UA89499U - 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 - Google Patents

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

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Publication number
UA89499U
UA89499U UAU201312642U UAU201312642U UA89499U UA 89499 U UA89499 U UA 89499U UA U201312642 U UAU201312642 U UA U201312642U UA U201312642 U UAU201312642 U UA U201312642U UA 89499 U UA89499 U UA 89499U
Authority
UA
Ukraine
Prior art keywords
aircraft
channel
measurement
measuring system
laser
Prior art date
Application number
UAU201312642U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Алексей Владимирович Коломийцев
Игорь Иванович Сачук
Геннадий Васильевич Алешин
Геннадий Владимирович Певцов
Александр Владимирович Довбня
Юрий Александрович Ковтунов
Анатолий Иванович Комышан
Олег Яковлевич Никонов
Сергей Владимирович Орлов
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 UAU201312642U priority Critical patent/UA89499U/en
Publication of UA89499U publication Critical patent/UA89499U/en

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Abstract

A 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 comprises a control element, unit for controlling deflectors, pumped laser, modified longitudinal mode selector, modified block of deflectors, transmitting optics, receiving optics, photodetectors, broadband amplifier, multifunction information block with σ – input of signal of measured aircraft circumferential velocity (attitude rates), resonance amplifiers adjusted to corresponding intermodal frequencies, pulse formers, 1|0 flip-flops, AND circuits, reversible counters, comparator circuits, electronic computer and- input of reference signals with intermodal frequenciesfrom transmitting laser. Next after the CC an electronic computer is included instead of electronic-digital computing machine.
UAU201312642U 2013-10-28 2013-10-28 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 UA89499U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201312642U UA89499U (en) 2013-10-28 2013-10-28 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

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201312642U UA89499U (en) 2013-10-28 2013-10-28 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

Publications (1)

Publication Number Publication Date
UA89499U true UA89499U (en) 2014-04-25

Family

ID=52281938

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201312642U UA89499U (en) 2013-10-28 2013-10-28 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

Country Status (1)

Country Link
UA (1) UA89499U (en)

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