SU149892A1 - The device for stabilization in space of the course of the ship, for example, space - Google Patents

The device for stabilization in space of the course of the ship, for example, space

Info

Publication number
SU149892A1
SU149892A1 SU751787A SU751787A SU149892A1 SU 149892 A1 SU149892 A1 SU 149892A1 SU 751787 A SU751787 A SU 751787A SU 751787 A SU751787 A SU 751787A SU 149892 A1 SU149892 A1 SU 149892A1
Authority
SU
USSR - Soviet Union
Prior art keywords
space
ship
course
mirrors
stabilization
Prior art date
Application number
SU751787A
Other languages
Russian (ru)
Inventor
Б.Н. Козлов
Original Assignee
Б.Н. Козлов
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 Б.Н. Козлов filed Critical Б.Н. Козлов
Priority to SU751787A priority Critical patent/SU149892A1/en
Application granted granted Critical
Publication of SU149892A1 publication Critical patent/SU149892A1/en

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  • Optical Radar Systems And Details Thereof (AREA)

Description

Известные устройства дл  стабилизации в пространстве курса корабл , содержащие систему зеркал и фотоэлектрический датчик, св занный с исполнительными механизмами объекта унравлени , не обеспечивают высокой точности и сложны конструктивно.The known devices for stabilization in space of the course of ships, containing a system of mirrors and a photoelectric sensor associated with the actuators of the object to be steered, do not provide high accuracy and are complex in design.

В, предлагаемом устройст1ве дл  обеспечени  независимости работы датчика от внешних источников света зеркала укреплены так, что луч образует замкнутую траекторию, на пути которой установлен кванто-механический усилитель света.In the proposed device, in order to ensure the independence of the sensor operation from external light sources, the mirrors are reinforced so that the beam forms a closed trajectory, in the path of which a quantum-mechanical light amplifier is installed.

На чертеже приведена принципиальна  схема описываемого устройства .The drawing is a schematic diagram of the described device.

Устройство имеет вогнутые зеркала 1, 2, 3 v( 4, расположенные на поверхности одной и той же (воображаемой) сферы, радиус которой Совпадает с радиусом кривизны зеркал. Луч света 5, отража сь от зеркал 1, 2, 3 и 4, образует замкнутую траекторию и не за1висит от внешних источников излучени . Посто нство интенсивности излучени  измен етс  вследствие отражений, поддерживаемого кванто-механическим усилителем света (лазером) 6, установленным на 1нути замкнутой траектории.The device has concave mirrors 1, 2, 3 v (4, located on the surface of the same (imaginary) sphere, whose radius coincides with the radius of curvature of the mirrors. A ray of light 5, reflected from mirrors 1, 2, 3 and 4, forms a closed path and does not depend on external sources of radiation.The state of the intensity of the radiation changes due to reflections supported by a quantum mechanical light amplifier (laser) 6 installed on the same closed path.

Система зеркал 1, 2, 3 и 4 жестко с-феплена с объектом стабилизации и каждое зеркало снабжено фотоэлементами 7. Зеркала конструктивно выполнены так, что отражающей их частью (собственно зеркалом)  вл етс  лишь небольшое п тно, куда падает луч света при неизменности курса корабл , а остальна , больша  часть, расположенна  вокруг собственного зеркала, служит в качестве фотоэлемента, позвол ющего регистрировать -поладание на него светового луча.A system of mirrors 1, 2, 3, and 4 is rigidly c-shaped with a stabilizing object, and each mirror is provided with photocells 7. The mirrors are structurally designed so that the reflecting part (the mirror itself) is only a small spot where the light beam falls the ship, and the rest, a large part, located around its own mirror, serves as a photocell, allowing it to record a light beam being hit on it.

При отклонении корабл  от заданного курса световой луч попадает на фотоэле.мепты, сообщаюшие сигнал на исполнительные механизмы , которые, благодар  соответствующим автоматическим устройства , вывод т корабль на заданный курс.When a ship deviates from a predetermined course, the light beam enters the photo eel. The signals communicate a signal to the actuators, which, thanks to the appropriate automatic devices, bring the ship to a predetermined course.

Описанное устройство может найти применение в космической навигации , а1виации и судовождении дл  стабилизации в .пространстве соответствующей системы (космической ракеты, самолета, корабл  подводной лодки).The described device can be used in space navigation, navigation and navigation in order to stabilize the corresponding system (space rocket, aircraft, submarine ship) in space.

Предмет из,обретени Item of gain

Устройство дл  стабилизации а пространстве курса корабл , например , космического, содержащее систему зеркал и фотоэлектрический датчик, св занный с исполнительными механизмами объекта управлени , отличающеес  тем, что, с целью обеспечени  независимости работы датчика от внешних ИСТОЧЕИКОВ света, зеркала укреплены так, что луч образует замкнутую траекторию, на пути которой установлен кванто-механический усилитель света.A device for stabilizing the space course of a ship, for example, a spacecraft, containing a system of mirrors and a photoelectric sensor associated with the actuators of the control object, characterized in that, in order to ensure the independence of the sensor operation from external SOURCES of light, the mirrors are reinforced so that the beam forms a closed path, on the way of which a quantum-mechanical amplifier of light is installed.

SU751787A 1961-11-15 1961-11-15 The device for stabilization in space of the course of the ship, for example, space SU149892A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU751787A SU149892A1 (en) 1961-11-15 1961-11-15 The device for stabilization in space of the course of the ship, for example, space

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU751787A SU149892A1 (en) 1961-11-15 1961-11-15 The device for stabilization in space of the course of the ship, for example, space

Publications (1)

Publication Number Publication Date
SU149892A1 true SU149892A1 (en) 1961-11-30

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
SU751787A SU149892A1 (en) 1961-11-15 1961-11-15 The device for stabilization in space of the course of the ship, for example, space

Country Status (1)

Country Link
SU (1) SU149892A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3370253A (en) * 1964-03-31 1968-02-20 Navy Usa Integral mirror-photodetector structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3370253A (en) * 1964-03-31 1968-02-20 Navy Usa Integral mirror-photodetector structure

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