CN204555828U - A kind of meteorological shadow rocket gun information collecting device - Google Patents

A kind of meteorological shadow rocket gun information collecting device Download PDF

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Publication number
CN204555828U
CN204555828U CN201520184610.1U CN201520184610U CN204555828U CN 204555828 U CN204555828 U CN 204555828U CN 201520184610 U CN201520184610 U CN 201520184610U CN 204555828 U CN204555828 U CN 204555828U
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China
Prior art keywords
potentiometer
data acquisition
end connector
detection module
collecting device
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Expired - Fee Related
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CN201520184610.1U
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Chinese (zh)
Inventor
文勇
文斌
肖秧琳
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Chengdu University of Information Technology
Chengdu Information Technology Co Ltd of CAS
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Chengdu Information Technology Co Ltd of CAS
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Abstract

The utility model discloses a kind of meteorological shadow rocket gun information collecting device, comprises data acquisition module, and the azimuth detection module be connected with data acquisition module respectively, angle of pitch detection module and bullet number detection module; Azimuth detection module comprises potentiometer R12 and potentiometer R8, potentiometer R12 one end connects power supply, and the other end is by resistance R9 ground connection, and potentiometer R8 one end connects power supply, the other end is by resistance R10 ground connection, and the output of potentiometer R12 and potentiometer R8 is connected respectively to data acquisition module.The utility model can collect the potentiometer linear with azimuthal variation voltage, with the angle of pitch change the output voltage of linear pitch reference, the number of times of the output voltage corresponding with bullet number, contribute to obtaining the azimuth of rocket gun operation, the angle of pitch and bullet number by follow-up data processing, this apparatus structure is simple, with low cost, image data is precise and stable.

Description

A kind of meteorological shadow rocket gun information collecting device
Technical field
The utility model relates to meteorological shadow rocket gun information gathering data fields, is specially a kind of meteorological shadow rocket gun information collecting device.
Background technology
In recent years; because mankind's activity exacerbates the change of climatic environment; diastrous weather frequently occurs; in order to prevent and reduce natural disasters; the means of shadow service are enriched constantly; operational benefit is also improving constantly, weather modification preventing and reducing natural disasters, the field such as ecological environmental protection construction and great social activities guarantee plays the effect become more and more important.The information intelligence back-stage management platform of the current shadow and software have started application all, play a significant role in the management process of drinking water project.But penetrate on last one kilometer that job information gathers as information system management automatically also to be strengthened at big gun.
Relative to antiaircraft gun, rocket car moves the relatively-stationary reference point of neither one everywhere, and azimuthal automatic collection has certain difficulty.Gathered by high-precision electronic compass at present, because rocket is all-metal construction, have great interference to compass, the common practice is by an aluminum frame, keeps a segment distance to measure with barrel.Its shortcoming has be high-precision electronic compass itself very expensive, uneconomical at three: one; Two is on rocket gun, have more a special-shaped structure, and attractive in appearance, safety is all subject to certain impact; Three is because electronic compass is nonlinear transducer, adopt the stability of data, precision is all subject to certain restriction.
Big gun is penetrated operation work and rest and is also comprised basic unit's drinking water project beginning and ending time, shell transmitting quantity and the angle of pitch etc., accurately and timely sending to of these information, is the basic data of operation effectiveness assessment and operation appropriation budget.
Utility model content
Be to provide a kind of based on the meteorological shadow rocket gun information collecting device for gathering the data relevant to the azimuth of rocket gun operation, the angle of pitch and bullet number of linear electron device for the problems referred to above the purpose of this utility model, technical scheme is as follows:
A kind of meteorological shadow rocket gun information collecting device, comprises data acquisition module, and the azimuth detection module be connected with data acquisition module respectively, angle of pitch detection module and bullet number detection module; Described azimuth detection module comprises potentiometer R12 and potentiometer R8, described potentiometer R12 one end connects power supply, the other end is by resistance R9 ground connection, described potentiometer R8 one end connects power supply, the other end is by resistance R10 ground connection, and the output of potentiometer R12 and potentiometer R8 is connected respectively to data acquisition module.
Further, the resistive element of described potentiometer R12 and potentiometer R8 is annular, annular electro resistance body is provided with the knob slided for controlling potential device brush.
Further, described angle of pitch detection module adopts LCA310 type obliquity sensor.
Further, described bullet number detection module comprises three end connectors, namely controls the A end connector that header is connected, the B end connector be connected with gun tube end with rocket launching, and the C end connector be connected with described data acquisition module; Described A end connector connects B end connector, and C end connector is connected between A end connector and B end connector by diode and bleeder circuit, and the negative pole of diode connects C end connector.
Further, the GPS module be connected with described data acquisition module is also comprised.
Further, the GPRS module be connected with described data acquisition module is also comprised.
The beneficial effects of the utility model are: the utility model can collect the potentiometer linear with azimuthal variation voltage, with the angle of pitch changes the output voltage of linear pitch reference, the voltage corresponding with bullet number exports number of times, contribute to obtaining the azimuth of rocket gun operation, the angle of pitch and bullet number by follow-up data processing, this apparatus structure is simple, with low cost, image data is precise and stable.
Accompanying drawing explanation
Fig. 1 is the circuit theory diagrams of the utility model meteorological shadow rocket gun information collecting device.
Fig. 2 is the utility model meteorological shadow rocket gun information collecting device azimuth detection module circuit theory diagrams.
Fig. 3 is that the meteorological shadow rocket gun information collecting device scheme of installation of the utility model and azimuth gather control panel schematic diagram.Fig. 4 is the utility model meteorological shadow rocket gun information collecting device bullet number detection module circuit theory diagrams.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described further: as shown in Figure 1, a kind of meteorological shadow rocket gun information collecting device, comprise data acquisition module, and the azimuth detection module be connected with data acquisition module respectively, angle of pitch detection module and bullet number detection module.
As shown in Figure 2, azimuth detection module comprises potentiometer R12 and potentiometer R8, described potentiometer R12 one end connects power supply, the other end is by resistance R9 ground connection, described potentiometer R8 one end connects power supply, the other end is by resistance R10 ground connection, and the output of potentiometer R12 and potentiometer R8 is connected respectively to data acquisition module.
Because the voltage being added in potentiometer two ends is DC voltage, potentiometer inside is pure resistance material, and resistance is linear unit, will obtain the output voltage of linear change when thus brush slides.Comparatively electronic compass is stable, precision is high for this measuring method, and expense is extremely cheap, and is installed together with gun tube, unaffected.
An embodiment of the present utility model, the resistive element of electric described potentiometer R12 and potentiometer R8 is annular, annular electro resistance body is provided with the knob slided for controlling potential device brush, as shown in Figure 3.In the process detected, the position of potentiometer R12 brush is positioned at Due South, and namely knob sensing is consistent with the direction of compass indication, and the direction that the position of potentiometer R8 brush and knob point to rocket gun tube is consistent.
Concrete measuring principle is as follows: first gun tube is turned to the positive north before measurement, and then by the knob of above-mentioned requirements regulator potentiometer R12 and potentiometer R8, make the knob of R12 point to Due South, the knob of R8 points to the positive north, now records the output voltage v of potentiometer R12 s, the output voltage v of potentiometer R8 n, the angle variable rate a (unit: radian/volt) that unit voltage change is corresponding can be drawn thus:
a = π v n - v s
Then the orientation turning to operation to need gun tube, again according to the knob of above-mentioned requirements regulator potentiometer R12 and potentiometer R8, make the knob of R12 point to Due South, the knob of R8 points to gun tube direction, now records the output voltage v of potentiometer R12 s', the output voltage v of potentiometer R8, then gun tube projection with the included angle A of Due South is:
A = ( v - v s ′ ) × π v n - v s
In actual job, can this device as a shadow rocket gun azimuth collector part be fixedly mounted on rocket gun tube launcher, as shown in Figure 3.Like this by the knob of potentiometer R8 regulate consistent with gun tube direction after, just do not need afterwards to regulate again, only need the knob of reference guide pin regulator potentiometer R12 each time.
Another embodiment of the present utility model, angle of pitch detection module adopts LCA310 type obliquity sensor, along with moving up and down of rocket gun tube, obliquity sensor output voltage U x-outchange thereupon, collect U x-outafter, only just need can obtain the angle of pitch by following calculating:
B=(U x-out-U 0)/β
Wherein, B is luffing angle, U x-outfor sensor output voltage, U 0for sensor zero point output voltage, i.e. the output voltage of gun tube when 0 angle), β is angular sensitivity (unit: mV/ °).
Another embodiment of the present utility model, bullet number detection module comprises three end connectors, namely controls the A end connector that header is connected, the B end connector be connected with gun tube end with rocket launching, and the C end connector be connected with described data acquisition module; Described A end connector connects B end connector, and C end connector is connected between A end connector and B end connector by diode and bleeder circuit, and the negative pole of diode connects C end connector.
Three end connectors for four pipe rocket guns are example, the internal structure of three end connectors is as shown in Figure 4: A end connector, B end connector and C end connector be ground connection GND simultaneously, 4 gun tube ignition leads are also connected with: CH1, CH2, CH3, CH4, from output OUT CH1, CH2, CH3, CH4 drawing respectively a line and be jointly connected to after bleeder circuit and diode C end connector between A end connector and B end connector.Output OUT connection data acquisition module.
After firing button a certain on rocket launching case is pressed, a circuit corresponding in gun tube ignition lead CH1, CH2, CH3, CH4 just has the voltage of 12V, C end connector just has a magnitude of voltage simultaneously, this magnitude of voltage is got by data acquisition module, often obtain a value and namely represent that one piece of rocket launching is gone out, so just can collect bullet number information.
Wherein, data acquisition module can select micro controller STM32F207, the analog voltage collected is carried out AD conversion, and then carries out the computing of the information such as azimuth, the angle of pitch, bullet number.Simultaneously by the beginning and ending time of real-time clock (RTC) Collecting operation of its inside.The inner RTC of STM32F207 has calendar function, by the format record calendar time of " Year/Month/Day/time/point/second ", therefore can record the beginning and ending time of drinking water project accurately with it.
Another embodiment of the present utility model, also comprises the GPS module be connected with described data acquisition module, can obtain the positional information of rocket gun.
Another embodiment of the present utility model, also comprises the GPRS module be connected with described data acquisition module, can cross this module and the data message collected is sent to mobile Internet.
The power module of powering for this device provides 9V and 3.3V supply voltage respectively, and 9V exports as azimuth detection module, angle of pitch detection module, GPRS module provide electricity.3.3V exports and powers for single-chip microcomputer, ADC reference voltage chip and GPS module.

Claims (6)

1. a meteorological shadow rocket gun information collecting device, is characterized in that, comprise data acquisition module, and the azimuth detection module be connected with data acquisition module respectively, angle of pitch detection module and bullet number detection module; Described azimuth detection module comprises potentiometer R12 and potentiometer R8, described potentiometer R12 one end connects power supply, the other end is by resistance R9 ground connection, described potentiometer R8 one end connects power supply, the other end is by resistance R10 ground connection, and the output of potentiometer R12 and potentiometer R8 is connected respectively to data acquisition module.
2. one according to claim 1 meteorological shadow rocket gun information collecting device, is characterized in that, the resistive element of described potentiometer R12 and potentiometer R8 is annular, annular electro resistance body is provided with the knob slided for controlling potential device brush.
3. one according to claim 1 meteorological shadow rocket gun information collecting device, is characterized in that, described angle of pitch detection module adopts LCA310 type obliquity sensor.
4. one according to claim 1 meteorological shadow rocket gun information collecting device, it is characterized in that, described bullet number detection module comprises three end connectors, namely the A end connector that header is connected, the B end connector be connected with gun tube end is controlled with rocket launching, and the C end connector be connected with described data acquisition module; Described A end connector connects B end connector, and C end connector is connected between A end connector and B end connector by diode and bleeder circuit, and the negative pole of diode connects C end connector.
5. the meteorological shadow rocket gun of the one according to any one of claim 1-4 information collecting device, is characterized in that, also comprise the GPS module be connected with described data acquisition module.
6. the meteorological shadow rocket gun of the one according to any one of claim 1-4 information collecting device, is characterized in that, also comprise the GPRS module be connected with described data acquisition module.
CN201520184610.1U 2015-03-30 2015-03-30 A kind of meteorological shadow rocket gun information collecting device Expired - Fee Related CN204555828U (en)

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Application Number Priority Date Filing Date Title
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CN107643105A (en) * 2017-10-30 2018-01-30 程鹏 A kind of weather modification rocket launcher detector
CN108088412A (en) * 2016-11-23 2018-05-29 北京地林远景信息技术有限公司 A kind of method at total powerstation automatic And Rapid Determination agricultural rocket gun azimuth inclination angle

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108088412A (en) * 2016-11-23 2018-05-29 北京地林远景信息技术有限公司 A kind of method at total powerstation automatic And Rapid Determination agricultural rocket gun azimuth inclination angle
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
CN107643105A (en) * 2017-10-30 2018-01-30 程鹏 A kind of weather modification rocket launcher detector
CN107643105B (en) * 2017-10-30 2024-04-02 程鹏 Weather modification rocket launcher detector

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150812

Termination date: 20160330

CF01 Termination of patent right due to non-payment of annual fee