 angular velocities of aircrafts with use of frequencies of inter-mode beats and capability of formation and processing the aircraft image for 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 additional scanning for a range test complex
Channel for measurement of aircraft attitude rates with television channel and aircraft recognition capability for a laser information and measuring system of a test range complex
Channel for measurement of slant range distance to aircrafts with use of intermodal frequencies and modified unit of deflectors with enhanced capability for 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 with capability of aircraft identification for laser measuring system of a range test complex
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 multifunctional information block for laser information and measuring system of a range 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