CN212302517U - Carrier rocket data acquisition system - Google Patents
Carrier rocket data acquisition system Download PDFInfo
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- CN212302517U CN212302517U CN202022778292.5U CN202022778292U CN212302517U CN 212302517 U CN212302517 U CN 212302517U CN 202022778292 U CN202022778292 U CN 202022778292U CN 212302517 U CN212302517 U CN 212302517U
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- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
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Abstract
The utility model relates to the technical field of carrier rockets, and provides a carrier rocket data acquisition system, which comprises a carrier rocket, a data acquisition terminal and an information server; the carrier rocket is provided with at least one data identification unit, the data identification unit is used for recording data of the carrier rocket, and the data comprises equipment information of each equipment in the carrier rocket and data information corresponding to the equipment; the data acquisition terminal is provided with a central processing unit, an identification recognition module, a data storage module and a display module, wherein the identification recognition module, the data storage module and the display module are all connected with the central processing unit, and the identification recognition module is used for recognizing a data identification unit of the carrier rocket; the information server is connected with the data acquisition terminal and is used for acquiring and storing the data of the carrier rocket acquired by the data acquisition terminal.
Description
Technical Field
The utility model relates to a carrier rocket technical field, more specifically say so, relate to a carrier rocket data acquisition system.
Background
With the vigorous development of the commercial aerospace field, the civil technology is continuously converted into the aerospace technology, and the development capability of the carrier rocket is continuously improved. The carrier rocket is a complex large-scale system, and the quality control in the development and production processes of the carrier rocket has important significance for the launching success of the rocket. Data acquisition and process recording are key contents of quality work, and the effective data acquisition can realize the rapid tracing of process information.
Because the production and assembly processes of the carrier rocket are complex, and the product scale is larger than that of other industrial products, the traditional paper recording mode cannot meet the requirement of digital acquisition of data information, and the data needs to be acquired in a digital mode, however, the currently adopted computer recording mode is poor in portability, the data acquisition of the carrier rocket is inconvenient, and large-scale application is difficult to obtain.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a carrier rocket data acquisition system to solve the inconvenient technical problem of carrier rocket data acquisition among the prior art.
In order to achieve the above object, the utility model adopts the following technical scheme: the carrier rocket data acquisition system comprises a carrier rocket, a data acquisition terminal and an information server;
the carrier rocket is provided with at least one data identification unit, the data identification unit is used for recording data of the carrier rocket, and the data comprises equipment information of each equipment in the carrier rocket and data information corresponding to the equipment;
the data acquisition terminal is provided with a central processing unit, an identification recognition module, a data storage module and a display module, wherein the identification recognition module, the data storage module and the display module are all connected with the central processing unit, and the identification recognition module is used for recognizing a data identification unit of the carrier rocket;
the information server is connected with the data acquisition terminal and is used for acquiring and storing the data information of the carrier rocket acquired by the data acquisition terminal.
In one embodiment, the data identification unit comprises a two-dimensional code, and the identification module comprises a two-dimensional code identification unit connected with the central processing unit.
In one embodiment, the data identification unit comprises an RFID tag, and the identification module comprises an RFID tag reading unit connected to the central processing unit.
In one embodiment, the data acquisition terminal is further provided with an identity verification module, and the identity verification module is connected with the central processing unit.
In one embodiment, the identity verification module comprises a fingerprint acquisition unit, which is connected with the central processing unit.
In one embodiment, the identity verification module comprises a face recognition unit, and the face recognition unit is connected with the central processing unit.
In one embodiment, the identity verification module comprises a voiceprint recognition unit, which is connected with the central processing unit;
and/or the identity authentication module comprises an iris recognition unit, and the iris recognition unit is connected with the central processing unit.
In one embodiment, the data acquisition terminal is connected with the information server through a data transmission device, the data transmission device includes a network security device and a network switching device, the network security device is connected with the information server, the network switching device is connected with the network security device, and the data acquisition terminal is connected with the network switching device.
In one embodiment, the data acquisition terminal is further provided with a wireless communication module, the wireless communication module is connected with the central processing unit, and the wireless communication module and the network switching equipment perform data interaction in a wireless communication mode.
In one embodiment, the wireless communication module is a WIFI module or a bluetooth module.
The utility model provides a carrier rocket data acquisition system's beneficial effect lies in at least:
(1) the utility model discloses a portable data acquisition terminal is as the executive equipment of record operation, and data acquisition terminal sends the data acquisition to information server and stores and data processing, has realized the miniaturization of recording equipment, and the form for traditional computer data collection is convenient nimble more.
(2) The utility model discloses a set up data identification unit at each equipment of carrier rocket, the data of each equipment need not to carry out data transmission through the mode that lasts wireless transmission, when needs carry out data acquisition, can obtain the data of each equipment through data acquisition terminal identification data identification unit, can not change the electromagnetic environment that carrier rocket located, has effectively ensured its security, has very extensive application prospect.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required for the embodiments or the prior art descriptions will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
Fig. 1 is a schematic structural diagram of a carrier rocket data acquisition system according to an embodiment of the present invention;
fig. 2 is a schematic structural diagram of a data acquisition terminal in a data acquisition system of a launch vehicle provided in an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a carrier rocket data acquisition system according to an embodiment of the present invention;
fig. 4 is a schematic structural diagram ii of a data acquisition terminal in a data acquisition system of a launch vehicle provided in an embodiment of the present invention.
Wherein, in the figures, the respective reference numerals:
10-a launch vehicle;
11-a data identification unit;
20-a data acquisition terminal;
21-a central processing unit;
22-identification recognition module;
23-a data storage module;
24-a display module;
25-an identity verification module;
26-a wireless communication module;
27-a power supply control module;
30-information server.
Detailed Description
In order to make the technical problem, technical solution and advantageous effects to be solved by the present invention more clearly understood, the following description is given in conjunction with the accompanying drawings and embodiments to illustrate the present invention in further detail. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly or indirectly secured to the other element. When an element is referred to as being "connected to" another element, it can be directly or indirectly connected to the other element. The terms "upper", "lower", "left", "right", "front", "rear", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positions based on the orientations or positions shown in the drawings, and are for convenience of description only and not to be construed as limiting the technical solution. The terms "first", "second" and "first" are used merely for descriptive purposes and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features. The meaning of "plurality" is two or more unless specifically limited otherwise.
The carrier rocket is used as a complex large-scale system, the quality control in the development and production process of the carrier rocket has important significance for the launching success of the rocket, the data acquisition and the process record are the key contents of quality work, the effective data acquisition can realize the rapid source tracing of process information, and therefore the data acquisition of the carrier rocket is needed.
The wireless communication technology represented by mobile communication enables real-time information recording and state reminding, but the carrier rocket is different from the traditional industry, partial equipment of the carrier rocket is sensitive to the electromagnetic environment, and the wireless transmission of signals can change the electromagnetic environment of the carrier rocket, so that the safety of the carrier rocket is affected. In addition, because the production and assembly processes of the carrier rocket are complex, and the product scale is larger than that of other industrial products, the traditional paper recording mode cannot meet the requirement of digital acquisition of data information, and needs to adopt a digital mode to acquire data, however, the currently adopted computer recording mode is poor in portability, the data acquisition of the carrier rocket is inconvenient, and large-scale application is difficult to obtain.
The non-contact information acquisition technologies such as RFID (Radio Frequency Identification) and two-dimensional code provide a new method for the data acquisition of products. Based on this, this embodiment provides a carrier rocket data acquisition system, through setting up sign identification module at data acquisition terminal, can discern the data identification unit that sets up on the carrier rocket with portable mode, combine the work content of carrier rocket can carry out the record to the data of carrier rocket, send data to information server through data acquisition terminal, can carry out data analysis on portable data acquisition's basis, help promoting data analysis efficiency by a wide margin.
Referring to fig. 1, the present embodiment provides a data acquisition system for a launch vehicle, which includes a launch vehicle 10, a data acquisition terminal 20, and an information server 30. The carrier rocket 10 is provided with at least one data identification unit 11, and the data identification unit 11 is used for recording data of the carrier rocket 10, where the data includes device information of each device in the carrier rocket 10 and data information corresponding to the device. Referring to fig. 2, the data acquisition terminal 20 is provided with a central processing unit 21, an identification module 22, a data storage module 23 and a display module 24, the identification module 22, the data storage module 23 and the display module 24 are all connected to the central processing unit 21, and the identification module 22 is used for identifying the data identification unit 11 of the launch vehicle 10. The information server 30 is connected to the data acquisition terminal 20, and is configured to acquire and store the data of the launch vehicle 10 acquired by the data acquisition terminal 20.
In this embodiment, the launch vehicle 10 includes a plurality of devices, each of which may be provided with a data identification unit 11, and the data identification unit 11 records device information (such as a device number) of the device and operation data information of the device. The data acquisition terminal 20 may be a mobile terminal of a type such as a smart phone, a tablet computer, or a notebook computer, or may be a customized terminal device or an industrial handheld terminal, which is not limited herein. When the data of each device in the carrier rocket 10 needs to be collected, the data identification unit 11 of each device of the carrier rocket 10 is identified through the data collection terminal 20, the data of the device is obtained, the data is stored in the data storage module 23, and the data is sent to the information server 30. The information server 30 may store the data after receiving the data, may process the data, and the like, and is not limited herein. The display module 24 of the data acquisition terminal 20 may be used only for displaying information, or may perform a touch operation, so as to facilitate a user to select an operation mode of the data acquisition terminal 20, for example, to control the data acquisition terminal 20 to perform data acquisition or to send data to the information server 30. Of course, the data acquisition terminal 20 may also be provided with keys for control, and is not limited herein.
The carrier rocket data acquisition system provided by the embodiment has the beneficial effects that:
(1) in the embodiment, the portable data acquisition terminal 20 is used as an executing device for recording operation, and the data acquisition terminal 20 sends the acquired data to the information server 30 for storage and data processing, so that the recording device is miniaturized, and the form of acquiring data by using the portable data acquisition terminal is more convenient and flexible compared with the traditional computer.
(2) In the embodiment, the data identification unit 11 is arranged on each device of the carrier rocket 10, data transmission of each device is not required to be performed in a continuous wireless transmission mode, when data acquisition is required, the data identification unit 11 is identified by the data acquisition terminal 20, so that the data of each device can be obtained, the electromagnetic environment of the carrier rocket is not changed, the safety of the carrier rocket is effectively guaranteed, and the carrier rocket has a very wide application prospect.
Further, the form of the data identification unit 11 may be set as needed.
In one embodiment, the data identification unit 11 includes a two-dimensional code, and correspondingly, the identification module 22 includes a two-dimensional code identification unit, the two-dimensional code identification unit is connected to the central processing unit 21, and when data of each device in the launch vehicle 10 needs to be acquired, the two-dimensional code is scanned by the two-dimensional code identification unit of the identification module 22, so that the data can be acquired. The two-dimensional code recognition unit may include one camera or a plurality of cameras, which is not limited herein.
In one embodiment, the data identification unit 11 includes an RFID tag, and correspondingly, the identification module 22 includes an RFID tag reading unit, which is connected to the central processing unit 21, and when data of each device in the launch vehicle 10 needs to be acquired, the data can be acquired by identifying the RFID tag through the RFID tag reading unit of the identification module 22.
Of course, in a preferred embodiment, each device may be configured to have the data identification unit 11 including a two-dimensional code or an RFID tag, and the identification module 22 may include a two-dimensional code identification unit and an RFID tag reading unit, so as to be able to identify different types of data identification units 11, and thus, the application scenarios are wider.
Referring to fig. 2, further, in order to ensure the use safety, the data acquisition terminal 20 is further provided with an authentication module 25, and the authentication module 25 is connected to the central processing unit 21. When the user needs to use the data acquisition terminal 20, authentication is required, and only the user who passes the authentication can use the data acquisition terminal 20. The identity verification module 25 may be integrated in the data acquisition terminal 20, or may be an external device connected to the data acquisition terminal 20, and the specific form may be set as required, which is not limited herein.
In one embodiment, the identity verification module 25 comprises a fingerprint acquisition unit, which is connected to the central processing unit. When the user needs to use the data acquisition terminal 20, the user needs to acquire a fingerprint through the fingerprint acquisition unit and perform fingerprint matching verification, and only the user who passes the identity verification can use the data acquisition terminal 20.
In one embodiment, the authentication module 25 comprises a face recognition unit, which is connected to the central processing unit. When the user needs to use the data acquisition terminal 20, the user needs to acquire a facial image through the face recognition unit and perform face image matching verification, and only the user who passes the identity verification can use the data acquisition terminal 20.
In one embodiment, the identity verification module 25 comprises a voiceprint recognition unit, which is connected to the central processing unit. When the user needs to use the data acquisition terminal 20, the voice of the user needs to be acquired through the voiceprint recognition unit and voiceprint matching verification is performed, and only the user who passes the identity verification can use the data acquisition terminal 20.
In one embodiment, the authentication module 25 comprises an iris recognition unit, which is connected to the central processing unit. When the user needs to use the data acquisition terminal 20, the iris information of the user needs to be acquired through the iris identification unit for matching verification, and only the user who passes the identity verification can use the data acquisition terminal 20.
It is understood that the identity verification module 25 may include one or more of the fingerprint collection unit, the face recognition unit, the voiceprint recognition unit and the iris recognition unit, which may be set as required, and is not limited herein.
Further, the data acquisition terminal 20 is connected to the information server 30 through a data transmission device. The data transmission device 40 includes a network security device and a network switching device, the network security device is connected to the information server 30, the network switching device is connected to the network security device, and the data acquisition terminal 20 is connected to the network switching device in a wired or wireless manner.
Referring to fig. 3 and 4, further, the data acquisition terminal 20 is further provided with a wireless communication module 26, the wireless communication module 26 is connected with the central processing unit 21, and the wireless communication module 26 performs data interaction with the network switching device in a wireless communication manner. The wireless communication module can be a WIFI module, which facilitates timely transmission of data to the information server 30. In other embodiments, the wireless communication module 26 may also be a bluetooth module, and the data collection terminal 20 may be located near the network switching device to transmit data to the data collection terminal via bluetooth. It is understood that the data acquisition terminal 20 may also be provided with other modules, such as a power control module 27, and the power control module 27 is connected with the central processing unit 21 for supplying power to the other modules in the data acquisition terminal 20.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.
Claims (10)
1. A carrier rocket data acquisition system is characterized by comprising a carrier rocket, a data acquisition terminal and an information server;
the carrier rocket is provided with at least one data identification unit, the data identification unit is used for recording data of the carrier rocket, and the data comprises equipment information of each equipment in the carrier rocket and data information corresponding to the equipment;
the data acquisition terminal is provided with a central processing unit, an identification recognition module, a data storage module and a display module, wherein the identification recognition module, the data storage module and the display module are all connected with the central processing unit, and the identification recognition module is used for recognizing a data identification unit of the carrier rocket;
the information server is connected with the data acquisition terminal and is used for acquiring and storing the data of the carrier rocket acquired by the data acquisition terminal.
2. A launch vehicle data acquisition system according to claim 1 and wherein said data identification unit comprises a two-dimensional code and said identification module comprises a two-dimensional code identification unit, said two-dimensional code identification unit being coupled to said central processing unit.
3. A launch vehicle data acquisition system according to claim 1, characterised in that said data identification unit comprises an RFID tag, said identification recognition module comprising an RFID tag reading unit, said RFID tag reading unit being connected to said central processing unit.
4. A launch vehicle data collection system according to claim 1, wherein said data collection terminal is further provided with an authentication module, said authentication module being connected to said central processing unit.
5. A launch vehicle data collection system according to claim 4, characterised in that said identity verification module comprises a fingerprint collection unit, said fingerprint collection unit being connected to said central processing unit.
6. A launch vehicle data acquisition system according to claim 4, characterised in that said authentication module comprises a face recognition unit, said face recognition unit being connected to said central processing unit.
7. A launch vehicle data collection system according to claim 4, wherein said authentication module includes a voiceprint recognition unit, said voiceprint recognition unit being connected to said central processing unit;
and/or the identity authentication module comprises an iris recognition unit, and the iris recognition unit is connected with the central processing unit.
8. A launch vehicle data acquisition system according to claim 1, wherein said data acquisition terminal is connected to said information server through a data transfer device, said data transfer device comprising a network security device and a network switching device, said network security device being connected to said information server, said network switching device being connected to said network security device, said data acquisition terminal being connected to said network switching device.
9. A launch vehicle data acquisition system according to claim 8 and wherein said data acquisition terminal is further provided with a wireless communication module, said wireless communication module being connected to said central processing unit, said wireless communication module wirelessly communicating with said network switching device for data interaction.
10. A launch vehicle data acquisition system according to claim 9, characterised in that said wireless communication module is a WIFI module or a bluetooth module.
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| CN202022778292.5U CN212302517U (en) | 2020-11-26 | 2020-11-26 | Carrier rocket data acquisition system |
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| CN202022778292.5U CN212302517U (en) | 2020-11-26 | 2020-11-26 | Carrier rocket data acquisition system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112887544A (en) * | 2021-01-21 | 2021-06-01 | 上海航天测控通信研究所 | Integrated wireless WIFI camera device suitable for carrier rocket |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112887544A (en) * | 2021-01-21 | 2021-06-01 | 上海航天测控通信研究所 | Integrated wireless WIFI camera device suitable for carrier rocket |
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