UA153829U - CHANNEL OF AUTOMATIC AIRCRAFT TRACKING IN DIRECTION USING INTER-MODE BIT FREQUENCIES AND GYRO-STABILIZATION FOR MOBILE SINGLE-POINT INFORMATION AND MEASUREMENT SYSTEM OF POLYGON TESTS - Google Patents

CHANNEL OF AUTOMATIC AIRCRAFT TRACKING IN DIRECTION USING INTER-MODE BIT FREQUENCIES AND GYRO-STABILIZATION FOR MOBILE SINGLE-POINT INFORMATION AND MEASUREMENT SYSTEM OF POLYGON TESTS Download PDF

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Publication number
UA153829U
UA153829U UAU202204759U UAU202204759U UA153829U UA 153829 U UA153829 U UA 153829U UA U202204759 U UAU202204759 U UA U202204759U UA U202204759 U UAU202204759 U UA U202204759U UA 153829 U UA153829 U UA 153829U
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UA
Ukraine
Prior art keywords
channel
gyro
measurement system
point information
stabilization
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UAU202204759U
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Ukrainian (uk)
Inventor
Олексій Володимирович Коломійцев
Геннадій Володимирович Пєвцов
Ольга Анатоліївна Усачова
Андрій Володимирович Власов
Дмитро Віталійович Черненко
Володимир Валерійович Ларін
Віктор Іванович Нікітченко
Віктор Олександрович Кузьменко
Олександр Васильович Юла
Андрій Анатолійович Мішок
Original Assignee
Державний науково-дослідний інститут випробувань і сертифікації озброєння та військової техніки
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Application filed by Державний науково-дослідний інститут випробувань і сертифікації озброєння та військової техніки filed Critical Державний науково-дослідний інститут випробувань і сертифікації озброєння та військової техніки
Priority to UAU202204759U priority Critical patent/UA153829U/en
Publication of UA153829U publication Critical patent/UA153829U/en

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Abstract

Канал автоматичного супроводження літальних апаратів за напрямкам з використанням частот міжмодових биттів та гіростабілізацією для мобільної однопунктної інформаційно-вимірювальної системи полігонних випробувань містить керуючий елемент, блок керування дефлекторами, лазер з накачкою, селектор подовжніх мод з багаточастотним розділенням каналів, модифікований блок дефлекторів, передавальну оптику, радіолокаційний модуль, який складений з антени, приймально-передавальної апаратури і апаратури захисту від завад, приймальну оптику, фотодетектор, широкосмуговий підсилювач, інформаційний блок, резонансні підсилювачі, настроєні на відповідні частоти міжмодових биттів, детектори, фільтри, формувачі імпульсів, тригери, схеми "і", лінії затримки, лічильники, цифро-аналогові перетворювачі, фільтри нижніх частот, підсилювачі (фільтри) сигналу похибки, виконавчі механізми, спеціалізовану електронну обчислювальну машину та а-введення опорного сигналу з частотою Δνм від передавального лазера, б-введення сигналу від каналу вимірювання кутових швидкостей літального апарата. Додатково введено гіростабілізовану платформу.The channel of automatic tracking of aircraft by directions using intermode beat frequencies and gyro stabilization for a mobile single-point information and measurement system of polygon tests includes a control element, a deflector control unit, a pump laser, a longitudinal mode selector with multi-frequency channel separation, a modified deflector unit, transmission optics, radar module, which consists of an antenna, transceiver equipment and interference protection equipment, receiving optics, photodetector, broadband amplifier, information unit, resonant amplifiers tuned to the appropriate frequencies of intermode bits, detectors, filters, pulse shapers, triggers, circuits " and", delay lines, counters, digital-to-analog converters, low-pass filters, amplifiers (filters) of the error signal, executive mechanisms, a specialized electronic computing machine and a-input of a reference signal with a frequency of Δνm from the transmitting laser, b-input of a signal from the channel measuring the angular velocities of the aircraft. Additionally, a gyro-stabilized platform was introduced.

UAU202204759U 2022-12-14 2022-12-14 CHANNEL OF AUTOMATIC AIRCRAFT TRACKING IN DIRECTION USING INTER-MODE BIT FREQUENCIES AND GYRO-STABILIZATION FOR MOBILE SINGLE-POINT INFORMATION AND MEASUREMENT SYSTEM OF POLYGON TESTS UA153829U (en)

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UAU202204759U UA153829U (en) 2022-12-14 2022-12-14 CHANNEL OF AUTOMATIC AIRCRAFT TRACKING IN DIRECTION USING INTER-MODE BIT FREQUENCIES AND GYRO-STABILIZATION FOR MOBILE SINGLE-POINT INFORMATION AND MEASUREMENT SYSTEM OF POLYGON TESTS

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Application Number Priority Date Filing Date Title
UAU202204759U UA153829U (en) 2022-12-14 2022-12-14 CHANNEL OF AUTOMATIC AIRCRAFT TRACKING IN DIRECTION USING INTER-MODE BIT FREQUENCIES AND GYRO-STABILIZATION FOR MOBILE SINGLE-POINT INFORMATION AND MEASUREMENT SYSTEM OF POLYGON TESTS

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UA153829U true UA153829U (en) 2023-09-06

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UAU202204759U UA153829U (en) 2022-12-14 2022-12-14 CHANNEL OF AUTOMATIC AIRCRAFT TRACKING IN DIRECTION USING INTER-MODE BIT FREQUENCIES AND GYRO-STABILIZATION FOR MOBILE SINGLE-POINT INFORMATION AND MEASUREMENT SYSTEM OF POLYGON TESTS

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UA (1) UA153829U (en)

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