UA102349U - Channel of automatic tracking of aircrafts by direction for mobile combined measuring system - Google Patents

Channel of automatic tracking of aircrafts by direction for mobile combined measuring system

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Publication number
UA102349U
UA102349U UAU201504056U UAU201504056U UA102349U UA 102349 U UA102349 U UA 102349U UA U201504056 U UAU201504056 U UA U201504056U UA U201504056 U UAU201504056 U UA U201504056U UA 102349 U UA102349 U UA 102349U
Authority
UA
Ukraine
Prior art keywords
channel
filters
aircrafts
measuring system
automatic tracking
Prior art date
Application number
UAU201504056U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Олексій Володимирович Коломійцев
Ігор Іванович Сачук
Геннадій Васильович Альошин
Замір Забірович Закіров
Олександр Леонідович Кузнєцов
Андрій Михайлович Носик
Сергій Володимирович Орлов
Владислав Олександрович Павлій
Дмитро Васильович Руденко
В'ячеслав Федорович Третяк
Original Assignee
Харківський Університет Повітряних Сил Імені Івана 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 Харківський Університет Повітряних Сил Імені Івана Кожедуба filed Critical Харківський Університет Повітряних Сил Імені Івана Кожедуба
Priority to UAU201504056U priority Critical patent/UA102349U/en
Publication of UA102349U publication Critical patent/UA102349U/en

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Abstract

A channel of automatic tracking of aircrafts by direction for mobile combined measuring system comprises a control element, unit for controlling deflectors, pumped laser, longitudinal mode selector, modified unit of deflectors, transmitting optics, optical-electronic module formed of television and infrared channels, receiving optics, photo-detector, broadband amplifier, resonance amplifiers adjusted to corresponding intermodal frequencies, detectors, filters, pulse formers, 1|0 flip-flops, AND gates, delay lines, counters, analog-to-digital converters, low pass filters, error amplifiers (filters), executive mechanisms, electronic computing machine and α - input of reference signal with frequency EMBED Equation.3 of transmitting laser, σ - input of the signal from the channel of evaluation of aircraft circumferential velocity (attitude rates). Additionally a gyro-stabilized platform is incorporated.
UAU201504056U 2015-04-27 2015-04-27 Channel of automatic tracking of aircrafts by direction for mobile combined measuring system UA102349U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201504056U UA102349U (en) 2015-04-27 2015-04-27 Channel of automatic tracking of aircrafts by direction for mobile combined measuring system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201504056U UA102349U (en) 2015-04-27 2015-04-27 Channel of automatic tracking of aircrafts by direction for mobile combined measuring system

Publications (1)

Publication Number Publication Date
UA102349U true UA102349U (en) 2015-10-26

Family

ID=54773834

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201504056U UA102349U (en) 2015-04-27 2015-04-27 Channel of automatic tracking of aircrafts by direction for mobile combined measuring system

Country Status (1)

Country Link
UA (1) UA102349U (en)

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