CN104581067A - Radar antenna calibration telescope electronic imaging system - Google Patents

Radar antenna calibration telescope electronic imaging system Download PDF

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Publication number
CN104581067A
CN104581067A CN201410852850.4A CN201410852850A CN104581067A CN 104581067 A CN104581067 A CN 104581067A CN 201410852850 A CN201410852850 A CN 201410852850A CN 104581067 A CN104581067 A CN 104581067A
Authority
CN
China
Prior art keywords
wire
telescope
calibration
pitching
transfer box
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
CN201410852850.4A
Other languages
Chinese (zh)
Inventor
丁求启
宋海军
陈曦
陶敏
孙林飞
王新荣
张桂平
贾云翔
王宇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
63680 TROOPS PLA
Original Assignee
63680 TROOPS PLA
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 63680 TROOPS PLA filed Critical 63680 TROOPS PLA
Priority to CN201410852850.4A priority Critical patent/CN104581067A/en
Publication of CN104581067A publication Critical patent/CN104581067A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a radar antenna calibration telescope electronic imaging system which comprises a calibration telescope, a shading cover, a high-definition camera, a pitching rotary joint, a pitching switch box, a low-frequency sliding ring, a direction switch box, a direct-current power supply and a measuring and displaying unit. The calibration telescope is connected with the high-definition camera through the shading cover, the high-definition camera is connected with the pitching rotary joint through a wire, the pitching rotary joint is connected with the pitching switch box through a wire, the pitching switch box is connected with the low-frequency sliding ring through a wire, the low-frequency sliding ring is connected with the direction switch box through a wire, the direct-current power supply provides work voltage for the direction switch box, and the direction switch box is connected with the measuring and displaying unit through a wire. The radar antenna calibration telescope electronic imaging system reduces the number of staff during telescope calibration, shortens calibration time and improves calibration precision.

Description

Radar antenna calibration telescope electronization imaging system
Technical field
The present invention relates to radar monitoring field, especially a kind of radar antenna calibration telescope electronization imaging system.
Background technology
In telescope calibration process, post personnel need climb up antenna human eye and take aim at the reading that telescope reads azimuth mark, this kind of method easily affects by personnel's subjective factor, human eye error in reading is large, long between man-hour, repeatable accuracy is difficult to ensure, and human users is more dangerous under reversing face mode, exists and link up the problems such as inharmonious up and down.There is provided herein a kind of radar antenna calibration telescope electronization imaging system for this reason, the drawbacks such as the reading existed in traditional telescope calibration is inaccurate, error is larger can be overcome.
Summary of the invention
The technical problem to be solved in the present invention is: the problems such as the reading existed in calibration process for radar antenna telescope is inaccurate, error is larger, proposing a kind of radar antenna calibration telescope electronization imaging system overcomes above-mentioned drawback, improves calibration precision.
The technical solution adopted in the present invention is: a kind of radar antenna calibration telescope electronization imaging system, comprises calibration telescope, light shield, high-definition camera, elevation rotary joint, pitching transfer box, low frequency slip ring, orientation transfer box, DC power supply and measurement display unit; Described calibration telescope is connected with high-definition camera by light shield; Described high-definition camera is connected by wire with elevation rotary joint; Elevation rotary joint is connected with pitching transfer box by wire; Described pitching transfer box is connected with low frequency slip ring by wire; Described low frequency slip ring is connected with orientation transfer box by wire; Described DC power supply provides operating voltage for orientation transfer box; Described orientation transfer box is connected with measurement display unit by wire.
Further, DC power supply of the present invention exports 24V operating voltage.
The present invention is undertaken after suitable coordinating install, utilizing the slip ring of radar antenna by transmission of video images to machine room, receiving display image finally by equipment such as image pick-up card or monitoring monitors by camera and telescope ocular.
The invention has the beneficial effects as follows: personnel amount when native system decreases telescope calibration, shorten calibration time, improve calibration precision.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is that signal wiring of the present invention implements block diagram.
Embodiment
The present invention is further detailed explanation with preferred embodiment by reference to the accompanying drawings now.These accompanying drawings are the schematic diagram of simplification, only basic structure of the present invention are described in a schematic way, and therefore it only shows the formation relevant with the present invention.
A kind of radar antenna calibration telescope electronization imaging system as shown in Figure 1, comprises calibration telescope, light shield, high-definition camera, elevation rotary joint, pitching transfer box, low frequency slip ring, orientation transfer box, DC power supply and measurement display unit; Described calibration telescope is connected with high-definition camera by light shield; Described high-definition camera is connected by wire with elevation rotary joint; Elevation rotary joint is connected with pitching transfer box by wire; Described pitching transfer box is connected with low frequency slip ring by wire; Described low frequency slip ring is connected with orientation transfer box by wire; Described DC power supply provides operating voltage for orientation transfer box; Described orientation transfer box is connected with measurement display unit by wire.
Before data acquisition, first use hood for protecting rider suitable camera and telescope ocular to be carried out coordinating and installs, secondly use Differential slip-ring transmission power supply, and by intermediate frequency transmitting video image, finally in machine room, show image by monitoring monitor reception.
Further, DC power supply of the present invention exports 24V operating voltage.
Camera coordinates installation method with telescopical.Suitable camera and telescope ocular carry out coordinating by native system use hood for protecting rider to be installed, and makes telescope internal spider break up line high-visible in video image by the position that adjustment eyepiece is suitable.
Image transfer method: according to the concrete condition of radar antenna, we use Differential slip-ring to transmit power supply, and by intermediate frequency transmitting video image, ensure that cable connection method is simple, and power supply is reliable, and image transmitting is undistorted.
The fixing means of imaging system: native system devises two sections of adjustable mounting and fixing brackets, is arranged on imaging system in antenna pitching structure, by the length of adjusting pole, reduces mounting process.
The just the specific embodiment of the present invention described in above specification, various illustrating is not construed as limiting flesh and blood of the present invention, person of an ordinary skill in the technical field after having read specification can to before described embodiment make an amendment or be out of shape, and do not deviate from the spirit and scope of the invention.

Claims (2)

1. a radar antenna calibration telescope electronization imaging system, is characterized in that: comprise calibration telescope, light shield, high-definition camera, elevation rotary joint, pitching transfer box, low frequency slip ring, orientation transfer box, DC power supply and measurement display unit; Described calibration telescope is connected with high-definition camera by light shield; Described high-definition camera is connected by wire with elevation rotary joint; Elevation rotary joint is connected with pitching transfer box by wire; Described pitching transfer box is connected with low frequency slip ring by wire; Described low frequency slip ring is connected with orientation transfer box by wire; Described DC power supply provides operating voltage for orientation transfer box; Described orientation transfer box is connected with measurement display unit by wire.
2. radar antenna calibration telescope electronization imaging system as claimed in claim 1, is characterized in that: described DC power supply exports 24V operating voltage.
CN201410852850.4A 2014-12-31 2014-12-31 Radar antenna calibration telescope electronic imaging system Pending CN104581067A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410852850.4A CN104581067A (en) 2014-12-31 2014-12-31 Radar antenna calibration telescope electronic imaging system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410852850.4A CN104581067A (en) 2014-12-31 2014-12-31 Radar antenna calibration telescope electronic imaging system

Publications (1)

Publication Number Publication Date
CN104581067A true CN104581067A (en) 2015-04-29

Family

ID=53096144

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410852850.4A Pending CN104581067A (en) 2014-12-31 2014-12-31 Radar antenna calibration telescope electronic imaging system

Country Status (1)

Country Link
CN (1) CN104581067A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111398921A (en) * 2020-04-22 2020-07-10 中国人民解放军63816部队 Method for reducing uncertainty of radar photoelectric difference calibration

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102103262A (en) * 2011-02-18 2011-06-22 福鼎市一雄光学仪器有限公司 Video display ocular lens
CN202522258U (en) * 2012-02-10 2012-11-07 中国人民解放军63680部队 Visualized monitoring system for shipborne radar central part

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102103262A (en) * 2011-02-18 2011-06-22 福鼎市一雄光学仪器有限公司 Video display ocular lens
CN202522258U (en) * 2012-02-10 2012-11-07 中国人民解放军63680部队 Visualized monitoring system for shipborne radar central part

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111398921A (en) * 2020-04-22 2020-07-10 中国人民解放军63816部队 Method for reducing uncertainty of radar photoelectric difference calibration

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Application publication date: 20150429

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