CN101738145B - Hood type target simulator - Google Patents
Hood type target simulator Download PDFInfo
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- CN101738145B CN101738145B CN2009101726700A CN200910172670A CN101738145B CN 101738145 B CN101738145 B CN 101738145B CN 2009101726700 A CN2009101726700 A CN 2009101726700A CN 200910172670 A CN200910172670 A CN 200910172670A CN 101738145 B CN101738145 B CN 101738145B
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- output shaft
- target simulator
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- 230000003287 optical effect Effects 0.000 claims abstract description 19
- 230000005855 radiation Effects 0.000 claims abstract description 17
- 239000011159 matrix material Substances 0.000 claims description 11
- 239000003550 marker Substances 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 3
- 230000008676 import Effects 0.000 claims description 2
- 238000001035 drying Methods 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000006748 scratching Methods 0.000 description 1
- 230000002393 scratching effect Effects 0.000 description 1
- 230000003595 spectral effect Effects 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to a hood type target simulator. The hood type target simulator comprises a hood, and a rotating device and an optical device which are arranged inside the hood; the inside of the hood is provided with a fixed channel which is fitted with the head of a missile to be detected; the rotating device comprises an electrically-controlled turn table of which the axis of an output shaft fixed on the hood runs through the axis of the fixed channel; the output shaft of the electrically-controlled turn table is fixedly connected with a support plate which extends along the axial direction of the fixed channel; one end of the support plate far from the output shaft is provided with an angular position station which is positioned on one side of the support plate towards the fixed channel; the optical device is fixed on the angular position station and comprises a collimator tube and a black body which is fixed outside the collimator tube; the black body is used for radiating infrared rays to the collimator tube; an infrared radiation outlet of the black body is provided with a dimmable aperture plate; and the axis of the collimator tube is coaxial with the axis of the fixed channel. The target simulator can simulate infrared targets with different radiation strengths and radiation sizes.
Description
Technical field
The present invention relates to a kind of hood type target simulator, belong to the infrared technique field.
Background technology
Precise guidance attack weapon receives the various countries military extensively to be favored.In future war, the attack precision that weapon is attacked in precise guidance possibly play crucial effects to the transformation of whole war situation situation, and therefore, each main military country all attacks weapon in the precise guidance of positive development precise guidance.Infrared guidance is used more extensive in precision guided weapon; The performance that when development and detection infrared guidance weapon, needs the infrared homing system of tester; When the infrared homing systematic function of test, adopt simulator to simulate the mode that the infrared target source is a kind of convenient and efficient.
Summary of the invention
The hood type target simulator that the purpose of this invention is to provide a kind of radiation intensity, radiation variable size is in order to detect infrared homing systemic-function.
For realizing above-mentioned purpose, the present invention adopts following technical scheme: a kind of hood type target simulator comprises head-shield and the tumbler and the Optical devices that are arranged in the head-shield; Has the stationary conduit that matches with nose of missile to be detected in the said head-shield; Said tumbler comprises the automatically controlled turntable of the axis process stationary conduit axis that is fixed in the output shaft on the head-shield; Be fixed with on the output shaft of automatically controlled turntable along the axially extended gripper shoe of stationary conduit; This gripper shoe is provided with position, angle platform away from an end of output shaft, and this position, angle platform is positioned at the side of gripper shoe towards stationary conduit, and said Optical devices are fixed on the platform of position, angle; These Optical devices comprise the black matrix that parallel light tube is outer with being fixed in parallel light tube; This black matrix is used for to the parallel light tube infrared radiation, and is provided with the adjustable diaphragm dish in the infrared radiation exit of black matrix, the axis of said parallel light tube and the axis coaxle of stationary conduit.
The arranged outside of said stationary conduit import department has clip.
Said parallel light tube adopts Cassegrain's formula optical system.
Said automatically controlled turntable is the worm gear electric rotary table.
The target seeker position marker of the output shaft of said automatically controlled turntable and guided missile to be detected is coaxial.
Be provided with tumbler in the hood type target simulator of the present invention, this tumbler has pitching and these two kinds of forms of motion that on horizontal plane, swing, and Optical devices are installed on the tumbler and with tumbler and move.When Optical devices moved with tumbler, the infrared spectral range that Optical devices are radiated the weapon head can change accordingly.In addition, be provided with the adjustable diaphragm dish, can regulate Optical devices through adjusting grating dish and penetrate ultrared intensity in the infrared radiation exit of Optical devices black matrix.It is thus clear that this hood type target simulator can be simulated radiation intensity, radiation size, can be used for detecting the target-seeking performance of infrared guidance weapon to different radiation intensity, radiation size target.Also have, the target seeker position marker of the output shaft of automatically controlled turntable and guided missile to be detected is coaxial, has saved the operation with required target and guided missile aligning like this, has simplified the inspection step, has improved checking efficiency.
Description of drawings
Fig. 1 is the structural representation that hood type target simulator of the present invention is installed on nose of missile;
Fig. 2 is the front view of tumbler;
Fig. 3 is the upward view of tumbler;
Fig. 4 is the structural representation of Optical devices.
The specific embodiment
Fig. 1,2,3, shown in 4, hood type target simulator of the present invention comprises head-shield 1, the front portion of this head-shield 1 is provided with stationary conduit 3; This target simulator is fixed on the head of guided missile 5 through stationary conduit 3; The profile of the shape of this stationary conduit 3 and guided missile 5 front ends is consistent, can better be secured to the head of guided missile 5 like this, in addition; In stationary conduit 3, being bonded with fabric protects the body surface to avoid scratching; Also have, clip 4 is arranged, can head-shield 1 and body be connected together closely through this clip 4 in the arranged outside of stationary conduit 3 opening parts.In head-shield 1, be installed with tumbler 6; This tumbler 6 comprises a worm gear electric rotary table 9; The axis of the output shaft 10 of worm gear electric rotary table 9 is through the axis of stationary conduit 3; And with the axis normal of stationary conduit 3, and the target seeker position marker of the axis of output shaft 10 and guided missile to be detected is coaxial.On output shaft 10, be installed with one along the axially extended gripper shoe 8 of stationary conduit; This gripper shoe 8 is provided with position, angle platform 7 away from an end of output shaft 10; Realize elevating movement through position, manual adjustments angle platform 7, realize swinging of horizontal direction through worm gear electric rotary table 9.On position, angle platform 7, be installed with Optical devices 2, these Optical devices 2 comprise a parallel light tube based on Cassegrain's formula, and the arranged outside of this parallel light tube has a black matrix 11; Black matrix 11 is used for infrared radiation in parallel light tube; Infrared radiation mouth place at black matrix 11 is provided with an adjustable diaphragm dish 12, has the different aperture in aperture on the adjustable diaphragm dish 12, through regulating the position of adjustable diaphragm dish 12; Infrared ray is penetrated from the aperture of different diameters; The ultrared energy that penetrates in the aperture in different apertures is different, therefore, can simulate the infrared target of different radiation intensity.The infrared ray that Optical devices are sent by black matrix 11 forms spot light through the aperture on the adjustable diaphragm dish 12 and outwards disperses; After level crossing 17 reflections, incide on the secondary mirror 16; Reenter through the light of secondary mirror 16 reflection and to be mapped on the principal reflection mirror 13; Infrared ray forms directional light after principal reflection mirror 13 reflections, project through infrared window 15 on the target seeker of guided missile.In parallel light tube, also be provided with drier 14 and guarantee the drying in the parallel light tube; One side of parallel light tube top drier is provided with observation window; Can whether lose efficacy from the agent 14 that sees drying of this observation window 20, and can open the bonnet of parallel light tube after drier 14 lost efficacy and change drier.
Claims (6)
1. a hood type target simulator is characterized in that: comprise head-shield and the tumbler and the Optical devices that are arranged in the head-shield; Has the stationary conduit that matches with nose of missile to be detected in the said head-shield; Said tumbler comprises the automatically controlled turntable of the axis process stationary conduit axis that is fixed in the output shaft on the head-shield; Be fixed with on the output shaft of automatically controlled turntable along the axially extended gripper shoe of stationary conduit; This gripper shoe is provided with position, angle platform away from an end of output shaft, and this position, angle platform is positioned at the side of gripper shoe towards stationary conduit, and said Optical devices are fixed on the platform of position, angle; These Optical devices comprise the black matrix that parallel light tube is outer with being fixed in parallel light tube; This black matrix is used for to the parallel light tube infrared radiation, and is provided with the adjustable diaphragm dish in the infrared radiation exit of black matrix, the axis of said parallel light tube and the axis coaxle of stationary conduit.
2. hood type target simulator according to claim 1 is characterized in that: the arranged outside of said stationary conduit import department has clip.
3. hood type target simulator according to claim 1 and 2 is characterized in that: said parallel light tube adopts Cassegrain's formula optical system.
4. hood type target simulator according to claim 1 and 2 is characterized in that: said automatically controlled turntable is the worm gear electric rotary table.
5. hood type target simulator according to claim 1 and 2 is characterized in that: the target seeker position marker of the output shaft of said automatically controlled turntable and guided missile to be detected is coaxial.
6. hood type target simulator according to claim 3 is characterized in that: the target seeker position marker of the output shaft of said automatically controlled turntable and guided missile to be detected is coaxial.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101726700A CN101738145B (en) | 2009-11-23 | 2009-11-23 | Hood type target simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101726700A CN101738145B (en) | 2009-11-23 | 2009-11-23 | Hood type target simulator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101738145A CN101738145A (en) | 2010-06-16 |
| CN101738145B true CN101738145B (en) | 2012-07-25 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009101726700A Expired - Fee Related CN101738145B (en) | 2009-11-23 | 2009-11-23 | Hood type target simulator |
Country Status (1)
| Country | Link |
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| CN (1) | CN101738145B (en) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102168988B (en) * | 2010-12-28 | 2012-06-27 | 哈尔滨工业大学 | Double-waveband collimator-tube target simulator |
| CN102621692A (en) * | 2012-03-09 | 2012-08-01 | 中国科学院长春光学精密机械与物理研究所 | Energy-adjustable infrared target simulation system |
| CN103033098B (en) * | 2012-11-27 | 2015-02-25 | 凯迈（洛阳）测控有限公司 | Manual diaphragm black body |
| CN103759587A (en) * | 2013-12-20 | 2014-04-30 | 河北汉光重工有限责任公司 | Ultra-low cost infrared tooling target simulator |
| CN104314930B (en) * | 2014-10-13 | 2017-09-26 | 凯迈（洛阳）测控有限公司 | A kind of adjustable clip and the target seeker fixing device using the clip |
| CN105021093A (en) * | 2015-06-25 | 2015-11-04 | 长春理工大学 | Zoom clamping type projection simulation device |
| CN106338221B (en) * | 2015-07-17 | 2019-01-08 | 北京航天计量测试技术研究所 | A kind of infrared seeker imaging automatic detection device can be used for launching site |
| CN105068369A (en) * | 2015-08-21 | 2015-11-18 | 哈尔滨工业大学 | Multi-band projection optical system |
| CN106839878A (en) * | 2015-12-07 | 2017-06-13 | 上海机电工程研究所 | A kind of middle-range infrared target simulator equipment |
| CN107525437B (en) * | 2017-09-04 | 2019-05-24 | 中国航发南方工业有限公司 | The detection method of infrared target simulator and guided missile tracking ability |
| CN109372652B (en) * | 2018-11-26 | 2024-05-24 | 北京金朋达航空科技有限公司 | Infrared enhancer with controllable radiation power |
| CN111221142B (en) * | 2020-01-14 | 2021-05-18 | 中国科学院长春光学精密机械与物理研究所 | Auxiliary optical machine installation and adjustment system |
| CN112179216B (en) * | 2020-09-25 | 2022-12-02 | 北京惠风联合防务科技有限公司 | Adjusting tool and using method thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3857042A (en) * | 1973-10-26 | 1974-12-24 | Us Navy | Laser seeker test set |
| DE3238897A1 (en) * | 1982-10-21 | 1984-04-26 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Infrared test device for missile homing heads |
| WO1992005601A1 (en) * | 1990-09-19 | 1992-04-02 | Scientific-Atlanta, Inc. | Apparatus and methods for simulating electromagnetic environments |
| US5596185A (en) * | 1993-11-10 | 1997-01-21 | Bodenseewerk Geratetechnik Gmbh | Device for generating picture information in real time for testing picture resolving sensors |
| US20050241384A1 (en) * | 2004-04-30 | 2005-11-03 | Clark Stephens | Portable guidance assembly test station |
| CN201583208U (en) * | 2009-11-23 | 2010-09-15 | 凯迈（洛阳）测控有限公司 | Head-covering type target simulator |
-
2009
- 2009-11-23 CN CN2009101726700A patent/CN101738145B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3857042A (en) * | 1973-10-26 | 1974-12-24 | Us Navy | Laser seeker test set |
| DE3238897A1 (en) * | 1982-10-21 | 1984-04-26 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Infrared test device for missile homing heads |
| WO1992005601A1 (en) * | 1990-09-19 | 1992-04-02 | Scientific-Atlanta, Inc. | Apparatus and methods for simulating electromagnetic environments |
| US5596185A (en) * | 1993-11-10 | 1997-01-21 | Bodenseewerk Geratetechnik Gmbh | Device for generating picture information in real time for testing picture resolving sensors |
| US20050241384A1 (en) * | 2004-04-30 | 2005-11-03 | Clark Stephens | Portable guidance assembly test station |
| CN201583208U (en) * | 2009-11-23 | 2010-09-15 | 凯迈（洛阳）测控有限公司 | Head-covering type target simulator |
Non-Patent Citations (2)
| Title |
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| 任获荣,张平,王家礼.VXI 总线导弹导引头模拟与自动测试系统.《计算机测量与控制》.2004,第12卷(第8期),757-758,786. * |
| 张兴堂.某型号导引头综合测试设备调试平台的研制.《中国优秀硕士学位论文全文数据库 工程科技II辑》.2009,(第3期),C032-16. * |
Also Published As
| Publication number | Publication date |
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| CN101738145A (en) | 2010-06-16 |
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| CB03 | Change of inventor or designer information |
Inventor after: Zhou Hailong Inventor after: Min Zhiyu Inventor after: Li Yan Inventor after: Dong Chunxia Inventor after: Chang Jia Inventor before: Zhou Hailong Inventor before: Li Yan Inventor before: Dong Chunxia Inventor before: Min Zhiyu |
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Free format text: CORRECT: INVENTOR; FROM: ZHOU HAILONG LI YAN DONG CHUNXIA MIN ZHIYU TO: ZHOU HAILONG MIN ZHIYU LI YAN DONG CHUNXIA CHANG JIA |
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