RU2002104057A - Method for optoelectronic alignment of a sighting device - Google Patents

Method for optoelectronic alignment of a sighting device

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Publication number
RU2002104057A
RU2002104057A RU2002104057/28A RU2002104057A RU2002104057A RU 2002104057 A RU2002104057 A RU 2002104057A RU 2002104057/28 A RU2002104057/28 A RU 2002104057/28A RU 2002104057 A RU2002104057 A RU 2002104057A RU 2002104057 A RU2002104057 A RU 2002104057A
Authority
RU
Russia
Prior art keywords
error
adjustment
sighting device
sighting
optical axis
Prior art date
Application number
RU2002104057/28A
Other languages
Russian (ru)
Inventor
Юрий Евгеньевич Крутиков
Игорь Игоревич Степанян
Original Assignee
Иркутский военный авиационный инженерный институт
Filing date
Publication date
Application filed by Иркутский военный авиационный инженерный институт filed Critical Иркутский военный авиационный инженерный институт
Publication of RU2002104057A publication Critical patent/RU2002104057A/en

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Claims (1)

Способ оптико-электронной юстировки визирного устройства, основанный на принципе действия квадрантных следящих устройств, заключается в том, что поток излучения в зависимости от смещения объекта относительно оптической оси распределяется между несколькими фоточувствительными элементами, сигналы с которых сравниваются между собой, в качестве базовых точек визирования используется источники светового излучения (излучающие диоды), устанавливаемые стационарно на борту ЛА; контроль котировочных параметров (Δε-погрешность юстировки по углу места, Δβ-погрешность юстировки по бортовому углу, Δγ-погрешность юстировки по крену) производится путем определения смещения центра пятна светового излучения относительно центра оптической оси квадрантного следящего устройства, расположенного на визирном устройстве.The method of optoelectronic alignment of the sighting device, based on the principle of operation of quadrant tracking devices, consists in the fact that the radiation flux is distributed among several photosensitive elements, depending on the displacement of the object relative to the optical axis, the signals from which are compared with each other, using the base points of sighting light sources (emitting diodes) installed permanently on board the aircraft; control of quotation parameters (Δε-error of adjustment by elevation, Δβ-error of adjustment by side angle, Δγ-error of adjustment by roll) is carried out by determining the offset of the center of the spot of light radiation relative to the center of the optical axis of the quadrant tracking device located on the sighting device.
RU2002104057/28A 2002-02-13 Method for optoelectronic alignment of a sighting device RU2002104057A (en)

Publications (1)

Publication Number Publication Date
RU2002104057A true RU2002104057A (en) 2003-10-20

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