CN201476702U - Real-time data acquisition device for anti-aircraft gun for weather modification operation - Google Patents
Real-time data acquisition device for anti-aircraft gun for weather modification operation Download PDFInfo
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- CN201476702U CN201476702U CN2009203075521U CN200920307552U CN201476702U CN 201476702 U CN201476702 U CN 201476702U CN 2009203075521 U CN2009203075521 U CN 2009203075521U CN 200920307552 U CN200920307552 U CN 200920307552U CN 201476702 U CN201476702 U CN 201476702U
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Abstract
The utility model relates to a real-time data acquisition device for an anti-aircraft gun for weather modification operation. The real-time data acquisition device comprises at least one information sensor, a data acquisition control unit, a data uploader and a system power supply for supplying electricity to the real-time data acquisition device; the data acquisition control unit comprises a singlechip, an A/D conversion circuit and an analog signal amplification circuit, the signal output of the information sensor is inputted into the singlechip via the analog signal amplification circuit and the A/D conversion circuit, the singlechip is connected with the data uploader through an interface circuit, and the information sensor is arranged at a corresponding information acquisition point on a gun body. Adopting the technical scheme of sensor sensing and measurement, the utility model realizes the automatic real-time acquisition of data, a GPRS remote transmission module is utilized to quickly transmit the acquired information to a remote control center, a command center directs the carryout of the weather modification operation of the on-site anti-aircraft gun, and thereby the weather modification operation can achieve an optimal operation effect.
Description
Technical field:
The utility model relates to the Weather modification operation technical field, relates in particular to a kind of Weather modification operation antiaircraft gun real time data acquisition device.
Background technology:
Arid, hail is the natural calamity that causes crop failure, utilizes antiaircraft gun or rocket gun to carry out Weather modification operation and the atmosphere cloud layer is carried out artificial affecting implements rain making, alleviates damage caused by a drought, avoids the formation of hail to obtain people using widely.But the collection of existing antiaircraft gun or rocket gun Weather modification operation data, obtain by hand-kept, the process of image data is loaded down with trivial details, time is long, easily careless omission, can not be in real time with the antiaircraft gun that collects or the position of rocket gun, launch azimuth, the inclination angle, information such as projectile quantity in time feed back to the Weather Modification Operation Command System Based center in a distant place, having affected command centre adversely assesses timely to executing the effect of penetrating, tend to miss the optimum position of timely adjustment antiaircraft gun or rocket gun, launch azimuth, the inclination angle, on the opportunity of projectile quantity, cause the Weather modification operation poor effect.
Summary of the invention:
In order to overcome the deficiency of existing antiaircraft gun or the artificial image data technology of rocket gun Weather modification operation, the purpose of this utility model provides a kind of Weather modification operation antiaircraft gun real time data acquisition device.Should be installed on antiaircraft gun or the rocket gun by real-time collector, position, launch azimuth, inclination angle, the projectile quantity information of the antiaircraft gun gathering in real time and record or rocket gun in time can be fed back to the command centre in a distant place, according to the information that collects antiaircraft gun or rocket gun Weather modification operation effect are carried out real-time assessment by command centre, and according to assessment result, instruct on-the-spot antiaircraft gun or rocket gun Weather modification operation, in time adjust the position of antiaircraft gun or rocket gun, launch azimuth, inclination angle, projectile quantity are to reach best operation effectiveness.
Goal of the invention of the present utility model is achieved in that a kind of Weather modification operation antiaircraft gun real time data acquisition device, and described real-time collector comprises that at least a information sensor, data are collected control module, data upload machine and is the system power supply of real-time collector power supply; Described data are collected control module and are included single-chip microcomputer, A/D change-over circuit and amplifying circuit of analog signal, the signal output of described information sensor is input to described single-chip microcomputer through amplifying circuit of analog signal and A/D change-over circuit, this single-chip microcomputer is connected with the data upload machine by interface circuit, and described information sensor is arranged on the corresponding information collection point on the big gun body.
Described real-time collector comprises barrel obliquity sensor, projectile sensor for countering, barrel aspect sensor; Described barrel obliquity sensor, projectile sensor for countering are integrated in the box body and are installed on the barrel; Described barrel aspect sensor, data are collected control module, data upload machine and are that the system power supply that real-time collector is powered is integrated on the structure casing, and this casing is installed on the barrel rotation platform.
Described real-time collector also comprises the emplacement coordinate sensor; Described emplacement coordinate sensor is integrated on the described structure casing.
Described data upload machine is the GPRS transport module.
Described barrel obliquity sensor is a kind of among gravity dip angle measuring appliance, the mechanical tilt sensor.
Described barrel aspect sensor is a kind of among electronic compass, the mechanical azimuthal sensor.
Described projectile sensor for countering is a kind of among acceleration transducer, the sound transducer.
Described emplacement coordinate sensor is global positioning system (GPS).
Effect of the present utility model is:
1, the utility model has adopted sensor sensing measuring technique scheme, realized data collection in real time automatically, and rapidly the information of gathering is passed to distant place control centre by the GPRS remote-transmission module, antiaircraft gun or rocket gun Weather modification operation effect are assessed according to the information that collects by command centre, and according to assessment result, instruct on-the-spot antiaircraft gun or rocket gun Weather modification operation, in time adjust the position of antiaircraft gun or rocket gun, launch azimuth, inclination angle, projectile quantity make antiaircraft gun or rocket gun Weather modification operation reach best operation effectiveness.
2, each unit module integrated level height of the present utility model is simple in structure, and simple installation, protective are good.
The utility model is described in further detail below in conjunction with drawings and Examples.
Description of drawings:
Fig. 1 is circuit theory diagrams of the present utility model;
Fig. 2 is that data of the present utility model are collected the control module circuit theory diagrams;
Fig. 3 is the scheme of installation of the utility model on the big gun body.
The specific embodiment
Embodiment:
Present embodiment provides a preferred forms of the present utility model.
Referring to Fig. 1, Fig. 2, Fig. 3, in the present embodiment, collector comprises that 4 kinds of information sensors such as barrel obliquity sensor 3-1, projectile sensor for countering 3-3, barrel aspect sensor 3-2, emplacement coordinate sensor 3-4 and data are collected control module 2, data upload machine 1 and is the system power supply of real-time collector power supply in real time; Described data are collected control module and are included single-chip microcomputer 2-1, A/D change-over circuit 2-2 and amplifying circuit of analog signal 2-3, the signal output of 4 kinds of information sensors is input to described single-chip microcomputer through amplifying circuit of analog signal and A/D change-over circuit, and this single-chip microcomputer is connected with the data upload machine by interface circuit.Described 4 information sensors are arranged on the corresponding information collection point on the big gun body, and wherein, described barrel obliquity sensor, projectile sensor for countering are integrated in the box body 8 and are installed on the barrel 9, gather barrel inclination angle, projectile quantity information from barrel; Described barrel aspect sensor, emplacement coordinate sensor, data are collected control module, data upload machine and are that the system power supply that real-time collector is powered is integrated on the structure casing 7, this casing is installed on the barrel rotation platform 10, gathers launch azimuth, emplacement coordinate information by described barrel aspect sensor, emplacement coordinate sensor.
In the present embodiment, described data upload machine is the GPRS transport module, and model can be moral letter PIML.By 485,232 interfaces, the GPRS transport module can be with transfer of data to command centre.
In the present embodiment, described single-chip microcomputer, A/D change-over circuit and amplifying circuit of analog signal are known general-purpose devices.
In the present embodiment, system power supply is the 12VDC dc source, can convert the 12VDC dc source to through the AC-DC inverter by civil power 220VAC.System power supply also can be the 12V battery, and for this battery is equipped with the 220V charger, when no civil power provided, battery also can be powered and be powered in 24 hours.
In the present embodiment, the barrel obliquity sensor is an XW02-1S2422 type gravity dip angle measuring appliance.The barrel obliquity sensor also can be the mechanical tilt sensor.
In the present embodiment, the barrel aspect sensor is a LP3201 type electronic compass.The barrel aspect sensor also can the mechanical azimuthal sensor.
In the present embodiment, the projectile sensor for countering is a sound transducer.The projectile sensor for countering also can be an acceleration transducer.The benefit that operation projectile amount adopts kinetic energy sensing counting modes such as acceleration transducer or sound transducer to count is when transmitter appearance emission is unsuccessful, because its kinetic energy can't trigger sensor, will not count.Therefore adopt kinetic energy sensing counting mode counting, data record is more accurate.
In the present embodiment, the emplacement coordinate sensor is global positioning system (GPS).The information that can use M387 type global location device to gather the emplacement coordinate in real time.
Launch point in some fixed emplacements, antiaircraft gun or rocket gun coordinate information are fixing known, the information of gathering the antiaircraft gun or the rocket gun of these fixed emplacements, and employed real-time collector can not comprise global positioning system (GPS).
In real time the operation principle of collector is: 4 kinds of information sensors are delivered to data with the Dynamic Signal of antiaircraft gun or rocket gun current state and collect control module, data are collected and are delivered to the A/D change-over circuit control module amplifies analog signal by amplifying circuit after, the A/D change-over circuit becomes data signal to deliver to single-chip microcomputer analog signal conversion, single-chip microcomputer is packed by routine processes, information after single-chip microcomputer is handled reaches the data upload machine then, the data upload machine passes to data by the wireless network in the command centre 5 command centre's central data collection device 6 in a distant place, antiaircraft gun or rocket gun Weather modification operation effect are assessed according to the information that collects by command centre, and according to assessment result, instruct on-the-spot antiaircraft gun or rocket gun Weather modification operation, in time adjust the position of antiaircraft gun or rocket gun, launch azimuth, the inclination angle, projectile quantity makes antiaircraft gun or rocket gun Weather modification operation reach best operation effectiveness.
Claims (8)
1. Weather modification operation antiaircraft gun real time data acquisition device is characterized in that: described real-time collector comprises that at least a information sensor, data collect control module, data upload machine and be the system power supply of real-time collector power supply; Described data are collected control module and are included single-chip microcomputer, A/D change-over circuit and amplifying circuit of analog signal, the signal output of described information sensor is input to described single-chip microcomputer through amplifying circuit of analog signal and A/D change-over circuit, this single-chip microcomputer is connected with the data upload machine by interface circuit, and described information sensor is arranged on the corresponding information collection point on the big gun body.
2. real-time collector according to claim 1 is characterized in that: described real-time collector comprises barrel obliquity sensor, projectile sensor for countering, barrel aspect sensor; Described barrel obliquity sensor, projectile sensor for countering are integrated in the box body and are installed on the barrel; Described barrel aspect sensor, data are collected control module, data upload machine and are that the system power supply that real-time collector is powered is integrated on the structure casing, and this casing is installed on the barrel rotation platform.
3. real-time collector according to claim 2 is characterized in that: described real-time collector also comprises the emplacement coordinate sensor, and described emplacement coordinate sensor is integrated on the described structure casing.
4. real-time collector according to claim 1 is characterized in that: described data upload machine is the GPRS transport module.
5. real-time collector according to claim 2 is characterized in that: described barrel obliquity sensor is a kind of among gravity dip angle measuring appliance, the mechanical tilt sensor.
6. real-time collector according to claim 2 is characterized in that: described barrel aspect sensor is a kind of among electronic compass, the mechanical azimuthal sensor.
7. real-time collector according to claim 2 is characterized in that: described projectile sensor for countering is a kind of among acceleration transducer, the sound transducer.
8. real-time collector according to claim 3 is characterized in that: described emplacement coordinate sensor is global positioning system (GPS).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009203075521U CN201476702U (en) | 2009-08-07 | 2009-08-07 | Real-time data acquisition device for anti-aircraft gun for weather modification operation |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009203075521U CN201476702U (en) | 2009-08-07 | 2009-08-07 | Real-time data acquisition device for anti-aircraft gun for weather modification operation |
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| CN201476702U true CN201476702U (en) | 2010-05-19 |
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| CN2009203075521U Expired - Fee Related CN201476702U (en) | 2009-08-07 | 2009-08-07 | Real-time data acquisition device for anti-aircraft gun for weather modification operation |
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Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102221309A (en) * | 2011-05-20 | 2011-10-19 | 陕西中天火箭技术有限责任公司 | Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method |
| CN102346002A (en) * | 2010-07-30 | 2012-02-08 | 江苏泰达机电设备有限责任公司 | Antiaircraft gun continuous shooting command simulation route generating system |
| CN102589351A (en) * | 2012-03-07 | 2012-07-18 | 成都信息工程学院 | Digitizing collection device and detection method based on antiaircraft gun operation parameter of weather modification |
| CN102754576A (en) * | 2012-06-25 | 2012-10-31 | 成都润联科技开发有限公司 | Automatic artificial influence weather system operation platform and realization method thereof |
| CN103123244A (en) * | 2011-11-18 | 2013-05-29 | 中国兵器科学研究院 | 57mm digitalized figure antiaircraft gun system |
| CN103808209A (en) * | 2014-02-21 | 2014-05-21 | 成都信息工程学院 | Digital acquisition device azimuth angle algorithm based on figure anti-aircraft gun operation |
| RU2539707C1 (en) * | 2013-12-17 | 2015-01-27 | Открытое акционерное общество "Радиозавод" | Control over artillery units fire |
| CN104567547A (en) * | 2015-01-08 | 2015-04-29 | 成都信息工程学院 | Operating data acquiring system and data processing method for silhouette rocket |
| CN104932034A (en) * | 2015-06-16 | 2015-09-23 | 中国气象科学研究院 | Man-made influence weather operation data acquisition and recognition system and method thereof |
| CN105004227A (en) * | 2014-04-21 | 2015-10-28 | 中国兵器科学研究院 | Silhouette rocket and silhouette antiaircraft gun cooperative control system based on wireless network |
| CN105532339A (en) * | 2015-12-30 | 2016-05-04 | 雷神科技（天津）有限公司 | Two-way firing type weather modification antiaircraft gun system |
| CN105608865A (en) * | 2015-12-17 | 2016-05-25 | 安徽诺安信息科技有限公司 | IMU data acquisition and processing system associated with meteorological data |
| CN105806389A (en) * | 2016-03-25 | 2016-07-27 | 成都信息工程大学 | Figure antiaircraft gun simulation system and control method |
| CN106969667A (en) * | 2017-05-10 | 2017-07-21 | 成都信息工程大学 | A kind of shadow rocket meticulous process intelligent acquisition device and data processing method |
| CN110237469A (en) * | 2019-07-18 | 2019-09-17 | 成都福禄泰安全技术有限公司 | A kind of fire-fighting monitor body |
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2009
- 2009-08-07 CN CN2009203075521U patent/CN201476702U/en not_active Expired - Fee Related
Cited By (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102346002A (en) * | 2010-07-30 | 2012-02-08 | 江苏泰达机电设备有限责任公司 | Antiaircraft gun continuous shooting command simulation route generating system |
| CN102346002B (en) * | 2010-07-30 | 2013-10-23 | 江苏泰达机电设备有限责任公司 | Antiaircraft gun continuous shooting command simulation route generating system |
| CN102221309A (en) * | 2011-05-20 | 2011-10-19 | 陕西中天火箭技术有限责任公司 | Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method |
| CN102221309B (en) * | 2011-05-20 | 2014-01-01 | 陕西中天火箭技术股份有限公司 | Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method |
| CN103123244A (en) * | 2011-11-18 | 2013-05-29 | 中国兵器科学研究院 | 57mm digitalized figure antiaircraft gun system |
| CN102589351B (en) * | 2012-03-07 | 2014-11-26 | 成都信息工程学院 | Digitizing collection device and detection method based on antiaircraft gun operation parameter of weather modification |
| CN102589351A (en) * | 2012-03-07 | 2012-07-18 | 成都信息工程学院 | Digitizing collection device and detection method based on antiaircraft gun operation parameter of weather modification |
| CN102754576A (en) * | 2012-06-25 | 2012-10-31 | 成都润联科技开发有限公司 | Automatic artificial influence weather system operation platform and realization method thereof |
| CN102754576B (en) * | 2012-06-25 | 2014-12-17 | 成都润联科技开发有限公司 | Automatic artificial influence weather system operation platform |
| RU2539707C1 (en) * | 2013-12-17 | 2015-01-27 | Открытое акционерное общество "Радиозавод" | Control over artillery units fire |
| CN103808209A (en) * | 2014-02-21 | 2014-05-21 | 成都信息工程学院 | Digital acquisition device azimuth angle algorithm based on figure anti-aircraft gun operation |
| CN103808209B (en) * | 2014-02-21 | 2016-06-01 | 成都信息工程学院 | A kind of based on shadow antiaircraft gun operation numeralization collecting device azimuth algorithm |
| CN105004227A (en) * | 2014-04-21 | 2015-10-28 | 中国兵器科学研究院 | Silhouette rocket and silhouette antiaircraft gun cooperative control system based on wireless network |
| CN104567547A (en) * | 2015-01-08 | 2015-04-29 | 成都信息工程学院 | Operating data acquiring system and data processing method for silhouette rocket |
| CN104932034A (en) * | 2015-06-16 | 2015-09-23 | 中国气象科学研究院 | Man-made influence weather operation data acquisition and recognition system and method thereof |
| CN104932034B (en) * | 2015-06-16 | 2017-04-05 | 中国气象科学研究院 | A kind of collection of Weather modification operation data and identifying system and its method |
| CN105608865A (en) * | 2015-12-17 | 2016-05-25 | 安徽诺安信息科技有限公司 | IMU data acquisition and processing system associated with meteorological data |
| CN105532339A (en) * | 2015-12-30 | 2016-05-04 | 雷神科技（天津）有限公司 | Two-way firing type weather modification antiaircraft gun system |
| CN105532339B (en) * | 2015-12-30 | 2018-06-22 | 雷神科技（天津）有限公司 | Two-way trigger type figure antiaircraft gun system |
| CN105806389A (en) * | 2016-03-25 | 2016-07-27 | 成都信息工程大学 | Figure antiaircraft gun simulation system and control method |
| CN105806389B (en) * | 2016-03-25 | 2017-11-07 | 成都信息工程大学 | A kind of figure antiaircraft gun simulation system and control method |
| CN106969667A (en) * | 2017-05-10 | 2017-07-21 | 成都信息工程大学 | A kind of shadow rocket meticulous process intelligent acquisition device and data processing method |
| CN106969667B (en) * | 2017-05-10 | 2018-06-05 | 成都信息工程大学 | A kind of bullet number detection data processing method of shadow rocket meticulous process intelligent acquisition device |
| CN110237469A (en) * | 2019-07-18 | 2019-09-17 | 成都福禄泰安全技术有限公司 | A kind of fire-fighting monitor body |
| CN110237469B (en) * | 2019-07-18 | 2024-05-24 | 成都福禄泰安全技术有限公司 | Fire monitor body |
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| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100519 Termination date: 20110807 |