Aerospace mission immersive simulation device
By introducing interactive control panels, vibration feedback, and MR technology into the aerospace simulation device, the problems of lack of interactivity and realism in existing devices have been solved. It provides realistic technological applications and immersive application of technology in aerospace missions, realizing the application of technology in aerospace missions and achieving an immersive simulation experience of technology in aerospace missions.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- BEIJING KANXING AEROSPACE TECH CO LTD
- Filing Date
- 2025-05-12
- Publication Date
- 2026-04-14
AI Technical Summary
Existing space simulation devices lack intuitive, vivid, and interactive simulation experiences, cannot accurately simulate spacecraft attitude changes, and cannot allow users to participate in interactive control, thus reducing the educational value and immersive experience of space simulation.
An immersive simulation device for aerospace missions was designed, comprising a simulated spacecraft cabin body, a spacecraft seat, a control panel, an LCD screen, and a vibration motor. The seat is set at a 45-degree angle and is equipped with an interactive control panel and vibration feedback, providing an immersive experience in combination with MR technology.
It achieves a realistic interactive experience and vibration sensation, enhancing the immersive experience of space missions and improving the effectiveness of science education and cultural tourism experiences.
Smart Images
Figure CN224123034U_ABST
Abstract
Description
Technical Field
[0001] This utility model belongs to the technical field of aerospace simulation devices, specifically relating to an immersive simulation device for aerospace missions. Background Technology
[0002] In today's era of rapid technological advancement and deep integration of science education and cultural tourism experiences, the aerospace field has become an important vehicle for attracting the public, especially students. However, currently, whether in science education programs for students or cultural tourism projects for tourists, simulated experiences of aerospace missions are relatively scarce.
[0003] Currently, most existing aerospace simulation devices remain at the level of mechanical and physical simulation, lacking intuitive, vivid, and interactive simulation experience. Students or tourists can only rely on their imagination to understand the complex aerospace launch process, the weightlessness and vibration environment in a space mission, and the operational details of astronauts inside the cabin. This abstract experience makes it difficult to achieve the original design intention of aerospace simulation devices.
[0004] Furthermore, existing aerospace simulation devices suffer from numerous design flaws. First, the seats in these devices lack proper angle planning, failing to accurately simulate the various attitude changes of a spacecraft during flight. This makes it difficult for participants to experience the realism of a space mission, and there is no corresponding vibration sensation. More importantly, these devices lack interactive control panels. Participants can only passively watch pre-set animations or scenes. Students or tourists cannot truly participate in the simulated aerospace mission, nor can they access intuitive visual displays. This undoubtedly greatly reduces the educational value and immersive experience of aerospace simulations.
[0005] Therefore, there is an urgent need to provide an immersive simulation device for aerospace missions that offers interactive experiences and realistic tactile simulation, enabling an immersive experience. Utility Model Content
[0006] The purpose of this invention is to provide an immersive simulation device for aerospace missions to solve the aforementioned problems in the prior art.
[0007] To achieve the above objectives, the present invention adopts the following technical solution:
[0008] This utility model provides an immersive simulation device for aerospace missions, including: a simulated spacecraft cabin body and a simulated spacecraft cabin shell;
[0009] The simulated spacecraft outer shell is disposed outside the simulated spacecraft main body and completely covers the simulated spacecraft main body. A simulated spacecraft seat is placed inside the simulated spacecraft main body. The simulated spacecraft seat is fixedly connected to the inner bottom surface of the simulated spacecraft main body. A simulated spacecraft control panel and an LCD screen are disposed inside the simulated spacecraft main body. The simulated spacecraft control panel and the LCD screen are both disposed corresponding to the simulated spacecraft seat, and the back of the simulated spacecraft control panel and the LCD screen are both connected to the simulated spacecraft main body.
[0010] A vibration motor is installed under the simulated spacecraft seat, and the simulated spacecraft seat is set at a 45-degree angle to the horizontal direction.
[0011] In one possible design, the simulated spacecraft seat includes a seat body, seat armrests, and seat pedals;
[0012] The seat body has an armrest on each side, a seat pedal is fixedly connected to the lower end of the seat body, and a switch-type cross rocker and an armrest grip are provided on each of the armrests on both sides of the seat body.
[0013] At least two simulated spacecraft seats are provided, and each simulated spacecraft seat is arranged side by side.
[0014] In one possible design, a simulated spacecraft control panel is provided between each of the simulated spacecraft seats, between any two adjacent simulated spacecraft seats.
[0015] Each of the simulated aerospace control consoles is equipped with a three-axis joystick and a single-axis push rod.
[0016] In one possible design, the back of the simulated aerospace control panel is connected to the main body of the simulated aerospace cabin via an electrically telescopic connecting rod, and the back of the LCD screen is connected to the main body of the simulated aerospace cabin via a support connecting rod.
[0017] The back of the simulated aerospace control panel is fixedly connected to one end of the electric telescopic connecting rod, the main body of the simulated aerospace cabin is fixedly connected to the other end of the electric telescopic connecting rod, the back of the LCD screen is fixedly connected to one end of the support connecting rod, and the main body of the simulated aerospace cabin is fixedly connected to the other end of the support connecting rod.
[0018] In one possible design, the front of the simulated aerospace control panel is equipped with a touch screen and physical operation buttons;
[0019] The simulated spaceflight control panel is positioned directly opposite the simulated spaceflight seat, the LCD screen is located above and to the side of the simulated spaceflight seat, and the physical operation buttons include a simulation start button.
[0020] In one possible design, both the LCD screen and the vibration motor are electrically connected to the simulated aerospace control panel;
[0021] The switch signal output of the simulated start button is electrically connected to the switch signal input terminals of the LCD screen and the touch screen, and the control signal output terminal of the simulated aerospace control panel is electrically connected to the controlled terminal of the vibration motor.
[0022] In one possible design, the simulated spacecraft cabin shell includes a shell body, a simulated antenna, a simulated solar panel, simulated spacecraft cabin support legs, a simulated hatch, and simulated spacecraft cabin steps;
[0023] The simulated antenna is located on the upper side of the main body of the outer shell, the simulated solar panel is located directly above the main body of the outer shell, the simulated spacecraft support legs are located on the lower side of the main body of the outer shell, the simulated hatch is located on the side of the main body of the outer shell and is movably connected to the main body of the outer shell, and the simulated spacecraft steps are provided below the simulated hatch.
[0024] In one possible design, the simulated aerospace control panel also includes an MR recognition area.
[0025] Beneficial Effects: This utility model provides an immersive simulation device for aerospace missions, including: a simulated spacecraft cabin body and a simulated spacecraft cabin shell; wherein, the simulated spacecraft cabin shell is disposed outside the simulated spacecraft cabin body and completely covers the simulated spacecraft cabin body, a simulated spacecraft seat is placed inside the simulated spacecraft cabin body, the simulated spacecraft seat is fixedly connected to the inner bottom surface of the simulated spacecraft cabin body, a simulated spacecraft control panel and an LCD screen are disposed inside the simulated spacecraft cabin body, the simulated spacecraft control panel and the LCD screen are both correspondingly disposed to the simulated spacecraft seat, and the back of the simulated spacecraft control panel and the LCD screen are both connected to the simulated spacecraft cabin body; a vibration motor is installed under the simulated spacecraft seat, and the simulated spacecraft seat is set at a 45-degree angle to the horizontal direction. This invention provides users with a realistic interactive experience through a simulated aerospace control panel set inside the main body of a simulated spacecraft cabin. It also provides real-time interactive feedback to users through an LCD screen, and a vibration motor is installed under the simulated spacecraft seat to provide users with a vibration experience during the spacecraft simulation. In addition, the simulated spacecraft seat is set at a 45-degree angle to the horizontal direction, which is more in line with the real spacecraft mission experience. This creates an immersive spacecraft mission simulation device with interactive experience and realistic body sensation simulation, which can provide an immersive experience. Attached Figure Description
[0026] Figure 1 A schematic diagram of the main body of the simulated spacecraft cabin of the immersive space mission simulation device provided in this embodiment of the utility model;
[0027] Figure 2 A schematic diagram of the structure of the simulated spacecraft cabin shell of the immersive space mission simulation device provided in this embodiment of the utility model;
[0028] Figure 3 A schematic diagram of the structure of the simulated space seat of the immersive simulation device for space missions provided in this embodiment of the utility model.
[0029] The components include: 1. Simulated spacecraft cabin main body; 2. Simulated spacecraft cabin shell; 3. Simulated spacecraft seat; 4. Simulated spacecraft control panel; 5. LCD screen; 6. Vibration motor; 7. Seat body; 8. Seat armrest; 9. Seat pedal; 10. Shell body; 11. Simulated antenna; 12. Simulated solar panel; 13. Simulated spacecraft cabin support legs; 14. Simulated hatch; and 15. Simulated spacecraft cabin steps. Detailed Implementation
[0030] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the present utility model will be briefly introduced below in conjunction with the accompanying drawings and descriptions of the embodiments or the prior art. Obviously, the following description of the structure of the accompanying drawings is only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort. It should be noted that the description of these embodiments is used to help understand this utility model, but does not constitute a limitation on this utility model.
[0031] It should be understood that although the terms first, second, etc., may be used herein to describe various units, these units should not be limited by these terms. These terms are only used to distinguish one unit from another. For example, the first unit may be referred to as the second unit, and similarly, the second unit may be referred to as the first unit, without departing from the scope of the exemplary embodiments of this utility model.
[0032] It should be understood that the term "and / or" that may appear in this document is merely a description of the relationship between related objects, indicating that three relationships can exist. For example, A and / or B can mean: A exists alone, B exists alone, and A and B exist simultaneously. The term " / and" that may appear in this document describes another relationship between related objects, indicating that two relationships can exist. For example, A / and B can mean: A exists alone, and A and B exist alone. In addition, the character " / " that may appear in this document generally indicates that the related objects before and after it are in an "or" relationship.
[0033] Example 1:
[0034] like Figure 1 As shown, this embodiment provides an immersive simulation device for aerospace missions, including: a simulated spacecraft cabin body 1 and a simulated spacecraft cabin shell 2;
[0035] The simulated spacecraft outer shell 2 is disposed outside the simulated spacecraft body 1 and completely covers the simulated spacecraft body 1. A simulated spacecraft seat 3 is placed inside the simulated spacecraft body 1. The simulated spacecraft seat 3 is fixedly connected to the inner bottom surface of the simulated spacecraft body 1. A simulated spacecraft control panel 4 and an LCD screen 5 are disposed inside the simulated spacecraft body 1. The simulated spacecraft control panel 4 and the LCD screen 5 are both disposed corresponding to the simulated spacecraft seat 3, and the back of the simulated spacecraft control panel 4 and the LCD screen 5 are both connected to the simulated spacecraft body 1.
[0036] A vibration motor 6 is installed below the simulated spacecraft seat 3, and the simulated spacecraft seat 3 is set at a 45-degree angle to the horizontal direction.
[0037] It should be noted that the immersive space mission simulation device provided in this embodiment is specifically designed for science education and cultural tourism experiences, providing users with a better immersive space experience. This immersive space mission simulation device, through a simulated spacecraft control panel 4 located inside the simulated spacecraft cabin 1, provides users with a realistic interactive experience. It also provides real-time interactive feedback through an LCD screen 5. Furthermore, a vibration motor 6 is installed under the simulated spacecraft seat 3, providing a vibration sensation during the space mission simulation. In addition, the simulated spacecraft seat 3 is set at a 45-degree angle to the horizontal, further simulating a real space mission experience. This creates an immersive space mission simulation device with interactive features and realistic tactile simulation, offering users a superior immersive experience.
[0038] Example 2:
[0039] like Figures 2-3 As shown, this embodiment provides an immersive simulation device for aerospace missions. In one possible implementation, the simulated aerospace seat 3 includes a seat body 7, a seat armrest 8, and a seat pedal 9.
[0040] The seat body 7 has an armrest 8 on each side, and the seat pedal 9 is fixedly connected to the lower end of the seat body 7. The armrests 8 on both sides of the seat body 7 are equipped with a switch-type cross rocker and an armrest grip.
[0041] At least two simulated spacecraft seats 3 are provided, and each simulated spacecraft seat 3 is arranged side by side.
[0042] It should be noted that,
[0043] In one possible implementation, a simulated spacecraft control panel is provided between each of the simulated spacecraft seats 3, for every two adjacent simulated spacecraft seats 3.
[0044] Each of the simulated aerospace control consoles is equipped with a three-axis joystick and a single-axis push rod.
[0045] In one possible implementation, the back of the simulated aerospace control panel 4 is connected to the main body 1 of the simulated aerospace cabin via an electrically telescopic connecting rod, and the back of the LCD screen 5 is connected to the main body 1 of the simulated aerospace cabin via a support connecting rod.
[0046] The back of the simulated aerospace control panel 4 is fixedly connected to one end of the electric telescopic connecting rod, the main body of the simulated aerospace cabin 1 is fixedly connected to the other end of the electric telescopic connecting rod, the back of the LCD screen 5 is fixedly connected to one end of the support connecting rod, and the main body of the simulated aerospace cabin 1 is fixedly connected to the other end of the support connecting rod.
[0047] In one possible implementation, the front of the simulated aerospace control panel 4 is provided with a touch screen and physical operation buttons;
[0048] The simulated spacecraft control panel 4 is positioned directly opposite the simulated spacecraft seat 3, the LCD screen 5 is positioned above and to the side of the simulated spacecraft seat 3, and the physical operation buttons include a simulation start button.
[0049] In one possible implementation, both the liquid crystal display screen 5 and the vibration motor 6 are electrically connected to the simulated aerospace control panel 4;
[0050] The switch signal output of the simulated start button is electrically connected to the switch signal input terminals of the LCD screen 5 and the touch screen, and the control signal output terminal of the simulated aerospace control panel 4 is electrically connected to the controlled terminal of the vibration motor 6.
[0051] It should be noted that, in a possible implementation, the switch-type cross joystick, the electric telescopic connecting rod, the three-axis joystick, and the single-axis push rod are also electrically connected to the simulated aerospace control panel 4 and the LCD screen 5. They can be started or stopped by the simulated start button, and the signals they emit can be visualized on the LCD screen 5. The electric telescopic connecting rod can be extended or retracted by the simulated aerospace control panel 4 to adapt to the needs of the user. When the user operates the three-axis joystick and the single-axis push rod, the vibration motor 6 under the simulated aerospace seat 3 will receive the signal and vibrate accordingly, providing the user with a more realistic experience.
[0052] In one possible implementation, the simulated spacecraft cabin shell 2 includes a shell body 10, a simulated antenna 11, a simulated solar panel 12, simulated spacecraft cabin support legs 13, a simulated hatch 14, and simulated spacecraft cabin steps 15;
[0053] The simulated antenna 11 is located on the upper side of the outer shell body 10, the simulated solar panel 12 is located directly above the outer shell body 10, the simulated spacecraft support leg 13 is located on the lower side of the outer shell body 10, the simulated hatch 14 is located on the side of the outer shell body 10 and is movably connected to the outer shell body 10, and the simulated spacecraft step 15 is provided below the simulated hatch 14.
[0054] It should be noted that the simulated antenna 11, simulated solar panel 12, simulated spacecraft support legs 13, simulated hatch 14, and simulated spacecraft steps 15 are set on the outer shell body 10, making the space mission immersive simulation device in this embodiment closer to the real spacecraft device and providing the experiencer with a better immersive experience.
[0055] In one possible implementation, the simulated aerospace control panel 4 is also provided with an MR recognition area.
[0056] It should be noted that the setting of the MR recognition area in this embodiment provides the possibility of MR technology intervention in the immersive simulation device for aerospace missions. In a possible implementation, the user wears MR glasses to recognize the MR recognition area to generate a virtual environment, and the virtual environment replaces part of the surrounding environment observed by the user. Only the simulated spacecraft seat 3, the simulated spacecraft control panel 4, and the LCD screen 5 are used to display real images normally, while other environments are replaced by a virtual environment generated by MR technology. For example, during the rocket launch, the user can observe the rocket flying around them, with space above and the ground tens of kilometers away below.
[0057] Finally, it should be noted that the above are merely preferred embodiments of this utility model and are not intended to limit the scope of protection of this utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the scope of protection of this utility model.
Claims
1. An immersive simulation device for space missions, characterized in that, include: Simulated spacecraft main body (1) and simulated spacecraft outer shell (2); The simulated spacecraft shell (2) is located outside the simulated spacecraft body (1) and completely covers the simulated spacecraft body (1). A simulated spacecraft seat (3) is placed inside the simulated spacecraft body (1). The simulated spacecraft seat (3) is fixedly connected to the bottom surface of the simulated spacecraft body (1). A simulated spacecraft control panel (4) and an LCD screen (5) are provided inside the simulated spacecraft body (1). The simulated spacecraft control panel (4) and the LCD screen (5) are both corresponding to the simulated spacecraft seat (3), and the back of the simulated spacecraft control panel (4) and the LCD screen (5) are both connected to the simulated spacecraft body (1). A vibration motor (6) is installed below the simulated spacecraft seat (3), and the simulated spacecraft seat (3) is set at a 45-degree angle to the horizontal direction.
2. The immersive simulation device for space missions according to claim 1, characterized in that, The simulated spacecraft seat (3) includes a seat body (7), seat armrests (8), and seat pedals (9); Among them, a seat armrest (8) is provided on each side of the seat body (7), the seat pedal (9) is fixedly connected to the lower end of the seat body (7), and a switch-type cross rocker and armrest grip are provided on the seat armrests (8) on both sides of the seat body (7); At least two of the simulated spacecraft seats (3) are provided, and each of the simulated spacecraft seats (3) is arranged side by side.
3. The immersive simulation device for space missions according to claim 2, characterized in that, In each of the simulated space seats (3), a simulated space operation table is provided between two adjacent simulated space seats (3); Each of the simulated aerospace control consoles is equipped with a three-axis joystick and a single-axis push rod.
4. The immersive simulation device for space missions according to claim 1, characterized in that, The back of the simulated aerospace control panel (4) is connected to the main body (1) of the simulated aerospace cabin via an electric telescopic connecting rod, and the back of the LCD screen (5) is connected to the main body (1) of the simulated aerospace cabin via a support connecting rod. The back of the simulated aerospace control panel (4) is fixedly connected to one end of the electric telescopic connecting rod, the main body of the simulated aerospace cabin (1) is fixedly connected to the other end of the electric telescopic connecting rod, the back of the LCD screen (5) is fixedly connected to one end of the support connecting rod, and the main body of the simulated aerospace cabin (1) is fixedly connected to the other end of the support connecting rod.
5. The immersive simulation device for space missions according to claim 1, characterized in that, The front of the simulated aerospace control panel (4) is equipped with a touch screen and physical operation buttons; The simulated spacecraft control panel (4) is positioned directly opposite the simulated spacecraft seat (3), the LCD screen (5) is positioned above and to the side of the simulated spacecraft seat (3), and the physical operation buttons include a simulated start button.
6. The immersive simulation device for space missions according to claim 5, characterized in that, The liquid crystal display screen (5) and the vibration motor (6) are both electrically connected to the simulated aerospace control panel (4); The switch signal output of the simulated start button is electrically connected to the switch signal input terminals of the liquid crystal display screen (5) and the touch screen, and the control signal output terminal of the simulated aerospace control panel (4) is electrically connected to the controlled terminal of the vibration motor (6).
7. The immersive simulation device for space missions according to claim 1, characterized in that, The simulated spacecraft cabin shell (2) includes a shell body (10), a simulated antenna (11), a simulated solar panel (12), simulated spacecraft support legs (13), a simulated hatch (14), and simulated spacecraft steps (15); The simulated antenna (11) is located on the upper side of the outer shell body (10), the simulated solar panel (12) is located directly above the outer shell body (10), the simulated spacecraft support leg (13) is located on the lower side of the outer shell body (10), the simulated hatch (14) is located on the side of the outer shell body (10) and is movably connected to the outer shell body (10), and the simulated spacecraft step (15) is provided below the simulated hatch (14).
8. The immersive simulation device for space missions according to claim 1, characterized in that, The simulated aerospace control panel (4) is also equipped with an MR recognition area.