CN114111643A - Equipment post capable of being used for positioning and orientation - Google Patents
Equipment post capable of being used for positioning and orientation Download PDFInfo
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- CN114111643A CN114111643A CN202111451176.5A CN202111451176A CN114111643A CN 114111643 A CN114111643 A CN 114111643A CN 202111451176 A CN202111451176 A CN 202111451176A CN 114111643 A CN114111643 A CN 114111643A
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- satellite navigation
- navigation system
- global satellite
- orientation
- post
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
- G01B11/26—Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
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- General Physics & Mathematics (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The invention belongs to the technical field of measurement. Based on the fact that the existing marker post is used as a common working equipment for artillery and is single in function, the invention provides the equipment marker post capable of being used for positioning and orientation. The marker post comprises a marker post body and a preposed orientation instrument; the preposed orientation instrument is arranged at the top of the post body and is provided with a shell, a power supply module and a second global satellite navigation module; the power supply module is arranged in the shell and provides power for the whole preposed direction finder; the second global satellite navigation system is arranged in the shell and is in communication connection with the first global satellite navigation system at the gun position; the north angle of the base line of the marker post and the gun position can be measured, then the marker post is aimed by combining the sighting device for the gun, and the north angle of the gun barrel can be calculated by utilizing the sighting device value, so that the purpose of gun orientation is realized.
Description
Technical Field
The invention belongs to the technical field of measurement, and particularly relates to an equipment marker post capable of being used for positioning and orientation.
Background
The marker post is a measuring tool, is in a rod shape and is mainly used for indicating a measuring point. The marker post is inserted into the measuring point during use, so that a measuring person can accurately observe the measuring point. The marker post is used as an operation equipment frequently used by artillery, and is mainly used as an aiming point manually set.
With the continuous development of digitalization and informatization, the requirements on functions and precision of equipment are more and more, and the marker post is used as an operation equipment frequently used by artillery and is supposed to play a greater role.
Disclosure of Invention
Based on the problem of single function of the existing marker post when used for artillery operation, the invention aims to provide an equipment marker post capable of being used for positioning and orientation, wherein the marker post can be used for positioning and orientation (measuring the shot of an artillery barrel).
In order to achieve the purpose, the invention adopts the following technical scheme:
an instrumented mast usable for positional orientation for gun position sighting, the gun position having a gun sight and a first global satellite navigation system, comprising:
a post body;
the preposed orientation instrument is arranged at the top of the mark post body and comprises a shell, a power supply module and a first global satellite navigation system;
the power supply module supplies power to the whole preposed orientation instrument and is arranged in the shell;
the second global satellite navigation system part is arranged in the shell;
the second global satellite navigation system is capable of being communicatively coupled to the first global satellite navigation system at the gun position.
By adopting the structure, the global satellite navigation module and the first global satellite navigation system at the gun position form double global satellite navigation direction finding, the north angle of the baseline at the marker post and the gun position can be measured, then the marker post is aimed by combining the sighting device for the gun, and the north angle of the gun barrel can be calculated by utilizing the sighting device value, so that the purpose of gun orientation is realized.
In one embodiment of the present invention, the front direction finder further includes:
the communication control panel is arranged in the shell and is connected with the second global satellite navigation system, and the communication control panel is provided with a wired interface; the wired interface is arranged on the peripheral wall of the shell;
wherein the wired interface is connectable with a first global satellite navigation system at the gun position.
In one technical scheme disclosed by the invention, the prepositive orientation instrument further comprises a wireless communication module which is connected with the communication control panel; the wireless communication module is provided with a communication antenna and a wireless interface, the communication antenna is arranged at the bottom of the shell, the wireless interface can be communicated with the first global satellite navigation system at the gun position, and the wireless mode and the wired mode can be switched as required.
In one technical scheme disclosed by the invention, the preposed orientation instrument is also provided with a man-machine interaction module, and the man-machine interaction module is in communication connection with the second global satellite navigation system and the power supply module.
In one technical scheme disclosed by the invention, the man-machine interaction module is provided with an operation display panel, and the operation display panel is arranged on the peripheral wall of the shell; and the operation display panel is provided with a power switch and a work indicator lamp.
In one technical scheme disclosed by the invention, the prepositive orientation instrument further comprises a beacon light, and the beacon light is arranged on the shell.
In one technical scheme disclosed by the invention, the prepositive orientation instrument further comprises a beacon light and a beacon light switch, wherein the beacon light is arranged at the bottom area of the operation display panel, and the beacon light switch is arranged on the operation display panel.
In one aspect of the disclosure, the second gnss has a second gnss antenna; the second global satellite navigation system antenna is arranged on the top of the shell.
In one technical scheme disclosed by the invention, the power supply module is provided with a battery and a charging interface; wherein the battery is built in the housing; the interface that charges sets up on the periphery wall of casing.
In one technical scheme disclosed by the invention, the top of the mark post body is provided with a screw hole which is provided with an internal thread; the bottom of casing is equipped with the sighting rod and connects, the sighting rod connect be equipped with the screw internal thread adaptation's external screw for fix leading direction finder.
In one technical scheme disclosed by the invention, the charging interface and the wired interface are both provided with protective covers.
As can be seen from the above description, the beneficial effects of the present invention are:
1. the top of the marker post body is additionally provided with a preposed orientation instrument, a second global satellite navigation system is arranged in the preposed orientation instrument, and the preposed orientation instrument and the first global satellite navigation system at the gun position can form double global satellite navigation system direction finding, so that the functions of positioning and gun orientation can be realized;
2. meanwhile, two modes of wired transmission and wireless transmission are arranged, different transmission modes can be selected according to actual conditions to transmit satellite navigation data, and the application range is wider.
3. Finally, the front orientation device is also provided with a beacon light, and the beacon light can be turned on at night or under the condition of poor illumination, so that the aiming is facilitated.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings needed to be used in the embodiments or technical descriptions will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present application, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of a front orientation apparatus according to the present invention;
FIG. 3 is a block diagram of the circuitry of the front pointing device of the present invention.
Reference numerals: 1-a post body; 2-preposition orientation instrument; 21-a housing; 211-pole joint; 22-a second global satellite navigation module; 221-a second global satellite navigation system; 222-a second global satellite navigation system antenna; 23-a communication control board; 231-a wired interface; 24-a power supply module; 241-a battery; 242-a charging interface; 25-a man-machine interaction module; 251-operating a display panel; 2511-a work indicator light; 2513-power switch; 26-beacon light; 261-beacon light switch; 27-a wireless communication module; 271-communication antenna.
Detailed Description
In the following, only certain exemplary embodiments are briefly described. As those skilled in the art will recognize, the described embodiments may be modified in various different ways, all without departing from the spirit or scope of the present invention. Accordingly, the drawings and description are to be regarded as illustrative in nature, and not as restrictive.
In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; the connection can be mechanical connection, electrical connection or communication; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly above and obliquely above the second feature, or simply meaning that the first feature is at a lesser level than the second feature.
Embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
Based on the problem that the prior marker post for the cannon is only used for aiming and has single function; the embodiment of the invention discloses an equipment marker post capable of being used for positioning and orienting, which is used for artillery operation. The structure of the sighting device is shown in attached figures 1-3, and mainly comprises a sighting rod body 1 and a preposed direction finder 2.
Specifically, the top of the marker post body 1 is provided with a screw hole, and the preposed orientation instrument 2 is in threaded connection with the top of the marker post 1.
The front orientation device 2 comprises a shell 21, a second global satellite navigation module 22, a communication control panel 23, a power supply module 24, a man-machine interaction module 25 and a beacon light 26.
Wherein, the bottom central region of casing 21 is provided with sighting rod joint 211, and sighting rod joint 211 has the external screw thread, with the internal screw thread adaptation of the screw at sighting rod 1 top for leading direction finder 2 of fixed.
The power module 24 is partially disposed in the housing 21, provides power to the entire front orienter 2, and has a battery 241 and a charging interface 242.
Wherein a battery 241 is mounted within the housing 21 to provide power to the overall system of the front pointing device 2. In the present embodiment, the battery 241 is a lithium battery.
The charging interface 242 is provided on the outer peripheral wall of the case 21 for charging the lithium battery 241.
The second global satellite navigation module 22 is disposed in the housing 21 and is used for measuring satellite navigation data at the post body 1, and the second global satellite navigation module 22 mainly includes a second global satellite navigation system 221 and a second global satellite navigation system antenna 222.
A second gnss antenna 222 is disposed on the top of the housing 21 for receiving satellite signals.
The second gnss 221 is disposed in the housing 21 and is connected to the second gnss antenna 221.
The communication control board 23 is disposed in the housing 21 and is communicatively connected to the second global satellite navigation system 221 for transmitting satellite navigation data to the outside. The outer peripheral wall of the housing 21 is provided with a wired interface 231.
The human-machine interaction module 25 is disposed on the housing 21 at a position substantially on the outer peripheral wall of the housing 21 between the charging interface 242 and the wired interface 231, and has an operation display panel 251 for controlling and displaying the operation of the front orientation instrument 2. The operation display panel 251 is provided with an operation indicator 2511 and a power switch 2513. When the power switch 2513 is turned on, the gnss module 22 starts to operate, and the operation indicator 2511 is turned on accordingly. In this embodiment, the operation indicator 2511 is an LED lamp.
As the optimization scheme of this embodiment, the charging interface 242 and the wired interface 231 are both provided with protective covers, so that dust and moisture are prevented from entering the interior of the front orientation device 2, and the use accuracy and the service life of the front orientation device 2 are prevented from being affected.
As a preferable solution of the present embodiment, the front direction finder 2 further includes a beacon 26 and a beacon switch 261, the beacon 26 is disposed on the outer peripheral wall of the housing 21 in the bottom region of the operation display panel 251 and electrically connected to the power supply module 24, and the beacon switch 261 is disposed on the operation display panel 251. When the sighting device is used at night or under the condition of poor illumination, the beacon switch 261 can be turned on, and sighting is facilitated.
As an optimized solution of this embodiment, the front direction finder 2 further includes a wireless communication module 27 installed in the housing 21, communicatively connected to the power module 24 and the communication control board 23, and configured to wirelessly transmit satellite navigation data, and having a communication antenna 271, where the communication antenna 271 is disposed at the bottom of the housing 21 and located at one side of the post joint 211; and the data is transmitted in a wireless mode, so that the data transmission is more convenient and quicker.
The working mode of the embodiment of the invention is as follows: firstly, screwing a preposed orientation instrument 2 on the top of a mark post body 1; inserting the marker post body 1 to a target, turning on a power switch of the front-mounted orientation device 2, carrying out measurement work by the global satellite navigation module 22, and lighting a work indicator 2511 on the operation display panel 251; in the first global positioning system or the resolver which transmits satellite navigation data to the gun position in a wired or wireless way through the communication control panel 23 or the wireless communication module 27, the first global satellite navigation system and the second global satellite navigation system 221 form a double global satellite navigation system for direction measurement, baseline north angles at a sighting rod and a gun position can be measured, then the sighting target rod of a gun sighting device is combined to enable the gun barrel direction angle to be related with the baseline north angle, when the accuracy of data transmitted by the preposed orientation instrument 2 meets the requirement, the gun barrel north angle can be resolved, and the goal of orientation can be directly determined as a calibration division.
As can be seen from the above description, the beneficial effects of the present invention are: the top of the marker post body is additionally provided with a preposed orientation instrument, a second global satellite navigation system is arranged in the preposed orientation instrument, and the preposed orientation instrument and the first global satellite navigation system at the gun position can form double global satellite navigation system direction finding, so that the functions of positioning and gun orientation can be realized; furthermore, two modes of wired transmission and wireless transmission are simultaneously arranged, different transmission modes can be selected according to actual conditions to transmit satellite navigation data, and the application range is wider; finally, the front orientation device is also provided with a beacon light, and the beacon light can be turned on at night or under the condition of poor illumination, so that the aiming is facilitated.
The above-mentioned embodiments are intended to illustrate the objects, technical solutions and advantages of the present invention in further detail, and it should be understood that the above-mentioned embodiments are merely exemplary embodiments of the present invention, and are not intended to limit the scope of the present invention, and any modifications, equivalent substitutions, improvements and the like made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (10)
1. An instrumented mast usable for positional orientation for sighting at a gun location having a gun sight and a first global satellite navigation system, comprising:
a post body;
the preposed orientation instrument is arranged at the top of the mark post body and comprises a shell, a power supply module and a second global satellite navigation system;
the power supply module supplies power to the whole preposed orientation instrument and is arranged in the shell;
the second global satellite navigation system part is arranged in the shell;
the second global satellite navigation system is capable of being communicatively coupled to the first global satellite navigation system at the gun position.
2. The accessory post usable for positioning and orienting of claim 1, wherein said front orienter further comprises:
the communication control panel is arranged in the shell and is connected with the second global satellite navigation system, and the communication control panel is provided with a wired interface; the wired interface is arranged on the peripheral wall of the shell;
wherein the wired interface is connectable with a first global satellite navigation system at the gun position.
3. The outfitting post useful for positioning and orienting of claim 2, wherein:
the preposed orientation instrument also comprises a wireless communication module;
the wireless communication module is in communication connection with the communication control panel;
the wireless communication module is provided with a communication antenna and a wireless interface, and the communication antenna is arranged at the bottom of the shell; the wireless interface is capable of communicating with a first global satellite navigation system at the gun position.
4. The equipment post for positioning and orientation as claimed in claim 1, wherein the front orientation device further comprises a man-machine interaction module, and the man-machine interaction module is communicatively connected to the second gnss and the power supply module.
5. The equipment post usable for positioning and orienting of claim 4, wherein said human-machine interaction module has an operation display panel provided on a peripheral wall of said housing; and the operation display panel is provided with a power switch and a work indicator lamp.
6. The outfitting post useful for positioning and orienting of claim 1, wherein said front-facing orienter further comprises a beacon disposed on said housing.
7. The outfit post for positioning and orienting of claim 5, wherein said front orientation device further comprises a beacon and a beacon switch; the beacon light is arranged at the bottom area of the operation display panel, and the beacon light switch is arranged on the operation display panel.
8. The equipment post usable for positioning and orientation according to claim 1, wherein said second global satellite navigation system has a second global satellite navigation system antenna; the second global satellite navigation system antenna is arranged on the top of the shell.
9. The accessory post usable for positional orientation of claim 1, wherein the power module has a battery and a charging interface; wherein the battery is built in the housing; the interface that charges sets up on the periphery wall of casing.
10. The accessory post usable for positional orientation of claim 9, wherein the wired interface and the charging interface are each provided with a protective cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111451176.5A CN114111643A (en) | 2021-12-01 | 2021-12-01 | Equipment post capable of being used for positioning and orientation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111451176.5A CN114111643A (en) | 2021-12-01 | 2021-12-01 | Equipment post capable of being used for positioning and orientation |
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| Publication Number | Publication Date |
|---|---|
| CN114111643A true CN114111643A (en) | 2022-03-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111451176.5A Pending CN114111643A (en) | 2021-12-01 | 2021-12-01 | Equipment post capable of being used for positioning and orientation |
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| CN (1) | CN114111643A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6670917B1 (en) * | 1997-01-31 | 2003-12-30 | Trimble Navigation Limited | Balanced integrated position determination system and communication system |
| US7062305B1 (en) * | 2000-09-15 | 2006-06-13 | Trimble Navigation Limited | Location identifying apparatus and method of identifying the location of a user |
| US20080180319A1 (en) * | 2007-01-26 | 2008-07-31 | Mohammad Mojahedul Islam | Wireless utility asset mapping device and method |
| CN201983799U (en) * | 2010-12-31 | 2011-09-21 | 北京星网宇达科技开发有限公司 | High-accuracy detection and demarcation device of inertia orientation equipment |
| CN105180713A (en) * | 2015-08-18 | 2015-12-23 | 中国人民解放军军械工程学院 | Artillery body tube measuring device based on Beidou radio navigation satellite system (RNSS) |
| CN106500678A (en) * | 2015-09-04 | 2017-03-15 | 莱卡地球***公开股份有限公司 | Measurement bar |
| US20190302270A1 (en) * | 2018-04-03 | 2019-10-03 | Operations Technology Development, Nfp | Method and apparatus for improved gnss location detection |
| CN110686565A (en) * | 2019-09-25 | 2020-01-14 | 西安昆仑工业（集团）有限责任公司 | Zero position and true north calibration device and calibration method for vehicle-mounted 30 mm artillery system |
| US20210088334A1 (en) * | 2019-09-20 | 2021-03-25 | Joshua Bembenek | Survey Pole with Electronic Measurement and Automatic Signal Transmittal |
| CN213363561U (en) * | 2020-06-24 | 2021-06-04 | 西安昆仑工业（集团）有限责任公司 | Consistency calibration device for artillery system |
-
2021
- 2021-12-01 CN CN202111451176.5A patent/CN114111643A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6670917B1 (en) * | 1997-01-31 | 2003-12-30 | Trimble Navigation Limited | Balanced integrated position determination system and communication system |
| US7062305B1 (en) * | 2000-09-15 | 2006-06-13 | Trimble Navigation Limited | Location identifying apparatus and method of identifying the location of a user |
| US20080180319A1 (en) * | 2007-01-26 | 2008-07-31 | Mohammad Mojahedul Islam | Wireless utility asset mapping device and method |
| CN201983799U (en) * | 2010-12-31 | 2011-09-21 | 北京星网宇达科技开发有限公司 | High-accuracy detection and demarcation device of inertia orientation equipment |
| CN105180713A (en) * | 2015-08-18 | 2015-12-23 | 中国人民解放军军械工程学院 | Artillery body tube measuring device based on Beidou radio navigation satellite system (RNSS) |
| CN106500678A (en) * | 2015-09-04 | 2017-03-15 | 莱卡地球***公开股份有限公司 | Measurement bar |
| US20190302270A1 (en) * | 2018-04-03 | 2019-10-03 | Operations Technology Development, Nfp | Method and apparatus for improved gnss location detection |
| US20210088334A1 (en) * | 2019-09-20 | 2021-03-25 | Joshua Bembenek | Survey Pole with Electronic Measurement and Automatic Signal Transmittal |
| CN110686565A (en) * | 2019-09-25 | 2020-01-14 | 西安昆仑工业（集团）有限责任公司 | Zero position and true north calibration device and calibration method for vehicle-mounted 30 mm artillery system |
| CN213363561U (en) * | 2020-06-24 | 2021-06-04 | 西安昆仑工业（集团）有限责任公司 | Consistency calibration device for artillery system |
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