UA89458U - Enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range complex - Google Patents

Enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range complex

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Publication number
UA89458U
UA89458U UAU201311810U UAU201311810U UA89458U UA 89458 U UA89458 U UA 89458U UA U201311810 U UAU201311810 U UA U201311810U UA U201311810 U UAU201311810 U UA U201311810U UA 89458 U UA89458 U UA 89458U
Authority
UA
Ukraine
Prior art keywords
deflectors
intermodal
modified block
measurement
frequencies
Prior art date
Application number
UAU201311810U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Алексей Владимирович Коломийцев
Игорь Иванович Сачук
Геннадий Васильевич Алешин
Андрей Владимирович Власов
Сергей Викторович Закиров
Сергей Иванович Кливец
Сергей Владимирович Орлов
Дмитрий Павлович Пашков
Иван Николаевич Теребуха
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 UAU201311810U priority Critical patent/UA89458U/en
Publication of UA89458U publication Critical patent/UA89458U/en

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Abstract

An enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range complex comprises a control element, unit controlling deflectors, pumped laser, longitudinal mode selector with frequency division multiplexing, modified block of deflectors, transmitting optics, receiving optics, photo-detector, broadband amplifier, multifunction information block with σ – input of signal of measured aircraft circumferential velocity (attitude rates), resonance amplifiers adjusted to the respective intermodal frequencies, pulse formers, 1|0 flip-flops, AND circuits, reversible counters, comparator circuits (CC) 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.
UAU201311810U 2013-10-07 2013-10-07 Enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range complex UA89458U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201311810U UA89458U (en) 2013-10-07 2013-10-07 Enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range complex

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201311810U UA89458U (en) 2013-10-07 2013-10-07 Enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range complex

Publications (1)

Publication Number Publication Date
UA89458U true UA89458U (en) 2014-04-25

Family

ID=52281897

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201311810U UA89458U (en) 2013-10-07 2013-10-07 Enhanced channel for measurement of aircraft attitude rates with use of intermodal frequencies and modified block of deflectors for a test range complex

Country Status (1)

Country Link
UA (1) UA89458U (en)

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