Control method, system, device and equipment of intelligent cockpit system

Abstract

The application discloses a control method, system and device of an intelligent cockpit system and equipment, and belongs to the technical field of intelligent cockpits. In the method, a processor of the intelligent cockpit system controls a display screen to display a plurality of interactive controls on an interactive interface, so that a user can select a working mode of the system, and then controls an antenna assembly associated with the working mode to be in a working state according to the working mode selected by the user. When the user switches the working mode, the current antenna assembly is controlled to be in an off state, and the antenna assembly associated with the working mode after the switching is controlled to be in the working state, so that the switching of the working mode is realized. In this way, the radiation and interference between different antennas are avoided, the system is ensured to be in a minimum interference environment, and the operation performance of the system and the human-computer interaction experience are improved.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of intelligent cockpit, and in particular to a control method, system, device and equipment of an intelligent cockpit system. BACKGROUND

[0002] In recent years, the automobile industry has entered an era of intelligence and electrification, and the development of intelligent cockpits is inevitable. The intelligent cockpit has more and more functions.

[0003] In the related art, in order to achieve the diversity and complexity of the intelligent cockpit function, multiple antennas such as a radio antenna, a Bluetooth antenna, a Global Positioning System (GPS) antenna, etc. are integrated in the intelligent cockpit system, and the radiation interference between different antennas is avoided by means of hardware board optimization.

[0004] However, although the hardware board optimization can reduce the radiation interference between different antennas to some extent, it cannot completely avoid the radiation interference, resulting in poor running performance of the intelligent cockpit system. SUMMARY

[0005] The embodiments of the present application provide a control method, system, device and equipment of an intelligent cockpit system, which can effectively avoid the radiation interference between different antennas in the system and improve the running performance of the system. The technical solution is as follows.

[0006] In a first aspect, a control method of an intelligent cockpit system is provided, applied to a processor of the intelligent cockpit system, the system further comprising a display screen and a plurality of antenna assemblies, the antenna assembly comprising a processing module control circuit, a processing module and an antenna, and the method comprising:

[0007] controlling the display screen to display a plurality of interactive controls on an interactive interface, the interactive controls indicating a working mode of the system, the working mode being associated with the antenna assembly;

[0008] in response to a trigger operation implemented on a first interactive control in the plurality of interactive controls, controlling a first antenna assembly in the plurality of antenna assemblies to be in a working state to realize a first working mode indicated by the first interactive control, wherein a first processing module control circuit in the first antenna assembly is controlled to supply power to a first processing module in the first antenna assembly, so that the first processing module receives a first signal transmitted by a first antenna in the first antenna assembly;

[0009] in response to a triggering operation performed on a second interaction control in the plurality of interaction controls, controlling the first antenna assembly to be in an off state and a second antenna assembly in the plurality of antenna assemblies to be in an on state to implement a second operation mode indicated by the second interaction control, wherein the first processing module control circuit is controlled to power off the first processing module so that the first processing module does not receive the first signal, and the second processing module control circuit in the second antenna assembly is controlled to power on the second processing module in the second antenna assembly so that the second processing module receives a second signal transmitted by a second antenna in the second antenna assembly.

[0010] In some embodiments, the plurality of antenna assemblies comprises any of the following:

[0011] a radio antenna assembly for implementing a radio mode of the system;

[0012] a Bluetooth antenna assembly for implementing a Bluetooth mode of the system;

[0013] a WIFI antenna assembly for implementing a network mode of the system;

[0014] a GPS antenna assembly for implementing a positioning mode of the system;

[0015] a communication antenna assembly for implementing a communication mode of the system.

[0016] In some embodiments, in response to a triggering operation performed on a second interaction control in the plurality of interaction controls, the first antenna assembly is controlled to be in an off state and a second antenna assembly in the plurality of antenna assemblies is controlled to be in an on state to implement a second operation mode indicated by the second interaction control, comprising:

[0017] in response to a triggering operation performed on the second interaction control, the display screen is controlled to display first prompt information on the interaction interface, the first prompt information indicating that the operation mode of the system is switched from the first operation mode to the second operation mode;

[0018] in response to a triggering operation performed on the first prompt information, the first antenna assembly is controlled to be in an off state and the second antenna assembly is controlled to be in an on state to switch the operation mode of the system from the first operation mode to the second operation mode.

[0019] In some embodiments, the method further comprises:

[0020] In response to a triggering operation performed on the second interaction control, the display screen is controlled to display second prompt information on the interactive interface, the second prompt information indicating that the working mode of the system is adjusted to be parallel to the first working mode and the second working mode.

[0021] In response to a triggering operation performed on the second prompt information, on the basis of the first antenna component being controlled to be in a working state, the second antenna component is controlled to be in a working state to realize that the first working mode and the second working mode are parallel.

[0022] In some embodiments, on the basis of the first antenna component being controlled to be in a working state, the second antenna component is controlled to be in a working state to realize that the first working mode and the second working mode are parallel, including:

[0023] The first antenna component and the second antenna component are controlled to be in a working state alternately in different time periods to realize that the first working mode and the second working mode are parallel.

[0024] In some embodiments, the first antenna component and the second antenna component are controlled to be in a working state alternately in different time periods to realize that the first working mode and the second working mode are parallel, including:

[0025] The first antenna component is controlled to be in a working state in a first time period and a third time period, and the second antenna component is controlled to be in a working state in a second time period and a fourth time period, the second time period being between the first time period and the third time period, and the fourth time period being after the third time period.

[0026] The first processing module is configured to simulate a first signal transmitted by the first antenna in the second time period based on a first signal received in the first time period and the third time period, and the second processing module is configured to simulate a second signal transmitted by the second antenna in the third time period based on a second signal received in the second time period and the fourth time period.

[0027] In a second aspect, an intelligent cockpit system is provided, the system including a processor, a display screen, and a plurality of antenna components, the antenna components including processing module control circuit, processing module, and antenna.

[0028] The processor is configured to:

[0029] The display screen is controlled to display a plurality of interaction controls on an interactive interface, the interaction controls indicating a working mode of the system, the working mode being associated with the antenna components.

[0030] in response to a triggering operation performed on a first interaction control in the plurality of interaction controls, controlling a first antenna assembly in the plurality of antenna assemblies to be in an active state to implement a first working mode indicated by the first interaction control, wherein the processor controls a first processing module control circuit in the first antenna assembly to supply power to a first processing module in the first antenna assembly to enable the first processing module to receive a first signal transmitted by a first antenna in the first antenna assembly;

[0031] in response to a triggering operation performed on a second interaction control in the plurality of interaction controls, controlling the first antenna assembly to be in an inactive state and a second antenna assembly in the plurality of antenna assemblies to be in an active state to implement a second working mode indicated by the second interaction control, wherein the processor controls the first processing module control circuit to cut off power to the first processing module to disable the first processing module from receiving the first signal, and controls a second processing module control circuit in the second antenna assembly to supply power to a second processing module in the second antenna assembly to enable the second processing module to receive a second signal transmitted by a second antenna in the second antenna assembly.

[0032] In a third aspect, a control device of an intelligent cockpit system is provided, configured to a processor of the intelligent cockpit system, the system further comprising a display screen and a plurality of antenna assemblies, the antenna assemblies comprising a processing module control circuit, a processing module, and an antenna; the device comprising:

[0033] a display screen control unit configured to control the display screen to display a plurality of interaction controls on an interaction interface, the interaction controls indicating working modes of the system, the working modes being associated with the antenna assemblies;

[0034] an antenna assembly control unit configured to, in response to a triggering operation performed on a first interaction control in the plurality of interaction controls, control a first antenna assembly in the plurality of antenna assemblies to be in an active state to implement a first working mode indicated by the first interaction control, wherein the processor controls a first processing module control circuit in the first antenna assembly to supply power to a first processing module in the first antenna assembly to enable the first processing module to receive a first signal transmitted by a first antenna in the first antenna assembly;

[0035] The antenna assembly control unit is further configured to, in response to a triggering operation performed on a second interactive control in the plurality of interactive controls, control the first antenna assembly to be in an off state and control a second antenna assembly in the plurality of antenna assemblies to be in an on state, so as to realize a second working mode indicated by the second interactive control, wherein the processor controls the first processing module control circuit to power off the first processing module, so that the first processing module does not receive the first signal, and controls the second processing module control circuit in the second antenna assembly to power on the second processing module in the second antenna assembly, so that the second processing module receives a second signal transmitted by a second antenna in the second antenna assembly.

[0036] In a fourth aspect, an electronic device is provided, which includes a memory and a processor, and the memory stores at least one computer program, which is loaded and executed by the processor to implement the control method of the intelligent cockpit system according to the first aspect.

[0037] In a fifth aspect, a computer readable storage medium is provided, which stores at least one computer program, which is loaded and executed by a processor to implement the control method of the intelligent cockpit system according to the first aspect.

[0038] To sum up, in the control method of the intelligent cockpit system provided in the embodiments of the present application, the processor of the intelligent cockpit system controls the display screen to display a plurality of interactive controls on the interactive interface, so that the user can select the working mode of the system, and then controls the antenna assembly associated with the working mode to be in an on state according to the working mode selected by the user, and when the user switches the working mode, controls the current antenna assembly to be in an off state and controls the antenna assembly associated with the working mode after the switching to be in an on state, so as to realize the switching of the working mode, thus avoiding the radiation and interference between different antennas, ensuring that the system is in a minimum interference environment, and further improving the system running performance and the human-computer interaction experience. BRIEF DESCRIPTION OF DRAWINGS

[0039] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings needed in the embodiment description will be briefly introduced. 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.

[0040] Figure 1 is a schematic diagram of an implementation environment provided by the embodiments of the present application;

[0041] Figure 2is a schematic diagram of an intelligent cockpit system provided by an embodiment of the present application;

[0042] Figure 3 is a flowchart of a control method of an intelligent cockpit system provided by an embodiment of the present application;

[0043] Figure 4 is another schematic diagram of an intelligent cockpit system provided by an embodiment of the present application;

[0044] Figure 5 is a schematic diagram of a control device of an intelligent cockpit system provided by an embodiment of the present application;

[0045] Figure 6 is a structural schematic diagram of an electronic device provided by an embodiment of the present application. DETAILED DESCRIPTION

[0046] To make the objectives, technical solutions and advantages of the present application clearer, the embodiments of the present application will be further described in detail below with reference to the drawings.

[0047] It should be noted that the information (including but not limited to user device information, user personal information, etc.), data (including but not limited to data for analysis, stored data, displayed data, etc.) and signals involved in the present application are all authorized by the user or fully authorized by all parties, and the collection, use and processing of related data need to comply with relevant laws, regulations and standards of relevant countries and regions. For example, the triggering operation, prompt information and the like involved in the present application are obtained under the condition of full authorization.

[0048] Figure 1 is a schematic diagram of an implementation environment provided by an embodiment of the present application. As shown in Figure 1 The implementation environment includes an intelligent cockpit system 100, which is deployed in a physical vehicle, for example, a vehicle-mounted terminal of a physical vehicle. Illustratively, the intelligent cockpit system 100 includes a processor 101, a display screen 102 and a plurality of antenna assemblies 103. The processor 101 is in communication connection with the display screen 102 and the plurality of antenna assemblies 103, respectively. In some embodiments, the intelligent cockpit system 100 can also be understood as an intelligent cockpit domain controller, which is not limited in the present application.

[0049] The processor 101 is configured to control the display screen 102 to display an interactive interface to realize human-computer interaction. In the embodiment of the present application, the intelligent cockpit system 100 includes multiple working modes, each antenna assembly 103 corresponds to one working mode, and the processor 101 is configured to control the multiple antenna assemblies 103 to switch between the working state and the off state to control the intelligent cockpit system 100 to switch between different working modes, that is, to realize the control method of the intelligent cockpit system provided in the present application. In addition, the number of processors 101 is not limited in the present application. For example, the processor 101 includes multiple types of processors, such as a microcontroller unit (MCU) and a system on chip (SOC), and the MCU and the SOC cooperatively realize the functions of the processor 101.

[0050] For any one antenna assembly 103, the antenna assembly 103 includes a processing module control circuit, a processing module, and an antenna. The processing module control circuit is in communication connection with the processing module, and the processing module control circuit controls the processing module to realize corresponding functions by powering on or powering off the processing module. The processing module is in communication connection with the antenna, and the processing module is configured to receive signals transmitted by the antenna, process the received signals, and send the processed signals to a peripheral circuit through an interface to drive the peripheral circuit to output signals, thereby realizing a corresponding working mode.

[0051] Illustratively, the multiple antenna assemblies 103 include any of the following multiple items:

[0052] (1) A radio antenna assembly for realizing a radio mode of the system; wherein the radio mode refers to receiving radio signals through a radio antenna to drive a vehicle-mounted loudspeaker to output radio sounds.

[0053] (2) A Bluetooth antenna assembly for realizing a Bluetooth mode of the system; wherein the Bluetooth mode refers to receiving Bluetooth signals through a Bluetooth antenna to realize functions such as Bluetooth calls and Bluetooth music.

[0054] (3) A WIFI antenna assembly for realizing a network mode of the system; wherein the network mode refers to receiving WIFI signals through a WIFI antenna to realize functions such as vehicle-mounted WIFI connection.

[0055] (4) A GPS antenna assembly for realizing a positioning mode of the system; wherein the navigation mode refers to receiving GPS positioning signals through a GPS antenna to realize functions such as navigation positioning.

[0056] (5) A communication antenna assembly for realizing a communication mode of the system; wherein the communication mode refers to receiving signals through a communication antenna such as a 4G / 5G communication antenna to realize functions such as data communication between the vehicle and an external network.

[0057] It should be noted that the above several antenna assemblies are only for illustration and do not constitute a limitation on the present application. In actual applications, more or fewer antenna assemblies can be configured according to requirements to achieve corresponding functions.

[0058] The architecture of the above intelligent cockpit system 100 is exemplarily illustrated below by taking a plurality of antenna assemblies 103 including a radio antenna assembly, a Bluetooth antenna assembly, a WIFI antenna assembly, and a GPS antenna assembly as an example. Referring to Figure 2 , Figure 2 is a schematic diagram of an architecture of an intelligent cockpit system provided by an embodiment of the present application. As shown in Figure 2 , the intelligent cockpit system 100 includes a processor 101, a display screen 102, a radio antenna assembly 103a, a Bluetooth antenna assembly 103b, a WIFI antenna assembly 103c, and a GPS antenna assembly 103d.

[0059] The processor 101 includes an MCU and an SOC, and the MCU and the SOC cooperatively implement the functions possessed by the processor 101. For example, the MCU and the SOC communicate with each other in a universal asynchronous receiver / transmitter (UART) communication mode and a serial peripheral interface (SPI) communication mode, which is not limited by the present application. Illustratively, the processor 101 is configured to run system applications and local applications, control the display screen 102 to display corresponding interactive interfaces, and perform software and hardware resource allocation and scheduling through an operating system (such as an Android system), and the like. The functions possessed by the processor 101 are not limited by the present application. For example, when a user implements various triggering operations on the interactive interface displayed by the display screen, the Android operating system receives a request for switching of a working mode, and informs the SOC of corresponding control information. After receiving the control request, the SOC informs the MCU of corresponding commands in a UART serial port communication mode or an SPI communication mode.

[0060] Illustratively, the radio antenna assembly 103a includes a radio module control circuit, a radio module, and a radio antenna; the Bluetooth antenna assembly 103b includes a Bluetooth module control circuit, a Bluetooth module, and a Bluetooth antenna; the WIFI antenna assembly 103c includes a network module control circuit, a network module, and a WIFI antenna; and the GPS antenna assembly 103d includes a positioning module control circuit, a positioning module, and a GPS antenna.

[0061] In some embodiments, the intelligent cockpit system 100 further includes a peripheral control circuit and a peripheral device, which are not limited by the present application.

[0062] Based on the above Figure 1 And Figure 2 The intelligent cockpit system 100 shown in the embodiment of the application provides a control method of an intelligent cockpit system, referring to Figure 3 , Figure 3 The flow chart of the control method of the intelligent cockpit system provided by the embodiment of the application, the method is applied to a processor of an intelligent cockpit system, the system further includes a display screen and a plurality of antenna assemblies, the antenna assembly includes a processing module control circuit, a processing module and an antenna, as shown in Figure 3 The method includes the following steps 301 to 303.

[0063] 301、The processor controls the display screen to display a plurality of interactive controls on the interactive interface, the interactive control indicates the working mode of the system, and the working mode is associated with the antenna assembly.

[0064] In the embodiment of the application, the processor runs the system application, controls the display screen to display a plurality of interactive controls on the interactive interface, for example, the interactive control is in the form of a key, a tab, a floating window, a pendant, etc., the application does not limit the display form of the interactive control, and the size and position of the interactive control can be adjusted according to the actual application. Among them, one interactive control corresponds to one working mode, and one working mode corresponds to one antenna assembly. Based on the foregoing introduction, the working mode of the system includes a radio mode, a Bluetooth mode, a network mode, a positioning mode, a communication mode, etc. Correspondingly, the antenna assembly includes a radio antenna assembly, a Bluetooth antenna assembly, a WIFI antenna assembly, a GPS antenna assembly, a communication antenna assembly, etc. Herein, no further description is given.

[0065] 302、The processor responds to the trigger operation implemented on the first interactive control in the plurality of interactive controls, controls the first antenna assembly in the plurality of antenna assemblies to be in a working state, to realize the first working mode indicated by the first interactive control.

[0066] In the embodiment of the application, the first interactive control refers to any one of the plurality of interactive controls, and the first interactive control indicates the first working mode, which is associated with the first antenna assembly. The trigger operation implemented on the first interactive control can be a single click, a long press, a double click, etc. operation implemented on the first interactive control on the interactive interface, or a voice input operation, which is not limited by the application.

[0067] Based on the foregoing introduction, the antenna assembly includes the processing module control circuit, the processing module and the antenna. Correspondingly, the first antenna assembly includes the first processing module control circuit, the first processing module and the first antenna. Illustratively, the processor controls the first antenna assembly to be in the working state, including: controlling the first processing module control circuit to supply power to the first processing module, so that the first processing module receives the first signal transmitted by the first antenna, and the first working mode is realized.

[0068] 303、The processor controls the first antenna assembly to be in the off state and controls the second antenna assembly in the working state in response to a trigger operation performed on the second interactive control in the plurality of interactive controls, so as to realize a second working mode indicated by the second interactive control.

[0069] In the embodiment of the present application, the second interactive control refers to any interactive control in the plurality of interactive controls except the first interactive control. The second interactive control indicates the second working mode, and the second working mode is associated with the second antenna assembly. The trigger operation performed on the second interactive control can be a single click, a long press, a double click or the like operation performed on the second interactive control on the interactive interface, or a voice input operation, which is not limited in the present application.

[0070] Based on the foregoing introduction, the antenna assembly includes the processing module control circuit, the processing module and the antenna. Correspondingly, the first antenna assembly includes the first processing module control circuit, the first processing module and the first antenna. Illustratively, the processor controls the first antenna assembly to be in the working state, including: controlling the first processing module control circuit to supply power to the first processing module, so that the first processing module receives the first signal transmitted by the first antenna, and the first working mode is realized.

[0071] In some embodiments, the processor can control the display screen to display prompt information to remind the user whether to switch the current working mode in response to the trigger operation implemented on the second interaction control, so as to avoid the working mode from being switched due to user misoperation, and thus improve the human-computer interaction experience. Illustratively, this step 303 includes: the processor controls the display screen to display first prompt information on the interaction interface in response to the trigger operation implemented on the second interaction control, the first prompt information indicating that the working mode of the system is switched from the first working mode to the second working mode; in response to the trigger operation implemented on the first prompt information, the first antenna assembly is controlled to be in the off state and the second antenna assembly is controlled to be in the working state, so as to switch the working mode of the system from the first working mode to the second working mode. The first prompt information can be displayed in any position of the interaction interface in the form of a pop-up window, a floating window, a message reminder, etc., or can be displayed in the vicinity of the second interaction control, etc., which is not limited in the present application. For example, the first prompt information is "please confirm whether to switch XX mode to YY mode". In addition, the trigger operation implemented on the first prompt information can be single-click, long-press, double-click, etc., or can be a voice input operation, which is not limited in the present application. For example, the first prompt information includes a "confirm button" and a "cancel button", and in response to the click operation implemented on the "confirm button", the first antenna assembly is controlled to be in the off state and the second antenna assembly is controlled to be in the working state. It should be understood that the form of the first prompt information herein is only illustrative and does not limit the present application. In some scenarios, the first prompt information can also be broadcast in the form of voice broadcast through the vehicle loudspeaker to remind the user, so that when the user is in the driving state, the user does not need to pay attention to the interaction interface to confirm whether to switch the working mode of the system in time, ensuring the safety of vehicle driving and improving the human-computer interaction experience.

[0072] In some embodiments, the system can be configured to run in a plurality of working modes, and the processor can be configured to control the display to display prompt information to remind the user whether to run the other working mode in parallel with the current working mode in response to the trigger operation performed on the second interactive control, thereby improving the human-computer interaction experience. Illustratively, the processor controls the display to display second prompt information on the interactive interface in response to the trigger operation performed on the second interactive control, the second prompt information indicating that the working mode of the system is adjusted to be in parallel with the first working mode and the second working mode; and in response to the trigger operation performed on the second prompt information, the processor controls the second antenna assembly to be in the working state on the basis of controlling the first antenna assembly to be in the working state, so as to realize the parallel running of the first working mode and the second working mode. The second prompt information can be displayed in any position of the interactive interface in the form of a pop-up window, a floating window, a message reminder, etc., or can be displayed in the vicinity of the second interactive control, etc., and the present application does not make any limitation in this regard. For example, the second prompt information is "please confirm whether to run the XX mode in parallel with the YY mode". In addition, the trigger operation performed on the second prompt information can be a single click, a long press, a double click, etc., or can be a voice input operation, and the present application does not make any limitation in this regard. For example, the second prompt information includes a "confirm button" and a "cancel button", and in response to the click operation performed on the "confirm button", the processor controls the second antenna assembly to be in the working state on the basis of controlling the first antenna assembly to be in the working state. It should be understood that the form of the second prompt information herein is only illustrative and does not constitute a limitation on the present application. In some scenarios, the second prompt information can also be broadcast in the form of voice broadcast through the vehicle loudspeaker to remind the user, so that when the user is in the driving state, the user does not need to pay attention to the interactive interface to confirm whether the system working mode needs to be switched in time, thereby ensuring the safety of vehicle driving and improving the human-computer interaction experience.

[0073] In some embodiments, the processor implements the first working mode and the second working mode in parallel by the following method: the processor controls the first antenna assembly and the second antenna assembly to alternately be in the working state in different time periods, so as to implement the first working mode and the second working mode in parallel. For example, the processor controls the first antenna assembly to be in the working state in the first time period and the third time period, and controls the second antenna assembly to be in the working state in the second time period and the fourth time period, the second time period being between the first time period and the third time period, and the fourth time period being after the third time period. The granularity of the time periods corresponding to different antenna assemblies can be adjusted according to specific technical implementation and performance requirements, and generally, the granularity is in the range of milliseconds to seconds, for example, the first time period and the third time period of the first antenna assembly are set to 50 milliseconds, and the second time period and the fourth time period of the second antenna assembly are set to 80 milliseconds, which are not limited in the present application. It should be understood that, since the granularity of the different time periods provided by the present application is small, even if there is a missing signal between the first time period and the third time period of the antenna assembly, it will not affect the overall running performance of the system. By this way of alternately being in the working state in different time periods, the radiation interference between different antennas can be effectively avoided on the basis of implementing the parallel of multiple working modes of the system, the system is ensured to be in the minimum interference environment, and the system running performance and the human-computer interaction experience are improved.

[0074] In addition, in some embodiments, when the above-mentioned way of alternately being in the working state in different time periods is adopted, the processor can control the antenna assembly to simulate the signal corresponding to the missing time period, so as to ensure the continuity of the signal on the basis of avoiding the antenna interference. Illustratively, taking the example that the first antenna assembly is in the working state in the first time period and the third time period, and the second antenna assembly is in the working state in the second time period and the fourth time period, the first processing module in the first antenna assembly is configured to simulate the first signal transmitted by the first antenna in the second time period based on the first signal received in the first time period and the third time period, that is, the first processing module can simulate the signal of the missing time period based on the signals received in the two adjacent time periods. Since the granularity of the different time periods provided by the present application is small, the first processing module can simulate the signal close to the real level, so as to ensure the continuity of the signal. Similarly, the second processing module in the second antenna assembly is configured to simulate the second signal transmitted by the second antenna in the third time period based on the second signal received in the second time period and the fourth time period. It should be noted that the present application does not limit the way in which the processing module in the antenna assembly simulates the signal, for example, a trained artificial intelligence model can be used to simulate the signal of the missing time period to improve the accuracy of the simulated signal, or an arithmetic average method can be used to obtain the average value of the signals corresponding to the two adjacent time periods to obtain the simulated signal of the missing time period, so as to improve the processing efficiency and save the computing resources, etc., which are not limited in the present application.

[0075] The following refers to Figure 4 , in combination with the foregoing Figure 2 intelligent cockpit system shown in the system, the control method of the intelligent cockpit system shown in steps 301 to 303 is illustrated by taking the plurality of antenna components in the system as an example, including a radio antenna component, a Bluetooth antenna component, a WIFI antenna component, and a GPS antenna component. Illustratively, Figure 4 is another schematic diagram of an intelligent cockpit system provided by the embodiments of the present application, as shown in Figure 4 The method comprises:

[0076] The processor runs system applications and local applications, controls the display screen to display corresponding interactive interfaces, and performs software and hardware resource allocation and scheduling through an operating system (such as an Android system).

[0077] The display screen displays a plurality of interactive controls on the interactive interface, the interactive controls indicating the working mode of the system, and the working mode being associated with the antenna components, wherein the plurality of interactive controls include a radio switch button, a Bluetooth switch button, a WIFI switch button, and a GPS switch button, corresponding to the radio mode, the Bluetooth mode, the network mode, and the positioning mode of the system, respectively.

[0078] The processor determines that the system enters the radio mode in response to a trigger operation implemented on a first interactive control (such as a radio switch button) on the interactive interface, controls the first antenna component to be in a working state, that is, controls the radio module control circuit to supply power to the radio module, so that the radio module receives the radio signal transmitted by the radio antenna in the power supply state, and drives the peripheral circuit to output the audio signal after the radio module processes the radio signal, thereby driving the vehicle-mounted loudspeaker to output the sound of the radio station. Further, the processor determines that the system switches to other working modes in response to a trigger operation implemented on a second interactive control (that is, other buttons except the radio switch button) on the interactive interface, and controls the radio module control circuit to be powered off, thereby achieving power-off of the radio module, at which time the radio module does not receive the radio signal transmitted from the outside, thereby avoiding interference with the vehicle environment. At the same time, the antenna components corresponding to other working modes are controlled to be in a working state to achieve switching of the system working mode.

[0079] The above is an example of taking the first interactive control as the radio switch button, and the other switch buttons are the same. The following illustrates the other switch buttons.

[0080] Taking the first interactive control as a GPS switch button as an example, the processor determines that the system enters a positioning mode in response to a triggering operation implemented on the GPS switch button on the interactive interface, and controls the GPS antenna assembly to be in a working state, that is, controls the positioning module control circuit to supply power to the positioning module, so that the positioning module receives a positioning signal transmitted by the GPS antenna in a powered state. After the positioning module processes the positioning signal, the processed positioning signal is transmitted to the system application. When the user opens a map application based on the system application service, the function of navigation map positioning is realized, thereby providing accurate navigation positioning service for the user. Further, when the system switches to other working modes, the processor powers off the positioning module control circuit, thereby realizing power-off of the positioning module. At this time, the processor does not receive the GPS radio frequency signal transmitted from the outside, thereby avoiding interference with the vehicle environment. At the same time, the antenna assembly corresponding to other working modes is controlled to be in a working state to realize switching of the system working mode.

[0081] Taking the first interactive control as a Bluetooth switch button as an example, the processor determines that the system enters a Bluetooth mode in response to a triggering operation implemented on the Bluetooth switch button on the interactive interface, and controls the Bluetooth antenna assembly to be in a working state, that is, controls the Bluetooth module control circuit to supply power to the Bluetooth module, so that the Bluetooth module receives a Bluetooth signal transmitted by the Bluetooth antenna in a powered state. After the Bluetooth module processes the Bluetooth signal, related functions such as Bluetooth call and Bluetooth music are realized. Further, when the system switches to other working modes, the processor powers off the Bluetooth module control circuit, thereby realizing power-off of the Bluetooth module. At this time, the processor does not receive the Bluetooth signal transmitted from the outside, thereby avoiding interference with the vehicle environment. At the same time, the antenna assembly corresponding to other working modes is controlled to be in a working state to realize switching of the system working mode.

[0082] Taking the first interactive control as a network switch button as an example, the processor determines that the system enters a network mode in response to a triggering operation implemented on the network switch button on the interactive interface, and controls the WIFI antenna assembly to be in a working state, that is, controls the network module control circuit to supply power to the network module, so that the network module receives a WIFI signal transmitted by the WIFI antenna in a powered state. After the network module processes the WIFI signal, related functions such as network connection are realized. Further, when the system switches to other working modes, the processor powers off the network module control circuit, thereby realizing power-off of the network module. At this time, the processor does not receive the WIFI signal transmitted from the outside, thereby avoiding interference with the vehicle environment. At the same time, the antenna assembly corresponding to other working modes is controlled to be in a working state to realize switching of the system working mode.

[0083] It can be seen that, compared with the related art, the system realizes anti-interference processing of the antenna radio frequency signal in a manner of combination of software and hardware. The user selects the working mode of the system through the user interface displayed on the display screen, so that the system processor can determine the current working mode of the system according to the operation of the user, thereby allocating relevant software and hardware resources to the system and controlling whether to supply power to the corresponding control circuit. In this way, the antenna components in the corresponding working mode are ensured to be in the working state, the radiation of the radio frequency signal is reduced, the working mode antennas also reduce the radiation and interference, so as to ensure that the system is in the minimum interference environment, thereby improving the operation performance and human-computer interaction experience of the system.

[0084] In summary, in the control method of the intelligent cockpit system provided in the embodiment of the present application, the processor of the intelligent cockpit system controls the display screen to display a plurality of interactive controls on the interactive interface, so that the user can select the working mode of the system, and then controls the antenna components associated with the working mode selected by the user to be in the working state. When the user switches the working mode, the current antenna components are controlled to be in the closed state and the antenna components associated with the switched working mode are controlled to be in the working state, so as to realize the switching of the working mode. In this way, the radiation and interference between different antennas are avoided, the system is ensured to be in the minimum interference environment, and the operation performance and human-computer interaction experience of the system are improved.

[0085] Referring to Figure 5 The embodiment of the present application provides a control device of an intelligent cockpit system, which is configured to a processor of the intelligent cockpit system. The system further includes a display screen and a plurality of antenna components. The antenna components include a processing module control circuit, a processing module and an antenna. The device includes a display screen control unit 501 and an antenna component control unit 502.

[0086] The display screen control unit 501 is configured to control the display screen to display a plurality of interactive controls on an interactive interface. The interactive controls indicate the working mode of the system, and the working mode is associated with the antenna components.

[0087] The antenna component control unit 502 is configured to control a first antenna component in the plurality of antenna components to be in a working state in response to a trigger operation performed on a first interactive control in the plurality of interactive controls, so as to realize a first working mode indicated by the first interactive control. The processor controls a first processing module control circuit in the first antenna component to supply power to a first processing module in the first antenna component, so that the first processing module receives a first signal transmitted by a first antenna in the first antenna component.

[0088] The antenna assembly control unit 502 is further configured to, in response to a triggering operation performed on the second interactive control in the plurality of interactive controls, control the first antenna assembly to be in an off state and control a second antenna assembly in the plurality of antenna assemblies to be in an on state, so as to realize a second working mode indicated by the second interactive control, wherein the processor controls the first processing module control circuit to power off the first processing module, so that the first processing module does not receive the first signal, and controls the second processing module control circuit in the second antenna assembly to power on the second processing module in the second antenna assembly, so that the second processing module receives a second signal transmitted by a second antenna in the second antenna assembly.

[0089] In some embodiments, the plurality of antenna assemblies comprises any of the following items:

[0090] A radio antenna assembly for realizing a radio mode of the system.

[0091] A Bluetooth antenna assembly for realizing a Bluetooth mode of the system.

[0092] A WIFI antenna assembly for realizing a network mode of the system.

[0093] A GPS antenna assembly for realizing a positioning mode of the system.

[0094] A communication antenna assembly for realizing a communication mode of the system.

[0095] In some embodiments, the antenna assembly control unit 502 is configured to:

[0096] In response to a triggering operation performed on the second interactive control, control the display screen to display first prompt information on the interactive interface, the first prompt information indicating that the working mode of the system is switched from the first working mode to the second working mode.

[0097] In response to a triggering operation performed on the first prompt information, control the first antenna assembly to be in an off state and control the second antenna assembly to be in an on state, so as to switch the working mode of the system from the first working mode to the second working mode.

[0098] In some embodiments, the antenna assembly control unit 502 is configured to:

[0099] In response to a triggering operation performed on the second interactive control, control the display screen to display second prompt information on the interactive interface, the second prompt information indicating that the working mode of the system is adjusted to be parallel to the first working mode and the second working mode.

[0100] In response to a triggering operation performed on the second prompt information, on the basis of controlling the first antenna assembly to be in the working state, the second antenna assembly is controlled to be in the working state to realize the first working mode and the second working mode in parallel.

[0101] In some embodiments, the antenna assembly control unit 502 is configured to:

[0102] The first antenna assembly and the second antenna assembly are controlled to be in the working state alternately in different time periods to realize the first working mode and the second working mode in parallel.

[0103] In some embodiments, the antenna assembly control unit 502 is configured to:

[0104] The first antenna assembly is controlled to be in the working state in the first time period and the third time period, and the second antenna assembly is controlled to be in the working state in the second time period and the fourth time period, the second time period being between the first time period and the third time period, and the fourth time period being after the third time period.

[0105] The first processing module is configured to simulate the first signal transmitted by the first antenna in the second time period based on the first signal received in the first time period and the third time period, and the second processing module is configured to simulate the second signal transmitted by the second antenna in the third time period based on the second signal received in the second time period and the fourth time period.

[0106] In summary, in the control device of the intelligent cockpit system provided in the embodiments of the present application, the processor of the intelligent cockpit system controls the display screen to display a plurality of interactive controls on the interactive interface, so that the user can select the working mode of the system, and then controls the antenna assembly associated with the working mode to be in the working state according to the working mode selected by the user. When the user switches the working mode, the current antenna assembly is controlled to be in the off state and the antenna assembly associated with the working mode after switching is controlled to be in the working state, thereby realizing the switching of the working mode. In this way, the radiation and interference between different antennas are avoided, the system is ensured to be in a minimum interference environment, and the system operation performance and the human-computer interaction experience are improved.

[0107] It should be noted that the control device of the intelligent cockpit system provided in the above embodiments is only exemplified by the division of the above functional modules when controlling the intelligent cockpit system. In actual applications, the above functions can be completed by different functional modules according to needs, i.e., the internal structure is divided into different functional modules to complete all or part of the above described functions. In addition, the control device of the intelligent cockpit system provided in the above embodiments and the control method of the intelligent cockpit system belong to the same concept, and the specific implementation process is described in detail in the method embodiments, which will not be repeated here.

[0108] Reference Figure 6 The embodiments of the present application also provide an electronic device, Figure 6 is a structural schematic diagram of an electronic device provided by the embodiments of the present application. The electronic device 600 can have great differences due to different configurations or performances, and can include one or more processors (Central Processing Units, CPUs) 601 and one or more memories 602, wherein the memory 602 stores at least one piece of computer program, the at least one piece of computer program is loaded and executed by the processor 601 to realize the control method of the intelligent cockpit system provided by the above-mentioned method embodiments. Of course, the electronic device can also have a wired or wireless network interface, a keyboard, and an input and output interface and the like components, so as to perform input and output, and the electronic device can also include other components for realizing device functions, which are not described here.

[0109] The above-mentioned serial numbers of the embodiments of the present application are only for description, and do not represent the advantages and disadvantages of the embodiments.

[0110] Those skilled in the art can understand that all or part of the steps of the above-mentioned embodiments can be completed by hardware, or by program instructing relevant hardware to complete, and the program can be stored in a computer readable storage medium, and the above-mentioned storage medium can be a read-only memory, a magnetic disk or an optical disk.

[0111] The above-mentioned is only the preferred embodiment of the present application, and does not limit the present application, and any modification, equivalent replacement, improvement and the like within the spirit and principle of the present application should be included in the protection scope of the present application.

Claims

1. A control method for an intelligent cockpit system, characterized in that, A processor for use in a smart cockpit system, the system further including a display screen and multiple antenna assemblies, the antenna assemblies including a processing module control circuit, a processing module, and antennas, the method comprising: The system controls the display screen to show multiple interactive controls on the interactive interface. These interactive controls indicate the operating mode of the system, and the operating mode is associated with the antenna assembly. In response to a trigger operation performed on the first interactive control among the plurality of interactive controls, the first antenna component among the plurality of antenna components is controlled to be in a working state to realize the first working mode indicated by the first interactive control, wherein the control circuit of the first processing module in the first antenna component is controlled to supply power to the first processing module in the first antenna component so that the first processing module receives the first signal transmitted by the first antenna in the first antenna component. In response to a trigger operation performed on the second interactive control among the plurality of interactive controls, the display screen is controlled to display a first prompt message on the interactive interface, the first prompt message indicating that the working mode of the system is switched from the first working mode to the second working mode indicated by the second interactive control; In response to the triggering operation performed on the first prompt information, the first antenna assembly is controlled to be in a closed state and the second antenna assembly among the plurality of antenna assemblies is controlled to be in a working state, so as to switch the working mode of the system from the first working mode to the second working mode, wherein the first processing module control circuit is controlled to power off the first processing module so that the first processing module does not receive the first signal, and the second processing module control circuit in the second antenna assembly is controlled to power on the second processing module in the second antenna assembly so that the second processing module receives the second signal transmitted by the second antenna in the second antenna assembly; The plurality of antenna components include any of the following: A radio antenna assembly is used to implement the radio reception mode of the system; Bluetooth antenna assembly, used to implement the Bluetooth mode of the system; A WIFI antenna assembly is used to implement the network mode of the system; GPS antenna assembly, used to implement the positioning mode of the system; A communication antenna assembly for implementing the communication mode of the system.

2. The method according to claim 1, characterized in that, The method further includes: In response to a trigger operation performed on the second interactive control, the display screen is controlled to display a second prompt message on the interactive interface, the second prompt message indicating that the working mode of the system is adjusted to the parallel operation of the first working mode and the second working mode; In response to the triggering operation performed on the second prompt information, while controlling the first antenna component to be in the working state, the second antenna component is also controlled to be in the working state, so as to realize the first working mode and the second working mode in parallel.

3. The method according to claim 2, characterized in that, The step of controlling the second antenna component to be in a working state, based on controlling the first antenna component to be in a working state, so as to realize the parallel operation of the first working mode and the second working mode, includes: The first antenna component and the second antenna component are controlled to alternately operate in different time periods to achieve parallel operation of the first operating mode and the second operating mode.

4. The method according to claim 3, characterized in that, The method of controlling the first antenna component and the second antenna component to alternately operate in different time periods to achieve parallel operation of the first operating mode and the second operating mode includes: The first antenna assembly is controlled to be in a working state during a first time period and a third time period, and the second antenna assembly is controlled to be in a working state during a second time period and a fourth time period, wherein the second time period is between the first time period and the third time period, and the fourth time period is after the third time period. The first processing module is used to simulate the first signal transmitted by the first antenna in the second time period based on the first signal received in the first time period and the third time period, and the second processing module is used to simulate the second signal transmitted by the second antenna in the third time period based on the second signal received in the second time period and the fourth time period.

5. An intelligent cockpit system, characterized in that, The system includes a processor, a display screen, and multiple antenna assemblies. Each antenna assembly includes a processing module control circuit, a processing module, and an antenna. The processor is used for: The system controls the display screen to show multiple interactive controls on the interactive interface. These interactive controls indicate the operating mode of the system, and the operating mode is associated with the antenna assembly. In response to a trigger operation performed on the first interactive control among the plurality of interactive controls, the processor controls the first antenna component among the plurality of antenna components to be in a working state to realize the first working mode indicated by the first interactive control, wherein the processor controls the first processing module control circuit in the first antenna component to supply power to the first processing module in the first antenna component so that the first processing module receives the first signal transmitted by the first antenna in the first antenna component. In response to a trigger operation performed on the second interactive control among the plurality of interactive controls, the display screen is controlled to display a first prompt message on the interactive interface, the first prompt message indicating that the working mode of the system is switched from the first working mode to the second working mode indicated by the second interactive control; In response to the triggering operation performed on the first prompt information, the first antenna assembly is controlled to be in a closed state and the second antenna assembly among the plurality of antenna assemblies is controlled to be in a working state, so as to switch the working mode of the system from the first working mode to the second working mode. The processor controls the first processing module control circuit to power off the first processing module so that the first processing module does not receive the first signal, and controls the second processing module control circuit in the second antenna assembly to power on the second processing module in the second antenna assembly so that the second processing module receives the second signal transmitted by the second antenna in the second antenna assembly. The plurality of antenna components include any of the following: A radio antenna assembly is used to implement the radio reception mode of the system; Bluetooth antenna assembly, used to implement the Bluetooth mode of the system; A WIFI antenna assembly is used to implement the network mode of the system; GPS antenna assembly, used to implement the positioning mode of the system; A communication antenna assembly for implementing the communication mode of the system.

6. A control device for an intelligent cockpit system, characterized in that, A processor configured in a smart cockpit system, the system also including a display screen and multiple antenna assemblies, the antenna assemblies including a processing module control circuit, a processing module, and antennas; the device includes: A display control unit is used to control the display screen to display multiple interactive controls on an interactive interface, the interactive controls indicating the operating mode of the system, the operating mode being associated with the antenna assembly; An antenna assembly control unit is configured to control the first antenna assembly among the plurality of antenna assemblies to be in a working state in response to a trigger operation performed on the first interactive control among the plurality of interactive controls, so as to realize the first working mode indicated by the first interactive control, wherein the processor controls the first processing module control circuit in the first antenna assembly to supply power to the first processing module in the first antenna assembly, so that the first processing module receives the first signal transmitted by the first antenna in the first antenna assembly. The antenna assembly control unit is further configured to, in response to a trigger operation performed on a second interactive control among the plurality of interactive controls, control the display screen to display a first prompt message on the interactive interface, the first prompt message indicating that the operating mode of the system is switched from the first operating mode to the second operating mode indicated by the second interactive control; in response to a trigger operation performed on the first prompt message, control the first antenna assembly to be in a closed state and control the second antenna assembly among the plurality of antenna assemblies to be in a working state, so as to switch the operating mode of the system from the first operating mode to the second operating mode, wherein the processor controls the first processing module control circuit to power off the first processing module so that the first processing module does not receive the first signal, and controls the second processing module control circuit in the second antenna assembly to power on the second processing module in the second antenna assembly so that the second processing module receives the second signal transmitted by the second antenna in the second antenna assembly; The plurality of antenna components include any of the following: A radio antenna assembly is used to implement the radio reception mode of the system; Bluetooth antenna assembly, used to implement the Bluetooth mode of the system; A WIFI antenna assembly is used to implement the network mode of the system; GPS antenna assembly, used to implement the positioning mode of the system; A communication antenna assembly for implementing the communication mode of the system.

7. An electronic device, characterized in that, The electronic device includes a memory and a processor, wherein the memory stores at least one computer program, which is loaded and executed by the processor to implement the control method of the intelligent cockpit system as described in any one of claims 1-4.

8. A computer-readable storage medium, characterized in that, The computer-readable storage medium stores at least one computer program, which is loaded and executed by a processor to implement the control method of the intelligent cockpit system according to any one of claims 1-4.

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