CN102261869A - Individual soldier digital fire control device for intercepting low altitude small target at slow speed - Google Patents
Individual soldier digital fire control device for intercepting low altitude small target at slow speed Download PDFInfo
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- CN102261869A CN102261869A CN2011101606208A CN201110160620A CN102261869A CN 102261869 A CN102261869 A CN 102261869A CN 2011101606208 A CN2011101606208 A CN 2011101606208A CN 201110160620 A CN201110160620 A CN 201110160620A CN 102261869 A CN102261869 A CN 102261869A
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Abstract
The invention discloses an individual soldier digital fire control device for intercepting a low altitude small target at slow speed. The device comprises a fire control computer (8), a power supply module (7), a white light aiming tool (1), a glimmer aiming tool (2), a laser distance measuring machine (3), an angle measuring device (4), a temperature meter (5), a graphic display (6) and a trajectory resolving assembly (9), wherein the fire control computer (8) performs data interactive with above various elements by adopting a data bus manner. The trajectory resolving assembly (9) resolves firing data according to the measured target information; the fire control computer (8) displays pre-measured aiming point on the eyepiece graphic display (6) in a digital form; and an operator shoots after aiming at a target according to the displayed aiming point. The device has the characteristics of light mass, low cost, convenience for operation, and the like, and can fast discover and track a low altitude small target at slow speed under an urban environment, and also can improve intercepting hit probability.
Description
Technical field
The present invention relates to a kind of fire control device, particularly a kind of interception low latitude little at a slow speed target individual soldier digitalization fire control device.
Background technology
The little at a slow speed target in low latitude mainly constitutes terrified or the destruction threat to momentous conference, big assembly etc. are movable.At present, domestic mainly by military antiaircraft fire control device detection, the little at a slow speed target in interception low latitude, as antiaircraft gun, air defence missile etc., but above-mentioned fire control device aim at search, interception high-altitude, at a high speed, large-scale fighter plane and design use, mainly contain detection radar, guidance radar, indication control board, fire control computer, supply module and form.It is applied in has following shortcoming on the interception low latitude little at a slow speed target:
1) owing to urban environment low target background complexity, the little at a slow speed target radar feature in low latitude is not obvious, and therefore, all kinds of military antiaircraft fire control devices are difficult to find target;
2) air defence missile fire control device is used to control seeker, and the function complexity needs many people compounding practice, is not suitable for the individual soldier and uses;
3) antiaircraft gun fire control device is used for control does not have the control bullet, and the pattern of operation is united with many covers, and multiple running fire increases interception probability, is unfavorable for the more place application deployment of personnel such as large-scale activity scene.
Summary of the invention
The object of the present invention is to provide a kind of interception low latitude little at a slow speed target individual soldier digitalization fire control device, the discovery target difficulty that exists when solving the little at a slow speed target in the military antiaircraft fire control device interception of present domestic use low latitude, the equipment complicated operation is unfavorable for the difficult problem of field deployment.
A kind of individual soldier digitalization fire control device of tackling the little at a slow speed target in low latitude, comprise: fire control computer, supply module also comprise: white light is taken aim at tool, low-light is taken aim at tool, range finder using laser, angular surveying device, temperature meter, image-text display, ballistic solution assembly.White light is taken aim at tool and low-light and is taken aim at tool and place fire control device front upper part; Range finder using laser places the front end of fire control device; Angular transducer, temperature sensor, supply module place the lower end of fire control device; Image-text display places the rear end of fire control device; Fire control computer and ballistic solution assembly place the middle part of fire control device.White light is taken aim at tool and is taken aim at tool with low-light and be connected by universal serial bus with image-text display, and image-text display is connected by video bus with fire control computer; Range finder using laser is connected by universal serial bus with fire control computer; The angular surveying device is connected by the analog-to-digital conversion interface with fire control computer with temperature meter; The ballistic solution assembly is connected by shared drive with fire control computer.
White light is taken aim at tool or low-light and is taken aim at tool target and background image thereof are imported in the image-text display; The distance of range finder using laser measurement target, the angular surveying device is measured the azimuth and the angle of pitch, and temperature meter is used for measures ambient temperature, and fire control computer is sent to the ballistic solution assembly by bus with above-mentioned data; Ballistic solution assembly inquiry firing table resolves the firing data and presets aiming point, and Query Result is sent to fire control computer again; Fire control computer will preset the aiming point parameter earlier and change into the electronic division line, be sent in the image-text display after mixing through picture and text then; The operator just can implement aiming and interception operation to the little at a slow speed target in low latitude by observing image-text display.
This device has light weight, and cost is low, simple operation, and the little at a slow speed target in low latitude can be found, follow the tracks of to characteristics such as automaticity height fast under urban environment, implement ballistic solution fast, and the emission of control interceptor improves the little at a slow speed target interception in low latitude hit probability.
Description of drawings
A kind of interception of Fig. 1 low latitude little at a slow speed target individual soldier digitalization fire control device schematic diagram.
1. white light is taken aim at tool 2. low-lights and is taken aim at tool 3. range finder using lasers 4. angular surveying devices 5. temperature meters 6. image-text displays
7. supply module 8. fire control computers 9. ballistic solution assemblies.
The specific embodiment
A kind of individual soldier digitalization fire control device of tackling the little at a slow speed target in low latitude, comprise: fire control computer 8, supply module 7 also comprise: white light is taken aim at tool 1, low-light is taken aim at tool 2, range finder using laser 3, angular surveying device 4, temperature meter 5, image-text display 6, ballistic solution assembly 9.White light is taken aim at tool 1 and low-light and is taken aim at tool 2 and place fire control device front upper part; Range finder using laser 3 places the front end of fire control device; Angular surveying device 4, temperature meter 5, supply module put 7 in the lower end of fire control device; Image-text display 6 places the rear end of fire control device; Fire control computer 8 and ballistic solution assembly 9 place the middle part of fire control device.White light is taken aim at tool 1 and low-light and is taken aim at tool 2 and image-text display 6 and be connected by universal serial bus, and image-text display 6 and fire control computer 8 are connected by video bus; Range finder using laser 3 and fire control computer 8 are connected by universal serial bus; Angular surveying device 4 is connected by the analog-to-digital conversion interface with fire control computer 8 with temperature meter 5; Ballistic solution assembly 9 is connected with fire control computer 8 shared drives.
White light is taken aim at tool 1 or low-light and is taken aim at tool 2 target and background image thereof are imported in the image-text display 6; The distance of range finder using laser 3 measurement target, angular surveying device 4 is measured the azimuth and the angle of pitch, and temperature survey 5 devices are used for measures ambient temperature, and fire control computer 8 is sent to ballistic solution assembly 9 by bus with above-mentioned data; Ballistic solution assembly 9 inquiry firing tables resolve the firing data and preset aiming point, and Query Result is sent to fire control computer 8 again; Fire control computer will preset the aiming point parameter earlier and change into the electronic division line, be sent in the image-text display 6 after mixing through picture and text then; The operator just can implement aiming and interception operation to the little at a slow speed target in low latitude by observing image-text display 6.
But this photoelectricity fire control device individual soldier pickaback or be fixedly mounted on the launcher turntable, during operating personnel's rotating operation, the fire control device can be searched for, follow the tracks of and measure target, in case the stable target of catching up with, operating personnel can launch laser immediately and find range, angular surveying device 4 is measured the azimuth and the angle of pitch of tracking target simultaneously, and ballistic solution assembly 9 calculates firing data and lead aiming point according to target oblique distance, azimuth, the angle of pitch and the meteorological condition etc. that record.Fire control computer 8 is presented at the lead aiming point in the middle of the eyepiece image-text display 6 with the digital form of enough accuracy, and shooter turns launcher according to shown aiming point, and run-home can be shot.Fire control computer was finished on the bullet of parameter and is bound when shooter pressed firing button, and provided ignition signal.
Claims (1)
1. individual soldier digitalization fire control device of tackling the little at a slow speed target in low latitude, comprise: fire control computer (8), supply module (7) is characterized in that also comprising: white light is taken aim at tool (1), low-light is taken aim at tool (2), range finder using laser (3), angular surveying device (4), temperature meter (5), image-text display (6), ballistic solution assembly (9); White light is taken aim at tool (1) and low-light and is taken aim at tool (2) and place fire control device front upper part; Range finder using laser (3) places the front end of fire control device; Angular surveying device (4), temperature meter (5), supply module (7) place the lower end of fire control device; Image-text display (6) places the rear end of fire control device; Fire control computer (8) and ballistic solution assembly (9) place the middle part of fire control device; Image-text display (6) is taken aim at tool (1) with white light respectively and is taken aim at tool (2) universal serial bus with low-light and be connected, and image-text display (6) is connected with fire control computer (8) video bus; Range finder using laser (3) is connected with fire control computer (8) universal serial bus; Fire control computer (8) is connected with temperature meter (5) analog-to-digital conversion interface with angular surveying device (4) respectively; Ballistic solution assembly (9) is connected with fire control computer (8) shared drive;
White light is taken aim at tool (1) or low-light and is taken aim at tool (2) target and background image thereof are imported in the image-text display (6); The distance of range finder using laser (3) measurement target, angular surveying device (4) is measured the azimuth and the angle of pitch, and temperature meter (5) is used for measures ambient temperature, and fire control computer (8) is sent to ballistic solution assembly (9) by bus with above-mentioned data; Ballistic solution assembly (9) inquiry firing table resolves the firing data and presets aiming point, and Query Result is sent to fire control computer (8) again; Fire control computer (8) will preset the aiming point parameter earlier and change into the electronic division line, be sent in the image-text display (6) after mixing through picture and text then; The operator just can implement aiming and interception operation to the little at a slow speed target in low latitude by observing image-text display (6).
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| Application Number | Priority Date | Filing Date | Title |
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| CN2011101606208A CN102261869A (en) | 2011-06-15 | 2011-06-15 | Individual soldier digital fire control device for intercepting low altitude small target at slow speed |
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| Application Number | Priority Date | Filing Date | Title |
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| CN2011101606208A CN102261869A (en) | 2011-06-15 | 2011-06-15 | Individual soldier digital fire control device for intercepting low altitude small target at slow speed |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104634185A (en) * | 2014-12-08 | 2015-05-20 | 河北汉光重工有限责任公司 | Evidence obtaining and fighting integrated device |
| CN105486175A (en) * | 2014-11-20 | 2016-04-13 | 中国久远高新技术装备公司 | Low-altitude security protection system and method based on large-power continuous laser |
| CN106532809A (en) * | 2016-10-27 | 2017-03-22 | 北京机械设备研究所 | Civil interceptor electric detonating controller |
| CN109443097A (en) * | 2018-11-16 | 2019-03-08 | 南京理工大学 | A kind of acquisition equipment and catching method for rotor wing unmanned aerial vehicle |
| WO2019233156A1 (en) * | 2017-12-16 | 2019-12-12 | 西安华科光电有限公司 | Multi-functional sight |
| CN112824820A (en) * | 2019-11-21 | 2021-05-21 | 北京恒星箭翔科技有限公司 | Reverse-low small slow target air defense missile system for 40 mm rocket launcher and intercepting method |
| CN114459292A (en) * | 2021-12-28 | 2022-05-10 | 中国人民解放军国防科技大学 | Trajectory calculation system for fire control correction |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1527020A (en) * | 2003-03-05 | 2004-09-08 | 陈仰帆 | Automatic low altitude flyer attacking method and gun system |
| WO2005033616A1 (en) * | 2003-10-02 | 2005-04-14 | Rheinmetall Waffe Munition Gmbh | Method and device for protecting ships against end-stage guided missiles |
| WO2006079029A2 (en) * | 2005-01-24 | 2006-07-27 | Ron Allen | Defense system and method |
| WO2008029392A2 (en) * | 2006-09-03 | 2008-03-13 | E.C.S. Engineering Consulting Services-Aerospace Ltd. | Method and system for defense against incoming rockets and missiles |
| WO2009045573A1 (en) * | 2007-06-08 | 2009-04-09 | Raytheon Company | Methods and apparatus for intercepting a projectile |
| CN101982720A (en) * | 2010-09-29 | 2011-03-02 | 北京机械设备研究所 | Interception method of low-altitude low-velocity small targets |
| CN102087082A (en) * | 2010-11-22 | 2011-06-08 | 北京机械设备研究所 | Firing table fitting-based low-altitude low-speed small object intercepting method |
-
2011
- 2011-06-15 CN CN2011101606208A patent/CN102261869A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1527020A (en) * | 2003-03-05 | 2004-09-08 | 陈仰帆 | Automatic low altitude flyer attacking method and gun system |
| WO2005033616A1 (en) * | 2003-10-02 | 2005-04-14 | Rheinmetall Waffe Munition Gmbh | Method and device for protecting ships against end-stage guided missiles |
| WO2006079029A2 (en) * | 2005-01-24 | 2006-07-27 | Ron Allen | Defense system and method |
| WO2008029392A2 (en) * | 2006-09-03 | 2008-03-13 | E.C.S. Engineering Consulting Services-Aerospace Ltd. | Method and system for defense against incoming rockets and missiles |
| WO2009045573A1 (en) * | 2007-06-08 | 2009-04-09 | Raytheon Company | Methods and apparatus for intercepting a projectile |
| CN101982720A (en) * | 2010-09-29 | 2011-03-02 | 北京机械设备研究所 | Interception method of low-altitude low-velocity small targets |
| CN102087082A (en) * | 2010-11-22 | 2011-06-08 | 北京机械设备研究所 | Firing table fitting-based low-altitude low-speed small object intercepting method |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105486175A (en) * | 2014-11-20 | 2016-04-13 | 中国久远高新技术装备公司 | Low-altitude security protection system and method based on large-power continuous laser |
| CN105486175B (en) * | 2014-11-20 | 2017-05-10 | 中国久远高新技术装备公司 | Low-altitude security protection system and method based on large-power continuous laser |
| CN104634185A (en) * | 2014-12-08 | 2015-05-20 | 河北汉光重工有限责任公司 | Evidence obtaining and fighting integrated device |
| CN106532809A (en) * | 2016-10-27 | 2017-03-22 | 北京机械设备研究所 | Civil interceptor electric detonating controller |
| CN106532809B (en) * | 2016-10-27 | 2019-03-15 | 北京机械设备研究所 | A kind of civilian interceptor electric initiating controller |
| WO2019233156A1 (en) * | 2017-12-16 | 2019-12-12 | 西安华科光电有限公司 | Multi-functional sight |
| CN109443097A (en) * | 2018-11-16 | 2019-03-08 | 南京理工大学 | A kind of acquisition equipment and catching method for rotor wing unmanned aerial vehicle |
| CN112824820A (en) * | 2019-11-21 | 2021-05-21 | 北京恒星箭翔科技有限公司 | Reverse-low small slow target air defense missile system for 40 mm rocket launcher and intercepting method |
| CN114459292A (en) * | 2021-12-28 | 2022-05-10 | 中国人民解放军国防科技大学 | Trajectory calculation system for fire control correction |
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Application publication date: 20111130 |