CN111260903A - Wireless data binding device - Google Patents
Wireless data binding device Download PDFInfo
- Publication number
- CN111260903A CN111260903A CN202010060633.7A CN202010060633A CN111260903A CN 111260903 A CN111260903 A CN 111260903A CN 202010060633 A CN202010060633 A CN 202010060633A CN 111260903 A CN111260903 A CN 111260903A
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- Prior art keywords
- ground
- missile
- equipment
- wireless
- borne
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Classifications
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J50/00—Circuit arrangements or systems for wireless supply or distribution of electric power
- H02J50/20—Circuit arrangements or systems for wireless supply or distribution of electric power using microwaves or radio frequency waves
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L2012/40208—Bus networks characterized by the use of a particular bus standard
- H04L2012/40215—Controller Area Network CAN
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Power Engineering (AREA)
- Signal Processing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a wireless data binding device, which comprises an missile-borne computer (3), ground equipment (1), missile-borne equipment (4) and a ground measurement and launch control system (2); the ground equipment (1) is fixed on the ground, and the pop-up equipment (4) is fixed on the cannonball and is in wireless connection with the ground equipment (1) to realize information transmission; the ground equipment (1) is connected with the ground measurement and launch control system (2) and is used for receiving a control signal of the ground measurement and launch control system (2) and transmitting information sent by the sprung equipment (4) to the ground measurement and launch control system (2); the missile-borne device (4) is connected with the missile-borne computer (3) and used for transmitting the information sent by the ground device (1) to the missile-borne computer and supplying power to the missile-borne device and the ground device. The wireless data binding device can realize continuous emission and quick emission and can ensure safety.
Description
Technical Field
The invention belongs to the technical field of missile launching control, and particularly relates to a wireless data binding device.
Background
Currently, a guided projectile is mainly subjected to system butt joint test through a disconnecting and inserting and ground test launching control system, data binding before launching and on-projectile thermal battery activation. Due to the limitation of the size of the barrel, the shells must be pulled out and inserted after being loaded into the barrel, and the guided shells cannot communicate with a ground test and launch control system through the insertion and the removal, so that the shells need to complete the whole shell test, data binding and thermal battery activation before being loaded into the barrel, and the shells are loaded into the barrel after the thermal battery activation and complete the launch test within the specified time.
The guided projectile is launched after the battery is activated, continuous launching can not be carried out, meanwhile, the battery is placed into the barrel after activation, certain safety risk exists, the launching strategy is difficult to adapt to the requirements of a simple launching field on convenient and fast launching, and the actual combat requirement can not be met.
Disclosure of Invention
In view of the above drawbacks and needs of the prior art, the present invention provides a wireless data binding apparatus, which includes a ground device and a pop-up device, wherein the ground device and the pop-up device are wirelessly connected for information transmission, the pop-up device is fixed on a projectile, the ground device is fixed on the ground, both the ground device and the pop-up device are connected to a pop-up computer, the pop-up computer sends control information to the ground device, the ground device transmits the control information to the pop-up device, thereby controlling the projectile, and transmitting information of the projectile to the pop-up computer through the ground device.
In order to achieve the purpose, the invention provides a wireless data binding device, which comprises an missile-borne computer, ground equipment, missile-borne equipment and a ground measurement and launch control system;
the ground equipment is fixed on the ground, and the pop-up equipment is fixed on the cannonball and is in wireless connection with the ground equipment to realize information transmission;
the ground equipment is connected with the ground measurement and launch control system and is used for receiving a control signal of the ground measurement and launch control system and transmitting information sent by the sprung equipment to the ground measurement and launch control system; the missile-borne equipment is connected with the missile-borne computer and used for transmitting the information sent by the ground equipment to the missile-borne computer and supplying power to the missile-borne equipment and the ground equipment.
Furthermore, the ground equipment comprises a first antenna, a first wireless transmission module and a first data processing module, the first data processing module is connected with the ground measurement and launch control system in a two-way mode, one end of the first wireless transmission module is connected with the first data processing module in a two-way mode, and the other end of the first wireless transmission module is connected with the first antenna in a two-way mode.
Furthermore, the ground equipment comprises a wireless charging transmitting module, and the wireless charging transmitting module is connected with the ground measurement transmitting system through a cable.
Furthermore, the pop-up device comprises a second antenna, a second wireless transmission module and a second data processing module, the second data processing module is connected with the pop-up computer in a bidirectional mode, one end of the second wireless transmission module is connected with the second data processing module, and the other end of the second wireless transmission module is connected with the second antenna.
Furthermore, still be equipped with on the equipment on the bullet with the wireless receiving module that charges of missile-borne computer cable connection.
Further, a voltage stabilizing module is arranged between the wireless charging receiving module and the missile-borne computer.
Furthermore, a bidirectional CAN bus is connected between the ground equipment and the missile-borne computer and between the missile-borne computer and the missile-borne equipment.
In general, compared with the prior art, the above technical solution contemplated by the present invention can achieve the following beneficial effects:
(1) the wireless data binding device is provided with ground equipment and missile-borne equipment which are wirelessly connected for information transmission, wherein the missile-borne equipment is fixed on a cannonball, the ground equipment is fixed on the ground, the ground equipment and the missile-borne equipment are both connected with a missile-borne computer, control information is sent out by the missile-borne computer and is transmitted to the ground equipment, and the ground equipment transmits the control information to the missile-borne equipment, so that the control of the cannonball is realized, and the information of the cannonball is transmitted to the missile-borne computer by the ground equipment.
(2) According to the wireless data binding device, the missile-borne equipment is provided with the wireless charging receiving module, the ground equipment is provided with the wireless charging transmitting module, the wireless charging transmitting module is connected with the ground measurement and transmission control system through a cable, the wireless charging receiving module is connected with the missile-borne computer through a cable, and the missile-borne computer is used for supplying power to the missile-borne equipment and the ground equipment; be equipped with voltage stabilizing module between missile-borne computer and the wireless receiving module that charges, provide steady voltage for equipment on the bullet through voltage stabilizing module.
Drawings
FIG. 1 is a schematic diagram of a wireless data binding device coupled to an on-board computer in accordance with an embodiment of the present invention;
FIG. 2 is a schematic connection diagram of a ground device and a ground measurement and control system according to an embodiment of the present invention;
fig. 3 is a schematic structural diagram of the pop-up device in the embodiment of the present invention.
In all the figures, the same reference numerals denote the same features, in particular: 1-ground equipment, 2-ground measurement and control system, 3-missile-borne computer, 4-missile-borne equipment, 101-first antenna, 102-first wireless transmission module, 103-first data processing module and 104-wireless charging and transmitting module; 401-a second antenna, 402-a second wireless transmission module, 403-a data processing module, 404-a voltage stabilizing module and 405-a wireless charging receiving module.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention. In addition, the technical features involved in the embodiments of the present invention described below may be combined with each other as long as they do not conflict with each other.
FIG. 1 is a schematic diagram of a wireless data binding device connected to an onboard computer according to an embodiment of the present invention. As shown in fig. 1, the wireless data binding device includes a ground device 1 and an on-board device 4, the ground device 1 and the on-board device 4 are both connected to an on-board computer 3, a CAN bus and a power supply cable are connected between the on-board computer 3 and the ground device 1 and the on-board device, the ground device 1 and the on-board device 4 are powered by the power supply cable, and information transmission between the on-board computer and the ground device 1 and the on-board device 4 is realized through the CAN bus.
The ground equipment 1 and the pop-up equipment 4 realize information transmission through wireless connection, and the ground equipment 1 comprises a first antenna 101, a first wireless transmission module 102 and a first data processing module 103; the first data processing module 103 is connected with the ground measurement and launch control system 2 in a bidirectional mode through a CAN bus, the ground measurement and launch control system 2 launches control information and receives information transmitted by the missile-borne device 4, the ground measurement and launch control system 2 is connected with the missile-borne computer 3, the control information of the ground measurement and launch control system 2 is regulated and controlled through the missile-borne computer 3, and the first data processing module 103 is used for analyzing the information transmitted by the missile-borne device and sending the information to the ground measurement and launch control system 2 through the CAN bus;
the first wireless transmission module 102 is connected with the data processing module 103 in a bidirectional manner, the first wireless transmission module 02 is used for transmitting information of the data processing module 103, the first antenna 101 is fixed on the ground device 1, the first wireless transmission module 102 is connected with the first antenna 101 in a bidirectional manner, and the first antenna 101 is used for sending ground information to the pop-up device 4 through the first wireless transmission module 102 and receiving information sent by the pop-up device 4.
Preferably, the ground device 1 further includes a wireless charging transmitting module 104, a power supply cable is connected between the wireless charging transmitting module 104 and the ground measurement and control system 2, the wireless charging transmitting module 104 is charged through the power supply cable, and the wireless charging transmitting module 104 serves as a power supply of the ground device to ensure normal operation of the ground device.
The pop-up device 4 comprises a second antenna 401, a second wireless transmission module 402, a second data processing module 403, a voltage stabilizing module 404 and a wireless charging receiving module 405, wherein the second antenna 401 is used for receiving information sent by the ground device 1 and sending the information of the pop-up device 4 to the ground device 1; one end of the second wireless transmission module 402 is bidirectionally connected with the second antenna 401, the other end of the second wireless transmission module is bidirectionally connected with the second data processing module 403, the second data processing module 403 is connected with the missile-borne computer 3, and the second data processing module 403 is used for completing analysis of information sent by the ground equipment and received by the second wireless transmission module 402, sending the information to the missile-borne computer through a CAN port, debugging the received CAN information sent by the missile-borne computer, and sending the information to the wireless transmission module.
The pop-up device 4 further comprises a wireless charging receiving module 405 and a voltage stabilizing module 404, the voltage stabilizing module 404 is connected with the pop-up computer 3 through a power supply cable, the voltage stabilizing module 404 is connected with the wireless charging receiving module 405 in a bidirectional manner, the voltage stabilizing module 405 is used for stabilizing the voltage output by the wireless charging receiving module at a fixed value, and preferably, the voltage stabilizing module 405 stabilizes the voltage at 28V, so as to provide a stable power supply voltage for the pop-up device 4.
During operation, the shell is in ground test, through taking off to insert the line power supply, after the shell gets into the barrel, takes off to insert and pulls out, and the wireless data binding device replaces to take off to insert the function, and when wireless data binding system ground equipment pasted the guidance shell wireless data binding system equipment of going up promptly, through the wireless power supply of the wireless module realization shell of charging, the unit power supply normal work after the shell goes up. Meanwhile, the wireless transmission module and the antenna are used for realizing the communication between the ground test and launch control system and the missile-borne computer, the test of the whole missile is completed, the thermal battery of the data binding machine is activated before launching, and the launch process can be carried out after the thermal battery of the product is activated.
The invention utilizes the wireless data binding device to realize wireless power supply, whole bullet test and thermal battery activation before the bullet is loaded into the barrel, thereby avoiding the thermal battery activation before the bullet is launched and reducing the risk before launching. The transmitting strategy can adapt to the requirements of a simple transmitting field on convenient and fast transmission and meet the requirements of actual combat and chemical combat.
It will be understood by those skilled in the art that the foregoing is only a preferred embodiment of the present invention, and is not intended to limit the invention, and that any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (7)
1. A wireless data binding device comprises an missile-borne computer (3), and is characterized by also comprising ground equipment (1), missile-borne equipment (4) and a ground measurement and launch control system (2);
the ground equipment (1) is fixed on the ground, and the pop-up equipment (4) is fixed on the cannonball and is in wireless connection with the ground equipment (1) to realize information transmission;
the ground equipment (1) is connected with the ground measurement and launch control system (2) and is used for receiving a control signal of the ground measurement and launch control system (2) and transmitting information sent by the sprung equipment (4) to the ground measurement and launch control system (2); the missile-borne device (4) is connected with the missile-borne computer (3) and used for transmitting the information sent by the ground device (1) to the missile-borne computer and supplying power to the missile-borne device and the ground device.
2. The wireless data binding device according to claim 1, wherein the ground equipment (1) comprises a first antenna (101), a first wireless transmission module (102) and a first data processing module (103), the first data processing module (103) is bidirectionally connected with the ground measurement and control system (2), one end of the first wireless transmission module (102) is bidirectionally connected with the first data processing module (103), and the other end is bidirectionally connected with the first antenna (101).
3. The wireless data binding device according to claim 2, wherein the ground device (1) comprises a wireless charging transmitting module (104), and the wireless charging transmitting module (104) is connected with the ground measuring and transmitting system (2) through a cable.
4. A wireless data binding apparatus according to claim 1, wherein the pop-up device (4) comprises a second antenna (401), a second wireless transmission module (402) and a second data processing module (403), the second data processing module (403) is bidirectionally connected with the pop-up computer (3), one end of the second wireless transmission module (402) is connected with the second data processing module (403) and the other end is connected with the second antenna (401).
5. The wireless data binding device according to claim 4, characterized in that the on-board device (4) is further provided with a wireless charging receiving module (405) which is connected with the on-board computer (3) through a cable.
6. The wireless data binding device according to claim 5, characterized in that a voltage stabilizing module (404) is arranged between the wireless charging receiving module (405) and the missile-borne computer (3).
7. A wireless data binding device according to claim 1, characterized in that a bidirectional CAN bus is connected between the ground device (1) and the pop-up device (4) and the pop-up computer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010060633.7A CN111260903A (en) | 2020-01-19 | 2020-01-19 | Wireless data binding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010060633.7A CN111260903A (en) | 2020-01-19 | 2020-01-19 | Wireless data binding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111260903A true CN111260903A (en) | 2020-06-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010060633.7A Pending CN111260903A (en) | 2020-01-19 | 2020-01-19 | Wireless data binding device |
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| Country | Link |
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| CN (1) | CN111260903A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113541740A (en) * | 2021-07-19 | 2021-10-22 | 西安电子科技大学 | Secondary transfer storage type micro-power-consumption wireless data binding device and method |
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| JP2012007804A (en) * | 2010-06-24 | 2012-01-12 | Yokogawa Denshikiki Co Ltd | Projection type flying body |
| KR101624325B1 (en) * | 2015-09-04 | 2016-05-25 | 주식회사 위스텍 | flight vehicles lunching system using wireless umbilical system and wireless intersection connection technology for flight vehicles and operating method thereof |
| CN207675040U (en) * | 2017-12-29 | 2018-07-31 | 四川保元防务技术有限公司 | A kind of wireless setter |
| CN209116866U (en) * | 2018-10-26 | 2019-07-16 | 北京星际荣耀空间科技有限公司 | A kind of remote wireless portable data set of data binding system |
| CN110435937A (en) * | 2019-08-15 | 2019-11-12 | 重庆零壹空间科技集团有限公司 | A kind of wireless charging system based on for arrow load main battery |
-
2020
- 2020-01-19 CN CN202010060633.7A patent/CN111260903A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012007804A (en) * | 2010-06-24 | 2012-01-12 | Yokogawa Denshikiki Co Ltd | Projection type flying body |
| KR101624325B1 (en) * | 2015-09-04 | 2016-05-25 | 주식회사 위스텍 | flight vehicles lunching system using wireless umbilical system and wireless intersection connection technology for flight vehicles and operating method thereof |
| CN207675040U (en) * | 2017-12-29 | 2018-07-31 | 四川保元防务技术有限公司 | A kind of wireless setter |
| CN209116866U (en) * | 2018-10-26 | 2019-07-16 | 北京星际荣耀空间科技有限公司 | A kind of remote wireless portable data set of data binding system |
| CN110435937A (en) * | 2019-08-15 | 2019-11-12 | 重庆零壹空间科技集团有限公司 | A kind of wireless charging system based on for arrow load main battery |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113541740A (en) * | 2021-07-19 | 2021-10-22 | 西安电子科技大学 | Secondary transfer storage type micro-power-consumption wireless data binding device and method |
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Application publication date: 20200609 |