Control method and device of display interface, storage medium and electronic equipment

Abstract

The application discloses a display interface control method, device, storage medium and electronic equipment. The display interface control method comprises the following steps: acquiring a current state parameter of an aircraft; calculating a standard display parameter according to the current state parameter of the aircraft; and adjusting a display parameter of the display interface to the standard display parameter. The application adjusts the display parameter of the display interface according to different flight stages by acquiring the current flight state of the aircraft. Since the data that the pilot needs to pay attention to on the display interface is different in different flight states, the readability of the data corresponding area is changed by adjusting the display parameter of the display interface, thereby improving the attention of the pilot to the corresponding area in the current flight state. In addition, the display interface seen by the pilot is related to the environmental parameter in the cockpit. The influence degree of the environmental parameter on the display parameter of the display interface is calculated, thereby further calibrating the standard display parameter to further achieve the display effect.

Description

Technical Field

[0001] This invention relates to the field of aircraft display interface technology, and in particular to a control method, device, storage medium, and electronic device for a display interface. Background Technology

[0002] During flight, the flight crew acquires and processes visual information through the cockpit display interface. When completing critical flight missions, the large amount of visual information can overload the crew's mental workload, potentially leading to flight accidents. A good flight display interface should be highly efficient, allowing pilots to quickly obtain the necessary information and make timely judgments and decisions. While color serves as an auxiliary code for information indication, the overlapping of foreground and background colors can also interfere with the crew's observation. Currently, aircraft designs use a single application of display colors throughout all phases of the flight, failing to meet the information capture needs of the flight crew in different scenarios. This results in lower flight performance and may even affect flight safety. For example, a small area of ​​high-brightness ground background color in the PFD can easily create a visual afterimage for the flight crew during long-duration flights, interfering with their observation of other display interfaces and the external field of vision. Summary of the Invention

[0003] This invention provides a control method, device, storage medium, and electronic device for a display interface that can effectively solve the problem that the same display interface is not conducive to pilots' observation of display interface data when the aircraft is in different flight stages.

[0004] According to one aspect of the present invention, a control method for a display interface is provided, the control method comprising: acquiring current state parameters of an aircraft; calculating standard display parameters based on the current state parameters of the aircraft; and adjusting the display parameters of the display interface to the standard display parameters.

[0005] Furthermore, obtaining the current state parameters of the aircraft includes: obtaining the current flight state of the aircraft and using the flight state as the state parameters.

[0006] Furthermore, the display interface includes a background interface and a data interface covering the background interface. The step of calculating the standard display parameters based on the current state parameters of the aircraft includes: determining a first parameter of the background interface based on the state parameters; and / or determining a second parameter of the data interface based on the state parameters; and using the first parameter, the second parameter, or the difference between the first parameter and the second parameter as the standard display parameters.

[0007] Furthermore, adjusting the display parameters of the display interface to the standard display parameters includes: adjusting the display parameters of the background interface to the first parameter.

[0008] Furthermore, adjusting the display parameters of the display interface to the standard display parameters further includes: adjusting the display parameters of the data interface covering the background interface to the second parameter.

[0009] Furthermore, adjusting the display parameters of the display interface to the standard display parameters further includes: adjusting the display parameters of the background interface to the first parameter and adjusting the display parameters of the data interface covering the background interface to the second parameter.

[0010] Furthermore, the aircraft includes a cockpit, the display interface is located in the cockpit, and the acquisition of the current status parameters of the aircraft includes: acquiring the current environmental parameters in the cockpit and using the environmental parameters as the status parameters.

[0011] Furthermore, the display interface includes a background interface and a data interface covering the background interface. The step of calculating the standard display parameters based on the current state parameters of the aircraft includes: calculating visual impact parameters based on the environmental parameters; determining a first parameter of the background interface based on the state parameters; and / or determining a second parameter of the data interface based on the state parameters; correcting the first parameter, the second parameter, or the difference between the first parameter and the second parameter respectively using the visual impact parameters, and using the corrected first parameter, the second parameter, or the difference between the first parameter and the second parameter as the standard display parameters.

[0012] Furthermore, adjusting the display parameters of the display interface to the standard display parameters includes: adjusting the display parameters of the background interface to the corrected first parameter.

[0013] Furthermore, adjusting the display parameters of the display interface to the standard display parameters further includes: adjusting the display parameters of the data interface covering the background interface to the corrected second parameters.

[0014] Furthermore, adjusting the display parameters of the display interface to the standard display parameters further includes: adjusting the display parameters of the background interface to the corrected first parameter and adjusting the display parameters of the data interface covering the background interface to the corrected second parameter.

[0015] According to another aspect of the present invention, a control device for a display interface is provided, the control device for the display interface comprising a status acquisition unit for acquiring current status parameters of an aircraft; a parameter calculation unit for calculating standard display parameters based on the current status parameters of the aircraft; and a display adjustment unit for adjusting the display parameters of the display interface to the standard display parameters.

[0016] According to another aspect of the present invention, a storage medium is provided, wherein computer instructions are stored on the storage medium, and when the computer instructions are executed by a processor, the control method for the display interface described in any embodiment of the present invention is implemented.

[0017] According to another aspect of the present invention, an electronic device is provided, including a processor and a memory, the processor being electrically connected to the memory, the memory being used to store instructions and data, and the processor being used to execute steps in the control method for a display interface according to any embodiment of the present invention.

[0018] The advantages of this invention lie in its ability to acquire the current flight status of the aircraft and adjust the display parameters of the display interface according to different flight stages. Since the data the pilot needs to pay attention to on the display interface differs depending on the flight state, adjusting the display parameters changes the readability of the corresponding data areas, thereby improving the pilot's attention to those areas in the current flight state. Furthermore, the display interface seen by the pilot is related to the environmental parameters within the cockpit. By calculating the degree of influence of environmental parameters on the display parameters, the standard display parameters are further calibrated to achieve a better display effect. Attached Figure Description

[0019] The technical solution and other beneficial effects of the present invention will become apparent from the following detailed description of specific embodiments of the invention, in conjunction with the accompanying drawings.

[0020] Figure 1 A flowchart illustrating the steps of a control method for a display interface provided in an embodiment of the present invention.

[0021] Figure 2 This is a schematic diagram of the structure of the control device for the display interface provided in an embodiment of the present invention.

[0022] Figure 3 This is a schematic diagram of the structure of an electronic device provided in an embodiment of the present invention. Detailed Implementation

[0023] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only a part of the embodiments of the present invention, and not all of them. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without creative effort are within the scope of protection of the present invention.

[0024] In the description of this invention, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "linking" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection, an electrical connection, or a connection that allows for communication; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components. Those skilled in the art can understand the specific meaning of the above terms in this invention according to the specific circumstances.

[0025] like Figure 1 The diagram shows a flowchart of the steps of a display interface control method provided in an embodiment of the present invention. The display interface control method includes:

[0026] Step S110: Obtain the current status parameters of the aircraft.

[0027] For example, the current flight state of the aircraft is obtained and used as the state parameter. The flight state includes stages such as aircraft takeoff, aircraft climb, aircraft descent, and aircraft approach. The different flight stages of the aircraft can be calculated from data obtained by various sensors inside the aircraft.

[0028] In some embodiments, flight phases can be divided according to aircraft altitude. The aircraft data transmission module obtains the aircraft altitude and transmits it to the integrated computer, which then determines the current flight phase.

[0029] In some embodiments, the aircraft includes a cockpit, and the display interface is disposed within the cockpit. Obtaining the current state parameters of the aircraft includes: obtaining the current environmental parameters within the cockpit, and using the environmental parameters as the state parameters. The environmental parameters include ambient brightness or ambient temperature within the cockpit, wherein the ambient brightness can be determined based on the current light intensity obtained by a light sensor, and the ambient temperature can be determined based on a temperature sensor disposed within the cockpit.

[0030] Step S120: Calculate the standard display parameters based on the current status parameters of the aircraft.

[0031] For example, the display interface includes a background interface and a data interface covering the background interface. A first parameter of the background interface is determined according to the state parameter. The background interface has the function of displaying different colors. The first parameter includes the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the background interface. By controlling the chromaticity value of each pixel unit, the background interface can display a corresponding color pattern combination.

[0032] In some embodiments, a second parameter of the data interface is determined based on the state parameters. The data interface is used to display different data information of the aircraft, such as the aircraft's attitude information and speed information. The second parameter includes the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the data interface. The data area is set above the background area, which is equivalent to the data area covering the background area, or the background area and the data area are set on the same layer without overlapping.

[0033] In some embodiments, the first parameter, the second parameter, or the difference between the first parameter and the second parameter are used as the standard display parameter. That is, the standard display parameter may also include both the first parameter and the second parameter, and the difference between the two is equivalent to the contrast ratio.

[0034] Step S130: Adjust the display parameters of the display interface to the standard display parameters.

[0035] For example, the display parameters of the background interface are adjusted to the first parameter. That is, this embodiment can change only the display pattern of the background area by adjusting the display parameters of the background interface. For example, the color or brightness of the background area can be changed. Furthermore, the area of ​​the background area can also be changed. For example, if the area of ​​the background area needs to be reduced, some pixel units within the background area can be adjusted to black, thereby changing the area of ​​the background area. Conversely, if the area of ​​the background area needs to be increased, some pixel units can be changed from black to other shades.

[0036] In some embodiments, the display parameters of the data interface covering the background interface are adjusted to the second parameter. That is, in this embodiment, only the color and brightness of the data interface may be changed.

[0037] In some embodiments, the display parameters of the background interface are adjusted to the first parameter, and the display parameters of the data interface covering the background interface are adjusted to the second parameter. Illustratively, in this embodiment, the color and brightness of the background area can be changed simultaneously with the color and brightness of the data area.

[0038] In other embodiments, when the state parameters include environmental parameters, calculating the standard display parameters based on the current state parameters of the aircraft includes calculating visual impact parameters based on the environmental parameters. The visual impact parameters can be understood as follows: when lights of the same brightness and color are viewed during the day and at night, the perceived color and brightness differ. Therefore, in a certain flight phase of the aircraft, the standard display parameters obtained through the above method theoretically allow the pilot to read data more easily visually. However, due to the influence of environmental parameters, the actual display effect does not achieve the target effect.

[0039] For example, during a certain phase of flight, to make it easier for the pilot to read data in a specific area of ​​the display, the brightness of the data interface and the background color are changed. Specifically, the data interface is made a brighter white, and the background is made black. This achieves a preset visual difference (e.g., contrast) between the background and data areas. However, when the ambient brightness is high, the originally calculated visual difference may not reach the actual visual difference perceived by the pilot, thus diminishing the readability improvement effect.

[0040] In some embodiments, a first parameter of the background interface is determined based on the state parameter.

[0041] In some embodiments, a second parameter of the data interface is determined based on the state parameter.

[0042] In some embodiments, after correcting the first parameter, the second parameter, or the difference between the first and second parameters using the visual impact parameter, the corrected first parameter, the second parameter, or the difference between the first and second parameters is used as the standard display parameter. As described above, through the visual impact parameter correction, for example, the data interface is changed to a brighter white, and the background interface is changed to black. This achieves a preset visual difference (e.g., contrast) between the background area and the data area. When the ambient brightness is high, the visual impact parameter reduces the visual difference, which can further increase the brightness of the data interface until the preset visual difference is reached.

[0043] In other embodiments, when the state parameters include environmental parameters, adjusting the display parameters of the display interface to the standard display parameters includes: adjusting the display parameters of the background interface to the corrected first parameter.

[0044] In other embodiments, when the state parameters include environmental parameters, adjusting the display parameters of the display interface to the standard display parameters further includes adjusting the display parameters of the data interface covering the background interface to the corrected second parameters.

[0045] In other embodiments, when the state parameters include environmental parameters, adjusting the display parameters of the display interface to the standard display parameters further includes: adjusting the display parameters of the background interface to the corrected first parameter and adjusting the display parameters of the data interface covering the background interface to the corrected second parameter.

[0046] To illustrate this, consider the aircraft during takeoff, climb, descent, and approach phases. During these phases, the display interface must provide the pilots with quick and accurate information. Therefore, the background area of ​​the display interface uses a concentrated area of ​​solid background color to clearly divide different categories of information based on their level of focus. In the center of the background is the attitude information area, which has the highest brightness, allowing the flight crew to maintain good concentration. The remaining areas containing basic aircraft information have a black background, making the numbers and symbols of other basic information stand out more, thus improving the flight crew's efficiency in obtaining specific aircraft performance information. In other words, during this phase, a specific area of ​​the display interface needs to be made easier to read.

[0047] When the aircraft is in cruise mode, the flight crew will spend a considerable amount of time looking at the display interface and switching between multiple displays to monitor and manage the aircraft. Therefore, the display interface must minimize adverse visual reactions for the flight crew during flight. To avoid excessive color contrast between the small, high-brightness area in the center and the surrounding black background, which could cause afterimages, the background color display area gradually expands across the entire display interface at a uniform speed as the climb phase ends and the flight enters cruise. This method uniformly displays the overall light intensity of the interface, helping to reduce adverse visual reactions for the flight crew during flight and thus improving their cognitive performance and comfort. In other words, during this phase, to reduce visual fatigue caused by prolonged pilot viewing of the display interface, the color and brightness of the entire display interface can be kept uniform, and display parameters are primarily calibrated and adjusted based on cockpit environmental parameters over a long period.

[0048] This invention acquires the aircraft's current flight status and adjusts the display parameters of the display interface according to different flight stages. Since the data the pilot needs to pay attention to on the display interface differs depending on the flight stage, adjusting the display parameters changes the readability of the corresponding data areas, thereby improving the pilot's attention to those areas in the current flight state. Furthermore, the display interface seen by the pilot is related to the environmental parameters within the cockpit. By calculating the degree of influence of environmental parameters on the display interface parameters, the standard display parameters are further calibrated to achieve a better display effect.

[0049] like Figure 2 The diagram shown is a schematic diagram of the control device for the display interface provided in an embodiment of the present invention. The control device includes: a status acquisition unit 10, a parameter calculation unit 20, and a display adjustment unit 30.

[0050] The state acquisition unit 10 is used to acquire the current state parameters of the aircraft. For example, it acquires the current flight state of the aircraft and uses this flight state as the state parameter. The flight state includes stages such as takeoff, climb, descent, and approach. These different flight stages can be calculated from data acquired by various sensors inside the aircraft.

[0051] In some embodiments, flight phases can be divided according to aircraft altitude. The aircraft data transmission module obtains the aircraft altitude and transmits it to the integrated computer, which then determines the current flight phase.

[0052] In some embodiments, the aircraft includes a cockpit, and the display interface is disposed within the cockpit. Obtaining the current state parameters of the aircraft includes: obtaining the current environmental parameters within the cockpit, and using the environmental parameters as the state parameters. The environmental parameters include ambient brightness or ambient temperature within the cockpit, wherein the ambient brightness can be determined based on the current light intensity obtained by a light sensor, and the ambient temperature can be determined based on a temperature sensor disposed within the cockpit.

[0053] The parameter calculation unit 20 is used to calculate standard display parameters based on the current state parameters of the aircraft. For example, the display interface includes a background interface and a data interface covering the background interface. A first parameter of the background interface is determined based on the state parameters. The background interface has the function of displaying different colors. The first parameter includes the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the background interface. By controlling the chromaticity value of each pixel unit, the background interface can display corresponding color pattern combinations.

[0054] In some embodiments, a second parameter of the data interface is determined based on the state parameters. The data interface is used to display different data information of the aircraft, such as the aircraft's attitude information and speed information. The second parameter includes the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the data interface. The data area is set above the background area, which is equivalent to the data area covering the background area, or the background area and the data area are set on the same layer without overlapping.

[0055] In some embodiments, the first parameter, the second parameter, or the difference between the first parameter and the second parameter are used as the standard display parameter. That is, the standard display parameter may also include both the first parameter and the second parameter, and the difference between the two is equivalent to the contrast ratio.

[0056] The display adjustment unit 30 is used to adjust the display parameters of the display interface to the standard display parameters. For example, the display parameters of the background interface are adjusted to the first parameter. That is, in this embodiment, by adjusting the display parameters of the background interface, only the display pattern of the background area can be changed. For example, the color or brightness of the background area can be changed. Furthermore, the area of ​​the background area can also be changed. For example, if the area of ​​the background area needs to be reduced, some pixel units within the background area can be adjusted to black, thereby changing the area of ​​the background area. Conversely, if the area of ​​the background area needs to be increased, some pixel units can be changed from black to other shades.

[0057] In some embodiments, the display parameters of the data interface covering the background interface are adjusted to the second parameter. That is, in this embodiment, only the color and brightness of the data interface can be changed.

[0058] In some embodiments, the display parameters of the background interface are adjusted to the first parameter, and the display parameters of the data interface covering the background interface are adjusted to the second parameter. Illustratively, in this embodiment, the color and brightness of the background area can be changed simultaneously with the color and brightness of the data area.

[0059] In other embodiments, when the state parameters include environmental parameters, calculating the standard display parameters based on the current state parameters of the aircraft includes calculating visual impact parameters based on the environmental parameters. The visual impact parameters can be understood as follows: when lights of the same brightness and color are viewed during the day and at night, the perceived color and brightness differ. Therefore, in a certain flight phase of the aircraft, the standard display parameters obtained through the above method theoretically allow the pilot to read data more easily visually. However, due to the influence of environmental parameters, the actual display effect does not achieve the target effect.

[0060] For example, during a certain phase of flight, to make it easier for the pilot to read data in a specific area of ​​the display, the brightness of the data interface and the background color are changed. This makes the data displayed in that area easier to read. Specifically, the data interface is changed to a brighter white, and the background is changed to black. This achieves a preset visual difference (e.g., contrast) between the background area and the data area. When the ambient brightness is high, the originally calculated visual difference may not reach the visual difference actually seen by the pilot, thus reducing the ease of reading.

[0061] In some embodiments, a first parameter of the background interface is determined based on the state parameter.

[0062] In some embodiments, a second parameter of the data interface is determined based on the state parameter.

[0063] In some embodiments, after correcting the first parameter, the second parameter, or the difference between the first and second parameters using the visual impact parameter, the corrected first parameter, the second parameter, or the difference between the first and second parameters is used as the standard display parameter. As described above, through the visual impact parameter correction, for example, the data interface is changed to a brighter white, and the background interface is changed to black. This achieves a preset visual difference (e.g., contrast) between the background area and the data area. When the ambient brightness is high, the visual impact parameter reduces the visual difference, which can further increase the brightness of the data interface until the preset visual difference is reached.

[0064] In other embodiments, when the state parameters include environmental parameters, adjusting the display parameters of the display interface to the standard display parameters includes: adjusting the display parameters of the background interface to the corrected first parameter.

[0065] In other embodiments, when the state parameters include environmental parameters, adjusting the display parameters of the display interface to the standard display parameters further includes adjusting the display parameters of the data interface covering the background interface to the corrected second parameters.

[0066] In other embodiments, when the state parameters include environmental parameters, adjusting the display parameters of the display interface to the standard display parameters further includes: adjusting the display parameters of the background interface to the corrected first parameter and adjusting the display parameters of the data interface covering the background interface to the corrected second parameter.

[0067] To illustrate this, consider the aircraft during takeoff, climb, descent, and approach phases. During these phases, the display interface must provide the pilots with quick and accurate information. Therefore, the background area of ​​the display interface uses a concentrated area of ​​solid background color to clearly divide different categories of information based on their level of focus. In the center of the background is the attitude information area, which has the highest brightness, allowing the flight crew to maintain good concentration. The remaining areas containing basic aircraft information have a black background, making the numbers and symbols of other basic information stand out more, thus improving the flight crew's efficiency in obtaining specific aircraft performance information. In other words, during this phase, a specific area of ​​the display interface needs to be made easier to read.

[0068] When the aircraft is in cruise mode, the flight crew will spend a considerable amount of time looking at the display interface and switching between multiple displays to monitor and manage the aircraft. Therefore, the display interface must minimize adverse visual reactions for the flight crew during flight. To avoid excessive color contrast between the small, high-brightness area in the center and the surrounding black background, which could cause afterimages, the background color display area gradually expands across the entire display interface at a uniform speed as the climb phase ends and the flight enters cruise. This method uniformly displays the overall light intensity of the interface, helping to reduce adverse visual reactions for the flight crew during flight and thus improving their cognitive performance and comfort. In other words, during this phase, to reduce visual fatigue caused by prolonged pilot viewing of the display interface, the color and brightness of the entire display interface can be kept uniform, and display parameters are primarily calibrated and adjusted based on cockpit environmental parameters over a long period.

[0069] This invention acquires the aircraft's current flight status and adjusts the display parameters of the display interface according to different flight stages. Since the data the pilot needs to pay attention to on the display interface differs depending on the flight stage, adjusting the display parameters changes the readability of the corresponding data areas, thereby improving the pilot's attention to those areas in the current flight state. Furthermore, the display interface seen by the pilot is related to the environmental parameters within the cockpit. By calculating the degree of influence of environmental parameters on the display interface parameters, the standard display parameters are further calibrated to achieve a better display effect.

[0070] like Figure 3 The diagram shown is a structural schematic of an electronic device provided in an embodiment of the present invention. This electronic device may include components such as a processor 401 with one or more processing cores, a memory 402 with one or more storage media, a power supply 403, and an input unit 404. Those skilled in the art will understand that... Figure 3 The device structure shown does not constitute a limitation on the device. Electronic devices may include more or fewer components than shown, or combine certain components, or have different component arrangements. Wherein:

[0071] The processor 401 is the control center of the device, connecting various parts of the device through various interfaces and lines. It executes software programs and / or unit modules stored in the memory 402, and calls data stored in the memory 402 to perform various functions and process data, thereby providing overall monitoring of the electronic device. Optionally, the processor 401 may include one or more processing cores; the processor 401 may be a Central Processing Unit (CPU), or other general-purpose processors, digital signal processors (DSPs), application-specific integrated circuits (ASICs), field-programmable gate arrays (FPGAs), or other programmable logic devices, discrete gate or transistor logic devices, discrete hardware components, etc. The general-purpose processor may be a microprocessor or any conventional processor. Preferably, the processor 401 may integrate an application processor and a modem processor, wherein the application processor mainly handles the operating system, user interface, and applications, and the modem processor mainly handles wireless communication. It is understood that the aforementioned modem processor may not be integrated into the processor 401.

[0072] The memory 402 can be used to store software programs and modules. The processor 401 executes various functional applications and data processing by running the software programs and modules stored in the memory 402. The memory 402 may mainly include a program storage area and a data storage area. The program storage area may store the operating system, applications required for at least one function, etc.; the data storage area may store data created according to the use of the electronic device, etc. In addition, the memory 402 may include high-speed random access memory, and may also include non-volatile memory, such as at least one disk storage device, flash memory device, or other volatile solid-state storage device. Accordingly, the memory 402 may also include a memory controller to provide the processor 401 with access to the memory 402.

[0073] The electronic device may also include a power supply 403 that supplies power to the various components. Preferably, the power supply 403 is logically connected to the processor 401 through a power management system, thereby enabling functions such as charging, discharging, and power consumption management through the power management system. The power supply 403 may also include one or more DC or AC power supplies, recharging systems, power fault detection circuits, power converters or inverters, power status indicators, and other arbitrary components.

[0074] The electronic device may also include an input unit 404 and an output unit 405. The input unit 404 can be used to receive input digital or character information and generate keyboard, mouse, joystick, optical or trackball signal inputs related to user settings and function control.

[0075] Although not shown, the electronic device may also include a display unit, etc., which will not be described in detail here. Specifically, in this application, the processor 401 in the electronic device loads the executable files corresponding to the processes of one or more application programs into the memory 402 according to the following instructions, and the processor 401 runs the application programs stored in the memory 402 to realize various functions, as follows:

[0076] Obtain the current status parameters of the aircraft;

[0077] Calculate the standard display parameters based on the current status parameters of the aircraft;

[0078] Adjust the display parameters of the display interface to the standard display parameters.

[0079] Those skilled in the art will understand that all or part of the steps in the various methods described above can be accomplished by instructions, or by controlling related hardware with instructions. These instructions can be stored in a storage medium and loaded and executed by the processor 401.

[0080] Therefore, embodiments of this application provide a storage medium, which may include: read-only memory (ROM), random access memory (RAM), a disk, or an optical disk, etc. Computer instructions are stored on the medium, and these instructions are loaded by a processor 401 to execute the steps in any of the display interface control methods provided in this application. For example, when the computer instructions are executed by the processor 401, they perform the following functions:

[0081] Obtain the current status parameters of the aircraft;

[0082] Calculate the standard display parameters based on the current status parameters of the aircraft;

[0083] Adjust the display parameters of the display interface to the standard display parameters.

[0084] The computer instructions stored in the storage medium can execute the steps of the control method for the display interface in any embodiment of this application. Therefore, the beneficial effects that the control method for the display interface in any embodiment of this application can achieve can be realized, as detailed in the preceding description, and will not be repeated here.

[0085] In summary, although the present invention has been disclosed above with reference to preferred embodiments, the above preferred embodiments are not intended to limit the present invention. Those skilled in the art can make various modifications and refinements without departing from the spirit and scope of the present invention. Therefore, the scope of protection of the present invention shall be determined by the scope defined in the claims.

Claims

1. A control method for a display interface, applicable to aircraft, characterized in that, The display interface includes a background interface and a data interface covering the background interface, and the control method includes: Obtain the current status parameters of the aircraft, including the flight status of the aircraft; The first parameter of the background interface is determined based on the state parameters, the first parameter including the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the background interface; and / or, The second parameter of the data interface is determined based on the state parameter. The second parameter includes the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the data interface. Use the first parameter, the second parameter, or the difference between the first parameter and the second parameter as the standard display parameter; Adjust the display parameters of the display interface to the standard display parameters.

2. The control method for the display interface according to claim 1, characterized in that, The acquisition of the current state parameters of the aircraft includes: Obtain the current flight status of the aircraft and use the flight status as the status parameter.

3. The control method for the display interface according to claim 1, characterized in that, Adjusting the display parameters of the display interface to the standard display parameters includes: Adjust the display parameters of the background interface to the first parameter.

4. The control method for the display interface according to claim 1, characterized in that, The step of adjusting the display parameters of the display interface to the standard display parameters further includes: Adjust the display parameters of the data interface covering the background interface to the second parameter.

5. The control method for the display interface according to claim 1, characterized in that, The step of adjusting the display parameters of the display interface to the standard display parameters further includes: Adjust the display parameters of the background interface to the first parameter and adjust the display parameters of the data interface covering the background interface to the second parameter.

6. The control method for the display interface according to claim 1, characterized in that, The aircraft includes a cockpit, and the display interface is located within the cockpit. Obtaining the current status parameters of the aircraft includes: Obtain the current environmental parameters inside the cockpit and use the environmental parameters as the state parameters.

7. The control method for the display interface according to claim 6, characterized in that, The control method further includes: Calculate the visual impact parameters based on the environmental parameters; Determine the first parameter of the background interface based on the state parameters; and / or, The second parameter of the data interface is determined based on the state parameter; After correcting the first parameter, the second parameter, or the difference between the first parameter and the second parameter respectively using the visual impact parameter, the corrected first parameter, the second parameter, or the difference between the first parameter and the second parameter is used as the standard display parameter.

8. The control method for the display interface according to claim 7, characterized in that, Adjusting the display parameters of the display interface to the standard display parameters includes: Adjust the display parameters of the background interface to the corrected first parameter.

9. The control method for the display interface according to claim 7, characterized in that, The step of adjusting the display parameters of the display interface to the standard display parameters further includes: Adjust the display parameters of the data interface covering the background interface to the corrected second parameter.

10. The control method for the display interface according to claim 7, characterized in that, The step of adjusting the display parameters of the display interface to the standard display parameters further includes: The display parameters of the background interface are adjusted to the corrected first parameter, and the display parameters of the data interface covering the background interface are adjusted to the corrected second parameter.

11. A control device with a display interface, suitable for aircraft, characterized in that, include: The status acquisition unit is used to acquire the current status parameters of the aircraft; A parameter calculation unit is used to determine a first parameter of the background interface based on the state parameters. The first parameter includes the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the background interface. And / or, determine a second parameter of the data interface based on the state parameter, the second parameter including the chromaticity values ​​of multiple pixel units and the brightness values ​​of different areas of the data interface; use the first parameter, the second parameter, or the difference between the first parameter and the second parameter as a standard display parameter; The display adjustment unit is used to adjust the display parameters of the display interface to the standard display parameters.

12. A storage medium, characterized in that, The storage medium stores computer instructions, which, when executed by a processor, implement the control method for the display interface as described in any one of claims 1-10.

13. An electronic device, characterized in that, It includes a processor and a memory, the processor being electrically connected to the memory, the memory being used to store instructions and data, and the processor being used to execute the steps of the control method for the display interface according to any one of claims 1 to 10.

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