UA92687U - Channel for automatic tracking of aircrafts by direction with capability of identification of a for a combined laser system - Google Patents

Channel for automatic tracking of aircrafts by direction with capability of identification of a for a combined laser system

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Publication number
UA92687U
UA92687U UAU201403586U UAU201403586U UA92687U UA 92687 U UA92687 U UA 92687U UA U201403586 U UAU201403586 U UA U201403586U UA U201403586 U UAU201403586 U UA U201403586U UA 92687 U UA92687 U UA 92687U
Authority
UA
Ukraine
Prior art keywords
channel
filters
identification
aircrafts
capability
Prior art date
Application number
UAU201403586U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Алексей Владимирович Коломийцев
Игорь Иванович Сачук
Геннадий Владимирович Певцов
Сергей Николаевич Власик
Сергей Иванович Кливец
Ярослав Николаевич Кожушко
Дмитрий Сергеевич Комин
Сергей Владимирович Орлов
Виталий Васильевич Посохов
Елена Геннадиевна Толстолузская
Original Assignee
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 Кожедуба filed Critical Харьковский Университет Воздушных Сил Имени Ивана Кожедуба
Priority to UAU201403586U priority Critical patent/UA92687U/en
Publication of UA92687U publication Critical patent/UA92687U/en

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Abstract

A channel for automatic tracking of aircrafts by direction with capability of aircraft identification for a combined laser system includes a control element, unit for control of deflectors, pumped laser, longitudinal mode selector, block of deflectors, transmitting optics, receiving optics, photo-detector, broadband amplifier, resonance amplifiers adjusted to respective intermodal frequencies, detectors, filters, pulse formers, 1|0 flip-flop, AND gates, delay lines, counters, digital-analog converters, low frequency filters, error amplifiers (filters), executive mechanisms, electronic computing machine, identification unit and a – input of the reference signal with frequency νfrom transmitting laser, b – input of the signal from the channel for measurement of aircraft circumferential velocity (attitude rates). Additionally an optical-electronic module is incorporated, this comprises television and infrared channels.
UAU201403586U 2014-04-07 2014-04-07 Channel for automatic tracking of aircrafts by direction with capability of identification of a for a combined laser system UA92687U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201403586U UA92687U (en) 2014-04-07 2014-04-07 Channel for automatic tracking of aircrafts by direction with capability of identification of a for a combined laser system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201403586U UA92687U (en) 2014-04-07 2014-04-07 Channel for automatic tracking of aircrafts by direction with capability of identification of a for a combined laser system

Publications (1)

Publication Number Publication Date
UA92687U true UA92687U (en) 2014-08-26

Family

ID=52682082

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201403586U UA92687U (en) 2014-04-07 2014-04-07 Channel for automatic tracking of aircrafts by direction with capability of identification of a for a combined laser system

Country Status (1)

Country Link
UA (1) UA92687U (en)

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