Spaceflight launch and recovery situation visualization system
By combining data acquisition modules and animation servers with 3D models and topographic maps, the problem of unintuitive information display during space launch and recovery was solved, enabling real-time visualization of spacecraft launch and recovery and improving the readability and comprehensibility of information.
Patent Information
- Application Number
- CN202423185557.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-24
- Publication Date
- 2025-12-16
- Estimated Expiration
- 2034-12-24
AI Technical Summary
Existing monitoring technologies for space launch and recovery processes mainly rely on numerical data and graphical displays, lacking intuitive spatial representation methods, resulting in poor readability and comprehensibility of information.
It employs a data acquisition module, a data server cluster, an animation server, and a large-screen display device. Data is collected through radar, optical tracking, and radio tracking equipment, and combined with 3D models and topographic maps to achieve real-time visualization of spacecraft launch and recovery.
It provides an intuitive 3D animation of the spacecraft launch and recovery process, improving the readability and comprehensibility of information and facilitating rapid decision-making.
Smart Images
Figure CN223681080U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to visual system technical field, concretely is space launch and recovery situation visual system. BACKGROUND
[0002] The visualization of space launch and recovery situation is an important technology in the field of space, which can more intuitively understand the whole process of space activities, including launch, operation, recovery and other links.
[0003] The existing space launch monitoring technology mainly relies on numerical data and chart display, and the readability and intuitiveness of information are poor, which is not conducive to the comprehensive understanding and rapid decision of the space launch and recovery process. Although the traditional radar, optical tracking, radio tracking and other equipment can accurately measure the state information of the spacecraft, these data can only be presented in the form of table or chart, and lack intuitive spatial display mode, therefore, the space launch and recovery situation visualization system is proposed. UTILITY MODEL CONTENT
[0004] The utility model aims at solving one of the technical problems in the prior art.
[0005] Therefore, one purpose of the utility model is to propose a space launch and recovery situation visualization system, which can realize the visualization of spacecraft launch and recovery, and can realize intuitive spatial display mode, which is convenient for understanding.
[0006] In order to achieve the above purpose, the utility model provides the following technical scheme: the space launch and recovery situation visualization system comprises a data acquisition module, a data server cluster, an animation server, a large screen display device and a switch, the data acquisition module is in communication connection with the data server cluster, the data server cluster is in communication connection with the switch, the switch is in communication connection with the animation server, and the data server cluster is in communication connection with the large screen display device.
[0007] Preferably, the data acquisition module comprises radar equipment, optical tracking equipment and radio tracking equipment.
[0008] Preferably, the animation server comprises modeling computer equipment, rendering computer equipment and engine computer equipment.
[0009] Preferably, the animation server is electrically connected with an input device.
[0010] Compared with the prior art, the utility model has the beneficial effects that:
[0011] The utility model discloses can through the data of spacecraft's collection, setting up animation server beforehand making three -dimensional model of spacecraft, and make the topographic map of recovery position, when spacecraft launch and recovery, all through the data of obtaining from data server cluster real -time three -dimensional animation making to can realize spacecraft launch and recovery's visualization, can realize the space display mode of intuitive, convenient for understanding. BRIEF DESCRIPTION OF DRAWINGS
[0012] Figure 1 It is the structure schematic diagram of the space launch and recovery situation visualization system of the utility model.
[0013] In the drawing: 1, data acquisition module, 2, data server cluster, 3, animation server, 4, large screen display device, 5, switch, 6, input device, 11, radar equipment, 12, optical tracking equipment, 13, radio tracking equipment, 31, modeling computer equipment, 32, rendering computer equipment, 33, engine computer equipment. DETAILED DESCRIPTION
[0014] The technical scheme in the embodiments of the utility model will be described clearly and completely below in conjunction with the drawings in the embodiments of the utility model, and obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by the ordinary skill in the art without creative labor belong to the scope of protection of the utility model.
[0015] Please refer to Figure 1 The embodiment of the utility model provides space launch and recovery situation visualization system, including data acquisition module 1, data server cluster 2, animation server 3, large screen display device 4 and switch 5, data acquisition module 1 is connected with data server cluster 2 communication, data server cluster 2 is connected with switch 5 communication, switch 5 is connected with animation server 3 communication, data server cluster 2 is connected with large screen display device 4 communication.
[0016] Among them, data acquisition module 1 includes radar equipment 11, optical tracking equipment 12 and radio tracking equipment 13.
[0017] Among them, animation server 3 includes modeling computer equipment 31, rendering computer equipment 32 and engine computer equipment 33.
[0018] In use, the radar device 11 of the data acquisition module 1 measures the position and speed of the spacecraft by sending electromagnetic waves and receiving reflected waves, the optical tracking device 12 is used for visually tracking the spacecraft, the radio tracking device 13 tracks the position of the spacecraft by receiving the radio signals emitted by the spacecraft, and then sends data to the data server cluster 2, and a satellite communication device can be additionally added to receive the position data of the spacecraft through a communication satellite.
[0019] The animation server 3 is in communication connection with the data server cluster 2, the animation server 3 pre-prepares a three-dimensional model of the spacecraft and prepares a topographic map of the recovery position, and real-time three-dimensional animation is made through the data obtained from the data server cluster 2 when the spacecraft is launched and recovered, so that the visualization of the spacecraft when launched and recovered can be realized.
[0020] Among them, in order to input data and instructions, the animation server 3 is electrically connected with an input device 6.
[0021] According to the above technical scheme, the working steps of the present scheme are summarized and combed: in use, the radar device 11 of the data acquisition module 1 measures the position and speed of the spacecraft by sending electromagnetic waves and receiving reflected waves, the optical tracking device 12 is used for visually tracking the spacecraft, the radio tracking device 13 tracks the position of the spacecraft by receiving the radio signals emitted by the spacecraft, and then sends data to the data server cluster 2, and a satellite communication device can be additionally added to receive the position data of the spacecraft through a communication satellite, the animation server 3 is in communication connection with the data server cluster 2, the animation server 3 pre-prepares a three-dimensional model of the spacecraft and prepares a topographic map of the recovery position, and real-time three-dimensional animation is made through the data obtained from the data server cluster 2 when the spacecraft is launched and recovered, so that the visualization of the spacecraft when launched and recovered can be realized.
[0022] The parts not involved in the present application are the same as or can be realized by the prior art. Although the embodiments of the present application have been shown and described, it can be understood by those skilled in the art that various changes, modifications, replacements and variations can be made to these embodiments without departing from the principles and spirits of the present application, and the scope of the present application is defined by the appended claims and their equivalents.
Claims
1. A space launch and recovery situation visualization system, characterized in that, include: The system includes a data acquisition module (1), a data server cluster (2), an animation server (3), a large screen display device (4), and a switch (5). The data acquisition module (1) is communicatively connected to the data server cluster (2), the data server cluster (2) is communicatively connected to the switch (5), the switch (5) is communicatively connected to the animation server (3), and the data server cluster (2) is communicatively connected to the large screen display device (4).
2. The space launch and recovery situation visualization system according to claim 1, characterized in that: The data acquisition module (1) includes a radar device (11), an optical tracking device (12), and a radio tracking device (13).
3. The space launch and recovery situation visualization system according to claim 1, characterized in that: The animation server (3) includes a modeling computer device (31), a rendering computer device (32), and an engine computer device (33).
4. The space launch and recovery situation visualization system according to claim 1, characterized in that: The animation server (3) is electrically connected to an input device (6).