Simulated system, method, electronic device and storage medium of lunar base

Abstract

The application provides a lunar base simulation system and method, electronic equipment and storage medium, and relates to the technical field of space application. The lunar base simulation system comprises a first experiment subsystem, a second experiment subsystem and a third experiment subsystem. The first experiment subsystem is configured to simulate lunar information within a preset range, wherein the lunar information at least comprises a target device and a lunar environment, and the target device runs in the lunar environment. The second experiment subsystem is configured to perform an environment experiment on the target device, wherein the target device at least comprises a manned device, a robot device and a load device. The third experiment subsystem is configured to simulate a target function required by the target device. The technical scheme of the application can solve the problem that the key technologies of lunar base construction and operation cannot be effectively verified.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of space application, in particular to a lunar base simulation system and method, an electronic device and a storage medium. BACKGROUND

[0002] The lunar environment (such as radiation, lunar dust, micro-meteors, low gravity, etc.) brings great challenges to the long-term residence of astronauts and the normal operation of the lunar base. In order to ensure the safe implementation of manned lunar exploration and lunar base construction tasks, it is necessary to verify the key technologies involved in lunar base construction, operation and astronaut life on Earth in advance. It is urgent to establish a lunar twin base on Earth to simulate the lunar environment and verify the feasibility of key technologies on the ground.

[0003] In theory, the design and construction of the lunar twin base should simulate the environment according to the lunar base site planned in the manned lunar mission. However, due to the limitations of the construction site, construction funds and experimental scientific and technological conditions, it is still not possible to achieve full simulation of a large range of lunar environment, for example, the lunar surface temperature generally varies by about 173℃-140℃ (the polar day-night temperature difference is relatively small), and currently a thermal vacuum tank is often used to simulate the lunar surface temperature on the ground. Its volume is limited and cannot be used for technical verification of key links such as lunar surface landing, lunar surface round trip, and other lunar base construction and operation, resulting in the problem that the key technologies of lunar base construction and operation cannot be effectively verified.

[0004] It should be noted that the information disclosed in the above background section is only used to strengthen the understanding of the background of the present application, and therefore can include information that does not constitute prior art known to those of ordinary skill in the art. SUMMARY

[0005] The purpose of the embodiments of the present application is to provide a lunar base simulation system and method, an electronic device and a storage medium, thereby at least partially overcoming the problem that the key technologies of lunar base construction and operation cannot be effectively verified.

[0006] Other characteristics and advantages of the present application will become apparent from the following detailed description, or will be learned by practice of the present application.

[0007] According to a first aspect of the embodiments of the present application, a simulation system of a lunar base is provided, comprising: a first experimental subsystem, a second experimental subsystem, and a third experimental subsystem, wherein the first experimental subsystem is configured to simulate lunar information within a preset range, wherein the lunar information at least comprises: a target device and a lunar environment, and the target device is configured to operate in the lunar environment; the second experimental subsystem is configured to perform an environmental experiment on the target device, wherein the target device at least comprises: a manned device, a robot device, and a load device; and the third experimental subsystem is configured to simulate a target function required by the target device.

[0008] In some example embodiments of the present application, based on the foregoing scheme, the first experimental subsystem comprises: a landing image navigation module configured to simulate image navigation of a lunar lander landing; a lunar surface inspection module configured to simulate lunar surface features, wherein the lunar surface features at least comprise: lunar surface dust; a man-machine joint driving module configured to verify whether a man-machine joint function of a manned lunar rover and a manned lunar robot is normal; and a lunar robot action module configured to simulate a motion function of a lunar robot, wherein the motion function at least comprises: a preset carrying amount, a preset motion distance, and a preset motion speed.

[0009] In some example embodiments of the present application, based on the foregoing scheme, the man-machine joint driving module comprises: a lunar soil simulation sub-module, a lunar dome simulation sub-module, a lunar crater simulation sub-module, a lunar obstacle simulation sub-module, and a lunar slope simulation sub-module.

[0010] In some example embodiments of the present application, based on the foregoing scheme, the first experimental subsystem further comprises: an in-situ resource utilization processing module configured to verify whether a lunar surface resource processing robot normally performs a preset operation, wherein the preset operation at least comprises: a 3D printing operation; and a first excavation mining module configured to simulate lunar resources, wherein the lunar resources at least comprise one of: water resources, mineral resources, and helium-3 resources.

[0011] In some example embodiments of the present application, based on the foregoing scheme, the first experimental subsystem further comprises: a first lunar robot operation and maintenance module configured to test operation data of a lunar robot and maintain operation data of the lunar robot; a first lunar robot facility construction module configured to construct infrastructure of the lunar base, wherein the infrastructure at least comprises: a base scene of the lunar base; and a first man-machine cooperation module configured to construct a man-machine cooperation digital simulation system and a man-machine cooperation operation system.

[0012] In some example embodiments of the present application, based on the foregoing scheme, the second experimental subsystem comprises: a second excavation mining module configured to simulate target conditions required by mining equipment of a lunar mining robot in a lunar environment, wherein the target conditions at least include: light adaptation function, and preset working duration; a second lunar surface robot operation and maintenance module configured to simulate light angles of lunar surface light within a preset duration; a second lunar surface robot facility construction module configured to verify whether the robot equipment is adapted to the lunar environment; a first digital lunar experiment module configured to display detection data of a lunar base; and a first environment test experiment module configured to test target lunar detection equipment or target lunar detection payload.

[0013] In some example embodiments of the present application, the third experimental subsystem comprises: a third lunar surface robot facility construction module configured to verify whether the lunar surface robot is adapted to the lunar environment in the case that the lunar surface is covered with dust; a second man-machine cooperation module configured to identify preset instructions sent by an astronaut to the lunar surface robot, wherein the preset instructions at least include one of the following: action instruction, and expression instruction; a second digital lunar experiment module configured to visually display an application scenario of a lunar base; a second environment test experiment module configured to simulate a preset temperature environment required by the lunar base through a hot vacuum tank; and a lunar exploration experience module configured to provide an experience function of the application scenario to the astronaut.

[0014] According to a second aspect of the embodiments of the present application, a simulation method of a lunar base is provided, comprising: a first experimental subsystem, a second experimental subsystem, and a third experimental subsystem, wherein the first experimental subsystem is configured to simulate lunar information within a preset range, wherein the lunar information at least includes: target equipment, and a lunar environment, wherein the target equipment runs in the lunar environment; the second experimental subsystem is configured to perform environment experiments on the target equipment, wherein the target equipment at least includes: manned equipment, robot equipment, and payload equipment; and the third experimental subsystem is configured to simulate and emulate target functions required by the target equipment.

[0015] According to a third aspect of the embodiments of the present application, an electronic device is provided, comprising: a processor; and a memory, wherein the memory has computer readable instructions stored thereon, and the computer readable instructions are executed by the processor to implement the simulation method of the lunar base according to any one of the above.

[0016] According to a fourth aspect of the embodiments of the present application, a computer readable storage medium is provided, wherein the computer readable storage medium has a computer program stored thereon, and the computer program is executed by a processor to implement the simulation method of the lunar base according to any one of the above.

[0017] The technical scheme provided by the embodiments of the present application can include the following beneficial effects:

[0018] The simulation system of the lunar base in the example embodiments of the present application comprises a first experiment subsystem, a second experiment subsystem and a third experiment subsystem. The first experiment subsystem is configured to simulate lunar information within a preset range, wherein the lunar information at least comprises a target device and a lunar environment, and the target device runs in the lunar environment. The second experiment subsystem is configured to perform an environment experiment on the target device, wherein the target device at least comprises a manned device, a robot device and a load device. The third experiment subsystem is configured to perform simulation and verification on a target function required by the target device. The present application not only verifies the integrity of the system construction of the lunar base within the preset range through the first experiment subsystem, but also verifies the adaptability of the target device running in the lunar base to the lunar environment through the second experiment subsystem. Finally, the function of the target device is simulated and verified through the third experiment subsystem, thereby solving the problem that the key technologies of the lunar base construction and operation cannot be effectively verified, and further improving the accuracy of the verification of the key technologies of the lunar base construction and operation.

[0019] It should be understood that the foregoing general description and the following detailed description are only exemplary and explanatory, and are not limiting to the present application. BRIEF DESCRIPTION OF DRAWINGS

[0020] The drawings incorporated in the specification and constituting a part of the specification illustrate embodiments consistent with the present application and, together with the specification, serve to explain the principles of the present application. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative labor on the basis of these drawings. In the drawings:

[0021] Figure 1 The schematic diagram of the simulation system of the lunar base according to some embodiments of the present application is schematically shown;

[0022] Figure 2 The schematic diagram of the system architecture according to some embodiments of the present application is schematically shown;

[0023] Figure 3 The schematic diagram of the simulation method of the lunar base according to some embodiments of the present application is schematically shown;

[0024] Figure 4 The structural schematic diagram of the computer system of the electronic device according to some embodiments of the present application is schematically shown;

[0025] Figure 5 The schematic diagram of the computer readable storage medium according to some embodiments of the present application is schematically shown.

[0026] In the drawings, the same or corresponding reference numerals represent the same or corresponding parts. DETAILED DESCRIPTION

[0027] Example implementations are now described with reference to the drawings. Example implementations can, however, be implemented in many different forms and should not be construed as limited to the examples set forth herein; rather, these examples are provided so that this disclosure will be thorough and complete, and will fully convey the scope of example implementations to those skilled in the art.

[0028] Moreover, the described features, structures, or characteristics can be combined in any suitable manner in one or more embodiments. In the following description, numerous specific details are provided to give a thorough understanding of embodiments of the application. One skilled in the relevant art will recognize, however, that the

[0029] In addition, the drawings are merely schematic and are not drawn to scale. A block diagram in the drawings represents a functional entity, not necessarily the physical arrangement of the entities. That is, the functional entities can be implemented in software, or in one or more hardware modules or integrated circuits, or in different network and / or processor devices and / or microcontroller devices.

[0030] In the present example embodiment, a lunar base simulation system is first provided, which can be applied to a terminal device or a server. The lunar base simulation system is described below taking the terminal device as an example. Figure 1 A schematic diagram of a lunar base simulation system according to some embodiments of the present application is shown schematically. Referring to Figure 1 As shown, the lunar base simulation system can include the following:

[0031] The first experiment subsystem 110 is configured to simulate lunar information within a preset range, wherein the lunar information at least includes a target device and a lunar environment, and the target device runs in the lunar environment.

[0032] It should be noted that the lunar base simulation system of the present application mainly includes a first experiment subsystem, a second implementation subsystem, and a third experiment subsystem.

[0033] The first experiment subsystem can be as follows: Figure 2The shown field experiment A area represents that the field experiment A area is mainly used for the full-process preliminary physical experiment of the lunar information in a wide range of lunar exploration technology. Specifically, the preset range can be a preset distance range around a landing point of a person or a device performing a lunar exploration task. The target device and the lunar environment required in the lunar base are constructed according to the preset range, and the lunar environment at least includes a lunar environment, a lunar topographic environment and the like.

[0034] Specifically, the first experimental subsystem includes: a landing image navigation module, used for simulating image navigation of a lunar lander landing; a lunar surface inspection module, used for simulating lunar topographic features, wherein the lunar topographic features at least include: lunar surface dust; a man-machine joint driving module, used for verifying whether the man-machine joint function of a manned lunar rover and a manned lunar robot is normal; and a lunar robot action module, used for simulating the motion function of a lunar robot, wherein the motion function at least includes: a preset carrying amount, a preset motion distance and a preset motion speed.

[0035] The landing image navigation module and the lunar surface inspection module can be represented by a landing image navigation and a lunar surface inspection experiment area in Figure 2 located in the field experiment A area, used for verifying lunar landing navigation and control related technologies. The construction of the experiment area includes three parts: first, the topographic design of the experiment area should be scaled down based on the lunar base site selection; second, the scaled topography can meet the image navigation of the lunar lander landing; third, the experiment area is equipped with a lunar lander motion measurement system, a data transmission communication system and a large-range lunar low-gravity simulation system. The present application improves the accuracy of key technology verification of the lunar base construction by building the landing image navigation module and the lunar surface inspection module.

[0036] The man-machine joint driving module can be represented by a man-machine joint driving experiment area in Figure 2 including: a lunar soil simulation submodule, a lunar hill simulation submodule, a lunar crater simulation submodule, a lunar obstacle simulation submodule and a lunar slope simulation submodule, located in the field experiment A area, used for verifying the man-machine joint driving key technology of the manned lunar rover and the manned lunar robot. The construction content of the experiment area is that the topographic design of the experiment area should be modularly spliced and simulated based on the lunar base site selection. The experiment area is equipped with a manned lunar rover and a manned lunar robot motion measurement system, a data transmission communication system and a lunar rover follow-up lunar low-gravity simulation system. The present application improves the accuracy of key technology verification of the lunar base construction by building the man-machine joint driving module.

[0037] The lunar robot action module can be represented by a lunar robot action experiment area in Figure 2The lunar surface robot movement, jumping and transportation experiment area in the lunar surface robot movement, jumping and transportation experiment area in the field experiment A area is used to verify the movement ability of the lunar surface robot, including the maximum carrying capacity, the maximum movement distance, the maximum movement speed, the limit terrain movement ability and the like. The construction content of the experiment area is a rough simulation of the lunar landform for the lunar base site selection, the robot movement measurement system, the data transmission communication system, the lunar low gravity simulation system. The application improves the accuracy of the key technology verification of the lunar base construction by building the lunar surface robot action module.

[0038] Specifically, the first experiment subsystem further includes: an in-situ resource utilization processing module, configured to verify whether the lunar surface resource processing robot normally performs a preset operation, wherein the preset operation at least includes: a 3D printing operation; and a first digging and mining module, configured to simulate lunar resources, wherein the lunar resources include at least one of the following: water resources, mineral resources, helium-3 resources.

[0039] The in-situ resource utilization processing module can be verified by Figure 2 The in-situ resource utilization processing experiment area in the lunar surface robot movement, jumping and transportation experiment area in the field experiment A area is used to verify the operation of the lunar surface resource processing robot related key technologies. The main construction content of the experiment area is to verify whether the key technologies of the lunar surface 3D printing robot and the lunar surface light rough simulation system are operated normally. The application improves the accuracy of the key technology verification of the lunar base construction by building the lunar surface robot action module.

[0040] As shown in Figure 2 The digging and mining experiment area is divided into two parts, one part (corresponding to the first digging and mining module in the application) is located in the field experiment A area, which is used to simulate the existence form and storage location of the lunar in-situ resources including water resources, mineral resources and helium-3 resources, and to verify the connection of the whole process technology of the lunar mining robot. The construction of this part of the experiment area includes two parts: one is the existence form and storage location simulation of the three kinds of lunar in-situ resources, water resources, mineral resources and helium-3 resources; the other is the lunar mining robot working process verification for different storage location in-situ resources. The experiment area is equipped with a lunar surface digging and mining movement measurement system and a data transmission communication system, which improves the accuracy of the key technology verification of the lunar base construction.

[0041] Specifically, the first experiment subsystem further includes: a first lunar surface robot operation and maintenance module, configured to test the operation data of the lunar surface robot and maintain the operation data of the lunar surface robot; a first lunar surface robot facility building module, configured to build the infrastructure of the lunar base, wherein the infrastructure at least includes: the base scene of the lunar base; and a first man-machine cooperation module, configured to build a man-machine cooperation digital simulation system and a man-machine cooperation operation system.

[0042] As shown in Figure 2As shown, the lunar robot autonomous operation testing and self-maintenance experimental area is designed in a cross shape, making the maintenance of various robots within the lunar base more rational. A portion of this experimental area (corresponding to the first lunar robot operation and maintenance module in this application) is located in the field experiment area A, used to verify the full-process technology of autonomous fault detection and fault repair for lunar robots. This experimental area improves the accuracy of verifying key technologies for lunar base construction by establishing a lunar robot fault simulation system and a lunar robot fault repair system.

[0043] Among them, such as Figure 2 As shown, a portion of the lunar robot construction facility experimental area (corresponding to the first lunar robot facility construction module in this application) is located in Field Experiment Area A, used to verify the entire process technology of lunar robot construction of lunar base facilities. The main construction content of this experimental area is a lunar base scene construction design system. By building a coarse simulation system of lunar terrain for lunar base site selection, and equipping it with a robot motion measurement system, a data transmission and communication system, and a large-scale lunar low gravity simulation system, the accuracy of key technology verification for lunar base construction is improved.

[0044] Among them, such as Figure 2 As shown, a portion of the human-machine collaboration experimental area (corresponding to the first human-machine collaboration module in this application) is located in the field experiment area A, which is used to verify the full-process technology of human-machine collaboration between astronauts and lunar robots living on the lunar base. This experimental area improves the accuracy of key technology verification for lunar base construction by building a human-machine collaboration digital simulation system and a human-machine collaboration operating system.

[0045] It should be noted that the first experimental subsystem also includes: a solar power plant experimental area and a service support area. The solar power plant experimental area is constructed in three modules, as shown in the attached diagram. Figure 2 As shown. During the operation of the lunar base, solar energy is currently the only available energy source. The layout primarily considers ensuring a reasonable and sufficient energy supply for various lunar robots during the operation of the lunar twin base. One module is entirely built in Field Experiment Area A to verify the entire operation process of the lunar base's solar power station. The service support area is located in Field Experiment Area A and is used to provide safety assurance and emergency response measures for the operation of the lunar base.

[0046] The second experimental subsystem 120 is used to conduct environmental experiments on the target equipment, wherein the target equipment includes at least: manned equipment, robotic equipment, and load equipment.

[0047] The second experimental subsystem can be as follows: Figure 2The shown field experiment B area represents, for example, that in the field experiment B area, the lunar environment lighting verification of the mining equipment running in the lunar environment can be carried out, and the adaptability verification of the robot equipment running in the lunar environment to the lunar terrain can be carried out. The second experiment subsystem greatly improves the accuracy of the key technology verification of the lunar base construction.

[0048] Specifically, the second experiment subsystem includes: a second mining module, used for simulating target conditions required by a mining robot in a lunar environment, wherein the target conditions at least include: lighting adaptability function, and preset working time length; a second lunar robot operation and maintenance module, used for simulating the light angle of the lunar surface light in the preset time length; a second lunar robot facility construction module, used for verifying whether the robot equipment is adapted to the lunar environment; a first digital lunar experiment module, used for displaying the detection data of the lunar base; and a first environment test experiment module, used for testing the target lunar detection equipment or target lunar detection load.

[0049] As shown in the figure, Figure 2 The mining experiment area is divided into two parts. Another part of the experiment area (corresponding to the second mining module in the application) is built in the field experiment B area. Compared with the part built in the field experiment A area, the part is additionally equipped with a lunar surface light long-time accurate simulation system with adjustable light angle, which is used for the lighting environment adaptability verification of the key equipment and equipment key load / components of the lunar mining robot, and the conventional working time length, etc.

[0050] As shown in the figure, Figure 2 Another part of the lunar robot autonomous operation test and self-maintenance experiment area (corresponding to the second lunar robot operation and maintenance module in the application) is built in the field experiment B area, which mainly verifies the lighting adaptability. By additionally building a lunar surface light long-time accurate simulation system with automatically adjustable light angle, the accuracy of the key technology verification of the lunar base construction is improved.

[0051] As shown in the figure, Figure 2 A part of the lunar robot construction facility experiment area (corresponding to the second lunar robot facility construction module in the application) is located in the field experiment B area, which mainly verifies the terrain adaptability and lighting adaptability in the construction process of the lunar robot. By additionally equipping a 1:1 scale lunar appearance accurate simulation system and a lunar surface light long-time accurate simulation system with automatically adjustable light angle, the accuracy of the key technology verification of the lunar base construction is improved.

[0052] As shown in the figure, Figure 2As shown, a portion of the digital moon experimental area (corresponding to the first digital moon experimental module in this application) is constructed in the field test area B, which is used to showcase new lunar exploration technologies researched by various aerospace institutes, enterprises, or schools. Through the first digital moon experimental module, this application not only improves the accuracy of key technology verification for lunar base construction but also realizes data sharing and display.

[0053] Among them, such as Figure 2 As shown, a portion of the environmental testing experimental area (corresponding to the first environmental testing experimental module in this application) is constructed in the field test area B for temporary or newly proposed lunar exploration equipment / payload testing. Furthermore, by equipping it with a 1:1 scale accurate lunar surface simulation system, an automatic adjustable long-term accurate simulation system for lunar surface illumination, and a lunar dust simulation system, the accuracy of key technology verification for lunar base construction is improved.

[0054] It should be noted that, as Figure 2 As shown, the second experimental subsystem also includes a solar power plant experimental area. Specifically, the solar power plant experimental area is constructed into three modules. One part of one module is located in the outdoor experimental area B, which mainly verifies key technologies such as energy conversion rate and energy transmission efficiency of key loads such as solar energy collection in the solar power plant.

[0055] The third experimental subsystem 130 is used to simulate the target functions required by the target device.

[0056] The third experimental subsystem can be as follows: Figure 2 The indoor experimental area shown indicates that, for example, the functions of mining equipment operating in the lunar environment can be simulated and verified, as can the functions of robotic equipment operating in the lunar environment. This application, through the third experimental subsystem, greatly improves the accuracy of key technology verification for lunar base construction.

[0057] Specifically, the third experimental subsystem includes: a third lunar robot facility construction module, used to verify whether the lunar robot can adapt to the lunar environment when the lunar surface is covered with dust; a second human-machine collaboration module, used to identify preset commands sent by astronauts to the lunar robot, wherein the preset commands include at least one of the following: action commands and facial expression commands; a second digital moon experiment module, used to visualize the application scenarios of the lunar base; a second environmental testing experiment module, used to simulate the preset temperature environment required for the lunar base through a hot vacuum tank; and a lunar exploration experience module, used to provide astronauts with experience functions of the application scenarios.

[0058] Among them, such as Figure 2As shown, a portion of the lunar robot construction facility experimental area (corresponding to the third lunar robot facility construction module in this application) is located in the inner field experimental area, which can verify the adaptability of the lunar robot to the lunar dust environment during the construction process. Furthermore, by additionally equipping a lunar dust environment simulation system, the accuracy of verifying key technologies for lunar base construction is improved.

[0059] Among them, such as Figure 2 As shown, a portion of the human-machine collaboration experimental area (corresponding to the second human-machine collaboration module in this application) is constructed in the indoor experimental area. It is mainly used for the verification of key technologies such as astronaut motion capture, facial expression capture, command generation and transmission during human-machine collaboration. By constructing an additional human-machine collaboration software integration system required for the above-mentioned key technologies, the accuracy of key technology verification for lunar base construction is improved.

[0060] Among them, such as Figure 2 As shown, a portion of the digital moon experimental area (corresponding to the second digital moon experimental module in this application) is located in the inner field experimental area, which is used for popularizing manned lunar landing technology for visitors or school students. Through visual simulation technology, visitors or school students can experience various scenarios of manned lunar landing and life on the lunar base, thereby improving the accuracy of key technology verification for lunar base construction.

[0061] Among them, such as Figure 2 As shown, a portion of the environmental testing experimental area (corresponding to the second environmental testing experimental module in this application) is located in the indoor experimental area to simulate the extreme temperature environment of the lunar base, thereby testing the extreme environmental adaptability of the lunar robot. By constructing a thermal vacuum tank that can cover the day and night temperature changes on the lunar surface, along with a motion measurement system and a data transmission and communication system, the accuracy of key technology verification for the construction of the lunar base is improved.

[0062] It should be noted that, as Figure 3 As shown, the third experimental subsystem also includes a solar power station experimental area and a lunar exploration experience area. Specifically, the solar power station experimental area is constructed in three modules. Part of one module is located in the inner field experimental area, mainly for functional simulation verification of each process in the entire operation of the lunar base solar power station. The lunar exploration experience area is located in the inner field experimental area and is used for training base personnel or astronauts to experience the entire process of lunar exploration and life. Through numerical simulation and scenario simulation, base personnel or astronauts experience various scenarios of life on the lunar base, improving the accuracy of key technology verification for lunar base construction.

[0063] In summary, according to the simulation system of the lunar base in the present example embodiment, the simulation system comprises a first experimental subsystem, a second experimental subsystem, and a third experimental subsystem. The first experimental subsystem is configured to simulate lunar information within a preset range, wherein the lunar information at least comprises a target device and a lunar environment, and the target device is operated in the lunar environment. The second experimental subsystem is configured to perform an environmental experiment on the target device, wherein the target device at least comprises a manned device, a robot device, and a load device. The third experimental subsystem is configured to perform simulation and emulation on a target function required by the target device. The present application not only verifies the integrity of the system construction of the lunar base within the preset range through the first experimental subsystem, but also verifies the adaptability of the target device running in the lunar base to the lunar environment through the second experimental subsystem. Finally, the function of the target device is simulated and verified through the third experimental subsystem, thereby solving the problem that the key technologies of the lunar base construction and operation cannot be effectively verified, and further improving the accuracy of the verification of the key technologies of the lunar base construction and operation.

[0064] In the present example embodiment, a simulation method of a lunar base is also provided, which can be applied to a terminal device or a server. Hereinafter, the simulation method of the lunar base is described by taking the terminal device as an example. Figure 3 A schematic diagram of a simulation method of a lunar base according to some embodiments of the present application is schematically shown. Referring to Figure 4 As shown, the simulation method of the lunar base can comprise the following steps:

[0065] In step S310, a first experimental subsystem is used to simulate lunar information within a preset range, wherein the lunar information at least comprises a target device and a lunar environment, and the target device is operated in the lunar environment.

[0066] In step S320, a second experimental subsystem is used to perform an environmental experiment on the target device, wherein the target device at least comprises a manned device, a robot device, and a load device.

[0067] In step S330, a third experimental subsystem is used to perform simulation and emulation on a target function required by the target device.

[0068] It should be noted that although the steps in the present application are described in a specific order in the accompanying drawings, this does not require or imply that the steps must be performed in this specific order, or that all the steps shown must be performed to achieve the desired results. Additionally or alternatively, some steps can be omitted, a plurality of steps can be combined into one step, and / or one step can be divided into a plurality of steps, etc.

[0069] The specific details of the simulation method for the lunar base mentioned above have been described in detail in the corresponding lunar base simulation system, so they will not be repeated here.

[0070] It should be noted that although several modules or units of the lunar base simulation system have been mentioned in the detailed description above, this division is not mandatory. In fact, according to the embodiments of this application, the features and functions of two or more modules or units described above can be embodied in one module or unit. Conversely, the features and functions of one module or unit described above can be further divided and embodied by multiple modules or units.

[0071] Furthermore, in an exemplary embodiment of this application, an electronic device capable of implementing the above-described lunar base simulation method is also provided.

[0072] Those skilled in the art will understand that various aspects of this application can be implemented as a system or a program product. Therefore, various aspects of this application can be specifically implemented as: a completely hardware embodiment, a completely software embodiment (including firmware, microcode, etc.), or an embodiment combining hardware and software aspects, collectively referred to herein as a "circuit," "module," or "system."

[0073] The following reference Figure 4 To describe an electronic device 400 according to such an embodiment of the present application. Figure 4 The electronic device 400 shown is merely an example and should not impose any limitations on the functionality and scope of use of the embodiments of this application.

[0074] like Figure 3 As shown, the electronic device 400 is manifested in the form of a general-purpose computing device. The components of the electronic device 400 may include, but are not limited to: at least one processing unit 410, at least one storage unit 420, a bus 430 connecting different system components (including storage unit 420 and processing unit 410), and a display unit 440.

[0075] The storage unit stores program code, which can be executed by the processing unit 410 to perform the steps described in the "Exemplary" section above, according to various exemplary embodiments of this application. For example, the processing unit 410 can perform actions such as... Figure 5At step S310 shown in the middle, the moon information in a preset range is simulated by the first experimental subsystem, wherein the moon information at least includes: a target device, a moon environment, wherein the target device runs in the moon environment; at step S320, the target device is subjected to environment experiment by the second experimental subsystem, wherein the target device at least includes: a manned device, a robot device, and a load device; at step S330, a target function required by the target device is simulated by the third experimental subsystem.

[0076] The storage unit 420 can include a readable medium in the form of a volatile storage unit, such as a random access memory (RAM) 421 and / or a cache memory 422, and can further include a read-only memory (ROM) 423.

[0077] The storage unit 420 can also include a program / utility 424 having a set (at least one) of program modules 425, such as an operating system, one or more application programs, other program modules, and program data, each of which can give implementation to the network environment in one or some combination of the examples.

[0078] The bus 430 can represent one or more of several types of bus structures, including a storage unit bus or bus controller, a peripheral bus, a graphics acceleration port, a processing unit bus, or a local bus using any of a variety of bus architectures.

[0079] The electronic device 400 can also communicate with one or more external devices 470, such as a keyboard or pointing device, a Bluetooth device, etc.; other devices that enable a user to interact with the electronic device 400; and / or one or more devices that enable the electronic device 400 to communicate with one or more other computing devices. Such communication can be facilitated by an input / output (I / O) interface 450. Still yet, the electronic device 400 can communicate with one or more networks, such as a local area network (LAN), a wide area network (WAN), and / or the public network, such as the Internet, via a network adapter 460. As depicted, the network adapter 460 communicates with the other components of the electronic device 400 via the bus 430. It should be appreciated that although not shown, other hardware and / or software components could be used in conjunction with the electronic device 400. These include, but are not limited to, microcode, device drivers, redundant processing units, external disk drive arrays, RAID systems, tape drives, and data archival storage systems, etc.

[0080] Those skilled in the art can easily understand from the above description of the embodiments that the example embodiments described herein can be implemented by software or by software in combination with necessary hardware. Therefore, the technical solutions according to the embodiments of the present application can be embodied in the form of a software product, which can be stored in a non-volatile storage medium (which can be a CD-ROM, a U disk, a mobile hard disk, etc.) or a network, and includes a number of instructions to make a computing device (which can be a personal computer, a server, a terminal device, or a network device, etc.) execute the steps according to the embodiments of the present application.

[0081] In the example embodiments of the present application, a computer readable storage medium is also provided, on which the program product capable of implementing the above-mentioned program product of the present specification is stored. In some possible embodiments, various aspects of the present application can also be implemented in the form of a program product, which includes program codes for causing a terminal device to execute the steps described in the "example" part of the present specification according to various example embodiments of the present application when the program product is run on the terminal device.

[0082] Reference ​ As shown, the program product 500 for implementing the simulation system of the lunar base according to the embodiments of the present application is described, which can adopt a portable compact disc read-only memory (CD-ROM) and includes program codes, and can be run on a terminal device, such as a personal computer. However, the program product of the present application is not limited thereto, and in the present document, the readable storage medium can be any tangible medium containing or storing a program, which can be used by or in combination with an instruction execution system, device or apparatus.

[0083] The program product can adopt any combination of one or more readable media. The readable medium can be a readable signal medium or a readable storage medium. The readable storage medium may, for example, be but is not limited to an electrical, magnetic, optical, electromagnetic, infrared, or semiconductor system, device or apparatus, or any combination of the above. More specific examples (non-exhaustive list) of the readable storage medium include an electrical connection having one or more wires, a portable disc, a hard disk, a random access memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or flash memory), an optical fiber, a portable compact disc read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the above.

[0084] A computer readable signal medium can include a propagated data signal with computer readable program code embodied therein, for example, in baseband or as part of a carrier wave. Such a propagated signal can take any of a variety of forms, including, but not limited to, electro-magnetic, optical, or any suitable combination thereof. A computer readable signal medium can be any computer readable medium that can be involved in

[0085] The code can be transmitted in any form, including, but not limited to, radio frequency, optical, electrical, or the like, or any suitable combination thereof.

[0086] The program code can be implemented in any of a variety of programming languages, including, but not limited to, C, C++, Java, or the like, and can be executed by one or more processors. The program code can execute entirely on a user's computing device, partly on the user's computing device, as a stand-alone software package, partly on the user's computing device and partly on a remote computing device, or entirely on the remote computing device or server. In the latter scenario, the remote computing device can be connected to the user's computing device through any type of network, including, but not limited to, a local area network (LAN) or a wide area network (WAN), or the connection can be made to an external computing device, such as through the Internet using an Internet Service Provider (ISP). It will be appreciated that the network connections shown are exemplary and other

[0087] In addition, the above-described flowcharts are merely illustrative examples of the processes included in the exemplary embodiments of the present application, and are not intended to limit the present application. It is readily understood that the processes shown in the above-described flowcharts do not indicate or limit the time sequence of the processes. In addition, it is readily understood that the processes can be executed synchronously or asynchronously, for example, in a plurality of modules.

[0088] From the above description of the embodiments, it is readily understood by those skilled in the art that the example embodiments described herein can be implemented by software and also can be implemented by software in combination with necessary hardware. Therefore, the technical solution according to the embodiments of the present application can be embodied in the form of a software product, which can be stored in a non-volatile storage medium (which can be a CD-ROM, a USB flash disk, a mobile hard disk, or the like) or a network, and includes a plurality of instructions to make a computing device (which can be a personal computer, a server, a touch terminal, or a network device, etc.) execute the technical solution according to the embodiments of the present application.

[0089] Other embodiments of the application will be apparent to those skilled in the art from consideration of the specification and practice of the application disclosed herein. It is intended that the specification and examples be considered as exemplary only, with the true scope and spirit of the application being indicated by the following claims.

[0090] It is to be understood that the application is not limited to the precise construction herein disclosed and shown in the drawings, and that various changes in shape, size and arrangements of parts can be made without departing from the scope of the application. The scope of the application is limited only by the claims that follow.

Claims

1. A simulation system for a lunar base, characterized in that, include: The first experimental subsystem, the second experimental subsystem, and the third experimental subsystem, among which... The first experimental subsystem is used to simulate lunar information within a preset range, wherein the lunar information includes at least: a target device and a lunar environment, wherein the target device operates in the lunar environment; The second experimental subsystem is used to conduct environmental experiments on the target device, wherein the target device includes at least: a manned device, a robotic device, and a load device; The third experimental subsystem is used to simulate the target functions required by the target device. The first experimental subsystem includes: The landing image navigation module is used to simulate image navigation for a lunar lander landing. The construction of the experimental area corresponding to the landing image navigation module includes three parts: first, the terrain design of the experimental area should be scaled down with reference to the selection of the lunar base site; second, the scaled-down terrain design should be able to meet the image navigation requirements of the lunar lander during landing; and third, it should have the ability to simulate the cross-coupling effects of the lander and lunar dust during landing. The experimental area is equipped with a lunar lander motion measurement system, a data transmission and communication system, and a large-scale lunar low gravity simulation system. The lunar surface exploration module is used to simulate lunar surface features, wherein the lunar surface features include at least: dust covering the lunar surface; The human-machine joint driving module is used to verify whether the human-machine joint function of the manned lunar rover and the manned lunar robot is normal. The construction content of the experimental area corresponding to the human-machine joint driving module is that the terrain design of the experimental area should be modularly spliced ​​and simulated with reference to the selection of the lunar base site. The experimental area is equipped with a manned lunar rover, a motion measurement system for the manned lunar robot, a data transmission and communication system, and a lunar rover follow-up lunar low gravity simulation system. The lunar robot motion module is used to simulate the motion functions of a lunar robot. The motion functions include at least: preset payload quantity, preset motion distance, and preset motion speed. The experimental area construction content corresponding to the lunar robot motion module includes a rough simulation of the lunar landscape for selecting a lunar base site, and the installation of a robot motion measurement system, a data transmission and communication system, and a lunar low gravity simulation system. The in-situ resource utilization and processing module is used to verify whether the lunar surface resource processing robot is performing preset operations normally, wherein the preset operations include at least: 3D printing operation; The first mining module is used to simulate lunar resources, including water, minerals, and helium-3. The construction of the experimental area corresponding to the first mining module includes two parts: first, simulating the existence forms and storage locations of the three in-situ lunar resources, namely water, minerals, and helium-3; second, verifying the workflow of the lunar mining robot for in-situ resources in different storage locations. The experimental area is equipped with a lunar surface mining motion measurement system and a data transmission and communication system. The first lunar robot operation and maintenance module is used to test the operational data of the lunar robot and maintain the operational data of the lunar robot; the experimental area corresponding to the first lunar robot operation and maintenance module is equipped with a lunar robot fault simulation system and a lunar robot fault repair system. The first lunar surface robot facility construction module is used to construct the infrastructure of the lunar base, wherein the infrastructure includes at least: the base scene of the lunar base; the experimental area corresponding to the first lunar surface robot facility construction module is equipped with a rough simulation system of the lunar landscape for selecting the lunar base site, a robot motion measurement system, a data transmission and communication system, and a large-scale lunar low gravity simulation system; The first human-machine collaboration module is used to construct a human-machine collaborative digital simulation system and a human-machine collaborative operating system; the experimental area corresponding to the first human-machine collaboration module is equipped with a human-machine collaborative digital simulation system and a human-machine collaborative operating system. The first experimental subsystem also includes a solar power station experimental area and a service support area. The solar power station experimental area is constructed in three modules, one of which is entirely built in the field experiment A area to verify the entire operation process of the solar power station at the lunar base. The service support area is located in the field experiment A area and is used to provide safety assurance and emergency measures for the operation of the lunar base. The second experimental subsystem includes: The second mining module is used to simulate the target conditions required by the mining equipment of the lunar mining robot in the lunar environment. The target conditions include at least: light adaptation function and preset working time. The experimental area corresponding to the second mining module is additionally equipped with a long-term lunar surface light simulation system with adjustable light angle. The second lunar robot operation and maintenance module is used to simulate the lunar surface illumination angle within a preset time period; an additional long-term lunar surface illumination simulation system with automatically adjustable illumination angle is built in the experimental area corresponding to the second lunar robot operation and maintenance module. The second lunar surface robot facility construction module is used to verify whether the robot equipment is adapted to the lunar environment; the experimental area corresponding to the second lunar surface robot facility construction module is additionally equipped with a 1:1 scale lunar appearance simulation system and a long-term lunar surface illumination simulation system with automatically adjustable illumination angle. The first digital lunar experiment module is used to display the exploration data from the lunar base; The first environmental testing experimental module is used to test the target lunar exploration equipment or the target lunar exploration payload; the experimental area corresponding to the first environmental testing experimental module is equipped with a 1:1 scale lunar surface simulation system, a long-term lunar surface illumination simulation system with automatically adjustable illumination angle, and a lunar dust simulation system. The second experimental subsystem corresponds to the solar power plant experimental area, and part of one of its modules is located in the field experiment area B, which is used to verify the key technologies of energy conversion rate and energy transmission efficiency of the key load of solar energy collection in the solar power plant. The third experimental subsystem includes: The third lunar robot facility construction module is used to verify whether the lunar robot can adapt to the lunar environment when the lunar surface is covered with dust; the experimental area corresponding to the third lunar robot facility construction module is additionally equipped with a lunar dust environment simulation system. The second digital moon experiment module is used to visualize the application scenarios of the lunar base; The lunar exploration experience module is used to provide astronauts with the ability to experience the application scenarios. The experimental area corresponding to the lunar exploration experience module allows trainees or astronauts at the base to experience various scenarios of life at the lunar base through numerical simulation and scenario simulation. The second human-machine collaboration module is used to identify preset commands sent by the astronaut to the lunar robot, wherein the preset commands include at least one of the following: action commands and facial expression commands; the experimental area corresponding to the second human-machine collaboration module is additionally equipped with a human-machine collaboration software integration system required for astronaut motion capture, facial expression capture, command generation and sending technology; The second environmental testing module is used to simulate the preset temperature environment required by the lunar base through a hot vacuum tank. The experimental area corresponding to the second environmental testing module is constructed with a hot vacuum tank that can cover the day and night temperature changes on the lunar surface, and is also equipped with a motion measurement system and a data transmission and communication system. A portion of a module in the solar power station experimental area corresponding to the third experimental subsystem is located in the indoor experimental area, and is used to perform functional simulation verification of each process in the entire operation process of the lunar base solar power station.

2. The system according to claim 1, characterized in that, The human-machine joint driving module includes: lunar soil simulation submodule, lunar hill simulation submodule, lunar crater simulation submodule, lunar surface obstacle simulation submodule, and lunar surface slope simulation submodule.

3. A method for simulating a lunar base, characterized in that, The simulation system applied to the lunar base as described in any one of claims 1 to 2 comprises: a first experimental subsystem, a second experimental subsystem, and a third experimental subsystem, wherein, The first experimental subsystem simulates lunar information within a preset range, wherein the lunar information includes at least: a target device and a lunar environment, wherein the target device operates in the lunar environment; The target device is subjected to environmental experiments through the second experimental subsystem, wherein the target device includes at least: manned equipment, robotic equipment, and load-bearing equipment; The target functions required by the target device are simulated through the third experimental subsystem.

4. An electronic device, comprising: processor; as well as A memory storing computer-readable instructions that, when executed by the processor, implement the lunar base simulation method as described in claim 3.

5. A computer-readable storage medium having a computer program stored thereon, which, when executed by a processor, implements the simulation method for a lunar base as described in claim 3.

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