CN210983820U - Multi-screen interactive demonstration device for satellite design and launching - Google Patents
Multi-screen interactive demonstration device for satellite design and launching Download PDFInfo
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- CN210983820U CN210983820U CN201920982637.3U CN201920982637U CN210983820U CN 210983820 U CN210983820 U CN 210983820U CN 201920982637 U CN201920982637 U CN 201920982637U CN 210983820 U CN210983820 U CN 210983820U
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Abstract
The utility model discloses a multi-screen interaction demonstration device for satellite design and launching, which comprises a plurality of operation tablet computers, computers and liquid crystal display screens; the tablet personal computer is used for inputting user operation information and is connected with the computer through the Internet; the computer carries a satellite operation demonstration program and is connected with the liquid crystal display screen through the HDMI interface. The method comprises the steps of carrying out satellite design program in a tablet personal computer, wherein the design program comprises six steps of design task selection, satellite platform selection, load configuration selection, operation orbit selection, satellite naming and satellite launching. The problem of current satellite design show instrument content boring, can not play the teaching purpose is solved.
Description
Technical Field
The utility model relates to a human-computer interaction design device, concretely relates to interactive presentation device of shielding more of satellite design and transmission.
Background
The knowledge point of the satellite platform is profound and complicated, and the commonly used display modes are physical model display and multimedia display. In the physical model display, the structural composition and the functional application of the satellite platform are displayed by matching the physical model display of the satellite with the description of the image-text plate. In the multimedia display, the knowledge of the satellite structure composition, the operation mode and the like is dynamically demonstrated in the forms of movie and television data, simulated animation and the like.
The physical model display mode is lack of vividness and is difficult for audiences to understand the process of satellite design. Multimedia display methods lack interest, and although the content is rich, the lecture type of lecture is boring.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a many screen interaction presentation device of satellite design and transmission for solve the problem that current satellite design show instrument content is boring, can not play the teaching purpose.
In order to solve the technical problem, the utility model adopts the following technical scheme:
a multi-screen interactive demonstration device for satellite design and launching comprises a plurality of operation tablet computers, computers and liquid crystal display screens;
the tablet personal computer is used for inputting user operation information and is connected with the computer through the Internet;
the computer carries a satellite operation demonstration program and is connected with the liquid crystal display screen through an HDMI interface.
The design program of the satellite carried in the tablet personal computer comprises six steps of design task selection, satellite platform selection, load configuration selection, operation orbit selection, satellite naming and satellite launching.
The utility model discloses above-mentioned technical scheme has following advantage:
in the scheme, the design idea of the satellite common platform is displayed by means of game, multi-user interaction participation is realized by adopting a multi-machine linkage mode, and interactivity and experience are improved. The method can be used for showing the knowledge related to the design of the artificial satellite in a science and technology museum or other science popularization places. The method effectively simplifies the steps of satellite design experience, and comprises 6 steps of design task selection, satellite platform selection, load configuration selection, operation orbit selection, satellite naming and satellite launching, and the standardization, universalization and serialization of the satellite platform are displayed in an assembly game mode. And a multi-machine linkage mode is adopted, so that a plurality of audiences can participate in interaction at the same time, and the independence and real-time performance of the operation of each audience are ensured.
Drawings
FIG. 1 is a schematic structural diagram of an embodiment of a multi-screen interaction demonstration apparatus for satellite design and launching according to the present invention;
FIG. 2 is a system flowchart of an embodiment of a multi-screen interactive demonstration apparatus for satellite design and launch according to the present invention;
Detailed Description
The following description is provided for illustrative purposes, and other advantages and features of the present invention will become apparent to those skilled in the art from the following detailed description.
It should be understood that the structure, ratio, size and the like shown in the drawings attached to the present specification are only used for matching with the content disclosed in the specification, so as to be known and read by those skilled in the art, and are not used for limiting the limit conditions that the present invention can be implemented, so that the present invention has no technical essential meaning, and any structure modification, ratio relationship change or size adjustment should still fall within the scope that the technical content disclosed in the present invention can cover without affecting the function that the present invention can produce and the purpose that the present invention can achieve. Meanwhile, the terms such as "upper", "lower", "left", "right", "middle", and the like used in the present specification are for the sake of clarity only, and are not intended to limit the scope of the present invention, and changes or adjustments of the relative relationship thereof are also considered to be the scope of the present invention without substantial changes in the technical content.
Example 1
A multi-screen interactive demonstration device for satellite design and launching comprises a plurality of operation tablet computers, computers and liquid crystal display screens;
the tablet personal computer is used for inputting user operation information and is connected with the computer through the Internet;
the computer carries a satellite operation demonstration program and is connected with the liquid crystal display screen through an HDMI interface.
The design program of the satellite carried in the tablet personal computer comprises six steps of design task selection, satellite platform selection, load configuration selection, operation orbit selection, satellite naming and satellite launching.
Referring to fig. 1, a tablet computer is placed in an operator's station on a display stand, and a computer and a liquid crystal display are placed in a display area on the display stand.
Referring to fig. 2, when the system is used, a plurality of users respectively perform six steps of design task selection, satellite platform selection, load configuration selection, operation orbit selection, satellite naming and satellite launching at an operation position, after the operation is completed, the tablet personal computer sends the completed program to the computer, and the computer displays the operation condition of the design result through the liquid crystal display screen.
The utility model discloses a recreation's means shows the design philosophy of the public platform of satellite, adopts the mode of multimachine linkage to realize many people interactive participation, improves interactive and experience nature. The method can be used for showing the knowledge related to the design of the artificial satellite in a science and technology museum or other science popularization places. The method effectively simplifies the steps of satellite design experience, and comprises 6 steps of design task selection, satellite platform selection, load configuration selection, operation orbit selection, satellite naming and satellite launching, and the standardization, universalization and serialization of the satellite platform are displayed in an assembly game mode. And a multi-machine linkage mode is adopted, so that a plurality of audiences can participate in interaction at the same time, and the independence and real-time performance of the operation of each audience are ensured.
Although the invention has been described in detail with respect to the general description and the specific embodiments, it will be apparent to those skilled in the art that modifications and improvements can be made based on the invention. Therefore, such modifications and improvements are intended to be within the scope of the invention as claimed.
Claims (1)
1. A multi-screen interactive demonstration device for satellite design and launching is characterized by comprising a plurality of operation tablet computers, computers and liquid crystal display screens;
the tablet personal computer is used for inputting user operation information and is connected with the computer through the Internet;
the computer is connected with the liquid crystal display screen through an HDMI interface.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201920982637.3U CN210983820U (en) | 2019-06-27 | 2019-06-27 | Multi-screen interactive demonstration device for satellite design and launching |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201920982637.3U CN210983820U (en) | 2019-06-27 | 2019-06-27 | Multi-screen interactive demonstration device for satellite design and launching |
Publications (1)
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CN210983820U true CN210983820U (en) | 2020-07-10 |
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CN201920982637.3U Active CN210983820U (en) | 2019-06-27 | 2019-06-27 | Multi-screen interactive demonstration device for satellite design and launching |
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CN (1) | CN210983820U (en) |
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2019
- 2019-06-27 CN CN201920982637.3U patent/CN210983820U/en active Active
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