阅读说明：本技术 一种飞行数据显示方法、装置、飞行器和可读存储介质 (Flight data display method and device, aircraft and readable storage medium ) 是由 赵德力 黄伟 李�杰 黄璐璐 林宗兵 于 2021-07-29 设计创作，主要内容包括：本发明实施例提供了一种飞行数据显示方法、装置、飞行器和可读存储介质,所述方法包括：获取所述飞行器当前的飞行姿态信息；所述飞行姿态信息包括偏航角信息、滚转角信息和俯仰角信息中的至少一种；根据所述飞行姿态信息控制在所述仪表盘显示图形化指示信息,所述图形化指示信息用于反映所述飞行器的飞行状态。根据本发明实施例,可以将飞行姿态数据以图形化的形式显示在仪表盘中。通过采用上述方法,可以直观显示飞行器的飞行姿态,提升飞行驾驶体验。(The embodiment of the invention provides a flight data display method, a flight data display device, an aircraft and a readable storage medium, wherein the method comprises the following steps: acquiring current flight attitude information of the aircraft; the flight attitude information comprises at least one of yaw angle information, roll angle information and pitch angle information; and controlling the instrument panel to display graphical indication information according to the flight attitude information, wherein the graphical indication information is used for reflecting the flight state of the aircraft. According to the embodiment of the invention, the flight attitude data can be displayed in the instrument panel in a graphical mode. By adopting the method, the flight attitude of the aircraft can be visually displayed, and the flight driving experience is improved.)

1. A method of displaying flight data for use with an aircraft having a dashboard, the method comprising:

acquiring current flight attitude information of the aircraft; the flight attitude information comprises at least one of yaw angle information, roll angle information and pitch angle information;

and controlling the instrument panel to display graphical indication information according to the flight attitude information, wherein the graphical indication information is used for reflecting the flight state of the aircraft.

2. The method according to claim 1, wherein the dashboard displays preset scales, indication marks and a virtual aircraft, and the controlling of displaying graphical indication information on the dashboard according to the flight attitude information comprises:

and controlling the preset scales and/or the indication marks to move relatively according to the flight attitude information so as to display the corresponding graphical indication information.

3. The method according to claim 2, wherein the preset scale comprises a preset yaw scale, the indication mark comprises a first indication mark, the preset yaw scale corresponds to a preset yaw angle in a one-to-one correspondence manner, the preset scale is controlled according to the flight attitude information, and/or the indication mark moves relatively, and the method comprises the following steps:

if the flight attitude information comprises the yaw angle information, determining a target yaw angle corresponding to the yaw angle information;

and controlling the preset yaw scale to rotate so that the first indication mark points to a target yaw scale corresponding to the target yaw angle.

4. The method of claim 2, wherein the predetermined scale comprises a predetermined roll scale, the indicator comprises a second indicator, the predetermined roll scale corresponds to a predetermined roll angle, the predetermined scale is controlled according to the flight attitude information, and/or the indicator moves relatively, comprising:

if the flight attitude information comprises the roll angle information, determining a target roll angle corresponding to the roll angle information;

and controlling the second indication mark to point to the target rolling scale corresponding to the target rolling angle.

5. The method according to claim 2, wherein the preset scale comprises a preset pitch scale, the indication mark comprises a third indication mark, the preset pitch scale corresponds to a preset pitch angle in a one-to-one manner, the preset scale is controlled according to the flight attitude information, and/or the indication mark moves relatively, and the method comprises the following steps:

if the flight attitude information comprises the pitch angle information, determining a target pitch angle corresponding to the pitch angle information;

and controlling the preset pitching scale to slide so that the third indication mark points to the target pitching scale corresponding to the target pitching angle.

6. The method according to claim 3, 4 or 5, wherein the preset yaw scale is an annular scale, and the preset yaw scale rotates along the center of the instrument panel; the preset rolling scales are arc scales; the preset pitching scale is a slidable scale, the preset pitching scale is located in the center of the instrument panel, and the virtual aircraft is displayed on the preset pitching scale in a stacked mode.

7. The method of claim 2, further comprising:

and adjusting the virtual flight state of the virtual aircraft according to the flight attitude information.

8. A flight data display device for use with an aircraft having an instrument panel, the device comprising:

the acquisition module is used for acquiring the current flight attitude information of the aircraft; the flight attitude information comprises at least one of yaw angle information, roll angle information and pitch angle information;

and the control module is used for controlling the instrument panel to display graphical indication information according to the flight attitude information, and the graphical indication information is used for reflecting the flight state of the aircraft.

9. An aircraft, characterized in that it comprises: processor, memory and computer program stored on the memory and capable of running on the processor, which computer program, when executed by the processor, carries out the steps of a flight data display method according to any one of claims 1 to 7.

10. A computer-readable storage medium, on which a computer program is stored which, when being executed by a processor, carries out the steps of a flight data display method according to any one of claims 1 to 7.

Technical Field

The present invention relates to the field of communications technologies, and in particular, to a flight data display method, a flight data display device, an aircraft, and a computer-readable storage medium.

Background

The flight attitude angle refers to an included angle between a machine body coordinate system and a ground inertia coordinate system and can be expressed by a rolling angle, a pitch angle and a yaw angle. The roll angle refers to an included angle between a symmetry plane of the aircraft and a vertical plane passing through a longitudinal axis of the aircraft body, and right roll is positive; the pitch angle is an included angle between a body shaft and a horizontal plane (horizontal plane), and the head-up is positive; the yaw angle refers to an included angle between the projection of the machine body axis on the horizontal plane and the ground axis, and the right yaw of the machine head is taken as the positive.

Data such as flight attitude and the like displayed on an aircraft, such as a flying automobile, are displayed in a digital form, and the display mode is not intuitive enough, so that the flight driving experience of a user is influenced.

Disclosure of Invention

In view of the above, embodiments of the present invention are proposed in order to provide a flight data display method and a corresponding flight data display device, an aircraft, and a computer-readable storage medium that overcome or at least partially address the above-mentioned problems.

The embodiment of the invention discloses a flight data display method, which is applied to an aircraft, wherein the aircraft is provided with an instrument panel, and the method comprises the following steps:

acquiring current flight attitude information of the aircraft; the flight attitude information comprises at least one of yaw angle information, roll angle information and pitch angle information;

and controlling the instrument panel to display graphical indication information according to the flight attitude information, wherein the graphical indication information is used for reflecting the flight state of the aircraft.

Optionally, the instrument panel displays preset scales, an indication mark and a virtual aircraft, and the control of displaying graphical indication information on the instrument panel according to the flight attitude information includes:

and controlling the preset scales and/or the indication marks to move relatively according to the flight attitude information so as to display the corresponding graphical indication information.

Optionally, the preset scale includes a preset yaw scale, the indication mark includes a first indication mark, the preset yaw scale corresponds to a preset yaw angle in a one-to-one manner, and the preset scale is controlled according to the flight attitude information, and/or the indication mark moves relatively, including:

if the flight attitude information comprises the yaw angle information, determining a target yaw angle corresponding to the yaw angle information;

and controlling the preset yaw scale to rotate so that the first indication mark points to a target yaw scale corresponding to the target yaw angle.

Optionally, preset the scale including presetting the roll scale, the pilot mark includes second pilot mark, preset the roll scale and preset roll angle one-to-one, according to flight attitude information control preset the scale, and/or, pilot mark relative motion includes:

if the flight attitude information comprises the roll angle information, determining a target roll angle corresponding to the roll angle information;

and controlling the second indication mark to point to the target rolling scale corresponding to the target rolling angle.

Optionally, the preset scale includes a preset pitch scale, the indication mark includes a third indication mark, the preset pitch scale corresponds to the preset pitch angle in a one-to-one manner, and the preset scale is controlled according to the flight attitude information, and/or the indication mark moves relatively, including:

if the flight attitude information comprises the pitch angle information, determining a target pitch angle corresponding to the pitch angle information;

and controlling the preset pitching scale to slide so that the third indication mark points to the target pitching scale corresponding to the target pitching angle.

Optionally, the preset yaw scale is an annular scale, and the preset yaw scale rotates along the center of the instrument panel; the preset rolling scales are arc scales; the preset pitching scale is a slidable scale, the preset pitching scale is located in the center of the instrument panel, and the virtual aircraft is displayed on the preset pitching scale in a stacked mode.

Optionally, the method further comprises:

and adjusting the virtual flight state of the virtual aircraft according to the flight attitude information.

The embodiment of the invention also discloses a flight data display device, which is applied to an aircraft, wherein the aircraft is provided with an instrument panel, and the device comprises:

the acquisition module is used for acquiring the current flight attitude information of the aircraft; the flight attitude information comprises at least one of yaw angle information, roll angle information and pitch angle information;

and the control module is used for controlling the instrument panel to display graphical indication information according to the flight attitude information, and the graphical indication information is used for reflecting the flight state of the aircraft.

Optionally, the dashboard displays preset scales, an indication mark and a virtual aircraft, and the control module includes:

and the control submodule is used for controlling the preset scales and/or the indication marks to move relatively according to the flight attitude information so as to display the corresponding graphical indication information.

Optionally, the preset scale includes a preset yaw scale, the indication mark includes a first indication mark, the preset yaw scale corresponds to the preset yaw angle one-to-one, and the control sub-module includes:

a first determining unit, configured to determine a target yaw angle corresponding to the yaw angle information if the flight attitude information includes the yaw angle information;

and the first control unit is used for controlling the preset yaw scale to rotate so that the first indication mark points to the target yaw scale corresponding to the target yaw angle.

Optionally, preset the scale including presetting the roll scale, the indicator includes second indicator, preset the roll scale and preset roll angle one-to-one, the control submodule includes:

the second determining unit is used for determining a target rolling angle corresponding to the rolling angle information if the flight attitude information comprises the rolling angle information;

and the second control unit is used for controlling the second indication mark to point to the target rolling scale corresponding to the target rolling angle.

Optionally, the preset scale includes a preset pitch scale, the indication mark includes a third indication mark, the preset pitch scale corresponds to the preset pitch angle one-to-one, and the control sub-module includes:

a third determining unit, configured to determine a target pitch angle corresponding to the pitch angle information if the flight attitude information includes the pitch angle information;

and the third control unit is used for controlling the preset pitch scales to slide so that the third indication mark points to the target pitch scale corresponding to the target pitch angle.

Optionally, the preset yaw scale is an annular scale, and the preset yaw scale rotates along the center of the instrument panel; the preset rolling scales are arc scales; the preset pitching scale is a slidable scale, the preset pitching scale is located in the center of the instrument panel, and the virtual aircraft is displayed on the preset pitching scale in a stacked mode.

Optionally, the method further comprises:

and the adjusting module is used for adjusting the virtual flight state of the virtual aircraft according to the flight attitude information.

The embodiment of the invention also discloses an aircraft, which comprises: a processor, a memory and a computer program stored on the memory and capable of running on the processor, the computer program, when executed by the processor, implementing the steps of a flight data display method as described above.

The embodiment of the invention also discloses a computer readable storage medium, wherein a computer program is stored on the computer readable storage medium, and when the computer program is executed by a processor, the steps of the flight data display method are realized.

The embodiment of the invention has the following advantages:

in an embodiment of the present invention, the flight attitude data may be displayed in a graphical form in the instrument panel. By adopting the method, the flight attitude of the aircraft can be visually displayed, and the flight driving experience is improved.

Drawings

FIG. 1 is a flow chart illustrating steps of a method for displaying flight data according to an embodiment of the present invention;

FIG. 2 is a flow chart illustrating steps of another method for displaying flight data according to an embodiment of the present invention;

FIG. 3 is a schematic illustration of an instrument panel of an aircraft according to an embodiment of the present invention;

FIG. 4 is a flow chart of a method of displaying flight data in accordance with an embodiment of the present invention;

fig. 5 is a block diagram of a flight data display device according to an embodiment of the present invention.

Detailed Description

In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below, and it is apparent that the described embodiments are only a part of the embodiments of the present invention, not all of them. All other embodiments that can be derived by one of ordinary skill in the art from the embodiments given herein are intended to be within the scope of the present invention.

Data such as flight attitude and the like displayed on an aircraft, such as a flying automobile, are displayed in a digital form, and the display mode is not intuitive enough, so that the flight driving experience of a user is influenced.

One of the core concepts of the embodiments of the present invention is that the flight attitude data may be displayed graphically in the dashboard. By adopting the method, the flight attitude of the aircraft can be visually displayed, and the flight driving experience is improved.

Referring to fig. 1, a flowchart illustrating steps of a flight data display method according to an embodiment of the present invention is shown, where the flight data display method is applied to an aircraft, where the aircraft has an instrument panel, and the method specifically includes the following steps:

step 101, obtaining current flight attitude information of the aircraft.

Wherein the flight attitude information includes at least one of yaw angle information, roll angle information, and pitch angle information.

In the embodiment of the invention, the flight attitude information can be acquired through a flight control system or a sensor system in the aircraft. In one example, after various sensors in the aircraft collect flight raw data, the flight raw data is transmitted to a flight control system, and flight attitude data is acquired from the flight control system of the aircraft. The aircraft may be a flying automobile, the aircraft having an instrument panel.

And step 102, controlling the instrument panel to display graphical indication information according to the flight attitude information.

The graphical indication information is used for reflecting the flight state of the aircraft.

In the embodiment of the invention, the flight attitude information of the aircraft can be displayed in the instrument panel in a graphical mode.

In a preferred example, before controlling the graphical indication information displayed on the instrument panel according to the flight attitude information, the method further comprises: and performing data conversion on the flight attitude information, and converting the flight attitude information into target flight attitude information meeting the display requirement of an instrument panel. The data conversion can be radian and angle conversion, and original flight attitude radian data is converted into flight attitude angle data.

In summary, in the embodiment of the present invention, the flight attitude data can be displayed in the instrument panel in a graphical form. By adopting the method, the flight attitude of the aircraft can be visually displayed, and the flight driving experience is improved.

Referring to fig. 2, a flowchart illustrating steps of another flight data display method according to an embodiment of the present invention is shown, where the method is applied to an aircraft, where the aircraft has an instrument panel, and the method specifically includes the following steps:

step 201, obtaining the current flight attitude information of the aircraft.

The flight attitude information comprises at least one of yaw angle information, roll angle information and pitch angle information; the aircraft is provided with a dashboard, and the dashboard displays preset scales, indication marks and the virtual aircraft. The preset scales correspond to the preset angles one by one; the indication mark is used for indicating preset scales; the virtual aircraft is a virtual aircraft model.

In the embodiment of the invention, the flight attitude information can be acquired through a flight control system or a sensor system in the aircraft.

Step 202, controlling the preset scales and/or the indication marks to move relatively according to the flight attitude information so as to display the corresponding graphical indication information.

In the embodiment of the invention, the relative movement refers to the relative position change between the preset scale and the indication mark. The preset scale can move, and the indication mark can also move. The preset scales can be controlled according to the flight attitude information, and/or the indication marks carry out relative movement, and then the flight attitude of the aircraft is determined according to the relative position relation.

In an optional example, the preset scales comprise preset yaw scales, the indication marks comprise first indication marks, and the preset yaw scales correspond to the preset yaw angles in a one-to-one mode.

For step 202, the following sub-steps may be performed:

and a substep S11, determining a target yaw angle corresponding to the yaw angle information if the flight attitude information includes the yaw angle information.

And a substep S12, controlling the preset yaw scale to rotate, so that the first indication mark points to a target yaw scale corresponding to the target yaw angle.

In the embodiment of the present invention, if the flight attitude information includes yaw angle information, a target yaw angle corresponding to the yaw angle information may be determined, and the preset yaw scale is controlled to rotate, so that the first indication identifier points to the target yaw scale corresponding to the target yaw angle. In this example, the preset yaw scale moves while the first indicator remains stationary.

In an optional example, the preset scale comprises a preset rolling scale, the indication mark comprises a second indication mark, and the preset rolling scale corresponds to the preset rolling angle in a one-to-one mode.

For step 202, the following sub-steps may be performed:

and a substep S21, determining a target roll angle corresponding to the roll angle information if the flight attitude information includes the roll angle information.

And a substep S22 of controlling the second indication mark to point to the target rolling scale corresponding to the target rolling angle.

In the embodiment of the present invention, if the flight attitude information includes roll angle information, a target roll angle corresponding to the roll angle information may be determined, and the second indication mark may be controlled to point at a target roll scale corresponding to the target roll angle. In this example, the preset roll scale remains stationary while the second indicator marks movement. Wherein the second indication identification can be a pointer.

In an optional example, the preset scales include a preset pitch scale, the indication marks include a third indication mark, and the preset pitch scale corresponds to the preset pitch angle in a one-to-one manner.

For step 203, the following sub-steps may be performed:

and a substep S31 of determining a target pitch angle corresponding to the pitch angle information if the flight attitude information includes the pitch angle information.

And a substep S32, controlling the preset pitch scale to slide, so that the third indication mark points to the target pitch scale corresponding to the target pitch angle.

In the embodiment of the invention, if the flight attitude information includes pitch angle information, a target pitch angle corresponding to the pitch angle information can be determined, and the preset pitch scale is controlled to slide, so that the third indication mark points to the target pitch scale corresponding to the target pitch angle. In this example, the preset pitch scale moves while the third indicator remains stationary.

Referring to fig. 3, a schematic diagram of an instrument panel of an aircraft according to an embodiment of the present invention is shown. In the figure, the scale on the outermost circle of the instrument panel is a preset yaw scale which is an annular scale and rotates along the center of the instrument panel; presetting the value range of yaw scales as 0-360 degrees;

the scale in the middle of the instrument panel in the figure is a preset pitching scale, the preset pitching scale is a slidable scale, the preset pitching scale is located in the center of the instrument panel, the virtual aircraft is superposed and displayed on the preset pitching scale, and the preset pitching scale is not more than 30 degrees (the part of the pitching scale in the figure is hidden and displayed);

the scale located between the preset yaw scale and the preset pitch scale in the figure is a preset rolling scale, the preset rolling scale is an arc scale, and the value range of the preset rolling scale is 0-30 degrees from the left to the right. The instrument panel in the figure also displays azimuth information. The graphical indication information displayed by the instrument panel changes along with the change of the flight attitude information of the aircraft.

In a preferred example, when the duration of the indication mark pointing to the preset maximum scale in the instrument panel exceeds the preset duration, the aircraft is judged to be in an out-of-control state. For example, for the roll scale in fig. 3, when the pointer points to the roll scale for 30 degrees longer than the preset duration, it can be determined that the aircraft is in an out-of-control state.

In a preferred example, the following steps may also be performed:

and adjusting the virtual flight state of the virtual aircraft according to the flight attitude information.

In the embodiment of the present invention, the virtual aircraft may further change the virtual flight state according to the flight attitude information, for example, the virtual aircraft may perform corresponding rotation or movement.

In order to enable those skilled in the art to better understand steps 201 to 202 of the embodiment of the present invention, the following description is made by way of an example:

referring to fig. 4, a flow chart of a flight data display method according to an embodiment of the invention is shown. The specific process is as follows:

1. acquiring flight original data of the aircraft through a sensor, transmitting the data to a flight control system, and acquiring flight attitude data including yaw data, roll data and pitch data from the flight control system of the manned aircraft;

2. and converting radian and angle of the acquired flight attitude data to acquire angle data.

3. And displaying the converted angle data on the instrument panel correspondingly. Wherein, the yaw angle change corresponds to the rotation of the yaw scale of the outermost circle in the instrument panel; the roll angle change corresponds to a roll pointer offset in the instrument panel; the pitch angle change corresponds to the slidable pitch scale of the dashboard sliding up or down.

In summary, in the embodiment of the present invention, the flight attitude data can be displayed in the instrument panel in a graphical form. By adopting the method, the flight attitude of the aircraft can be visually displayed, and the flight driving experience is improved.

It should be noted that, for simplicity of description, the method embodiments are described as a series of acts or combination of acts, but those skilled in the art will recognize that the present invention is not limited by the illustrated order of acts, as some steps may occur in other orders or concurrently in accordance with the embodiments of the present invention. Further, those skilled in the art will appreciate that the embodiments described in the specification are presently preferred and that no particular act is required to implement the invention.

Referring to fig. 5, a structural block diagram of a flight data display device according to an embodiment of the present invention is shown, where the flight data display device is applied to an aircraft, where the aircraft has an instrument panel, and specifically includes the following modules:

an obtaining module 501, configured to obtain current flight attitude information of the aircraft; the flight attitude information comprises at least one of yaw angle information, roll angle information and pitch angle information;

a control module 502, configured to control, according to the flight attitude information, to display graphical indication information on the instrument panel, where the graphical indication information is used to reflect a flight state of the aircraft.

In an embodiment of the present invention, the dashboard displays preset scales, an indication mark, and a virtual aircraft, and the control module includes:

and the control submodule is used for controlling the preset scales and/or the indication marks to move relatively according to the flight attitude information so as to display the corresponding graphical indication information.

In an embodiment of the present invention, the preset scales include a preset yaw scale, the indication mark includes a first indication mark, the preset yaw scale corresponds to a preset yaw angle in a one-to-one manner, and the control sub-module includes:

a first determining unit, configured to determine a target yaw angle corresponding to the yaw angle information if the flight attitude information includes the yaw angle information;

and the first control unit is used for controlling the preset yaw scale to rotate so that the first indication mark points to the target yaw scale corresponding to the target yaw angle.

In an embodiment of the present invention, the preset scale includes a preset rolling scale, the indication mark includes a second indication mark, the preset rolling scale corresponds to the preset rolling angle in a one-to-one manner, and the control sub-module includes:

the second determining unit is used for determining a target rolling angle corresponding to the rolling angle information if the flight attitude information comprises the rolling angle information;

and the second control unit is used for controlling the second indication mark to point to the target rolling scale corresponding to the target rolling angle.

In an embodiment of the present invention, the preset scale includes a preset pitch scale, the indication mark includes a third indication mark, the preset pitch scale corresponds to the preset pitch angle in a one-to-one manner, and the control sub-module includes:

a third determining unit, configured to determine a target pitch angle corresponding to the pitch angle information if the flight attitude information includes the pitch angle information;

and the third control unit is used for controlling the preset pitch scales to slide so that the third indication mark points to the target pitch scale corresponding to the target pitch angle.

In the embodiment of the invention, the preset yaw scale is an annular scale, and the preset yaw scale rotates along the center of the instrument panel; the preset rolling scales are arc scales; the preset pitching scale is a slidable scale, the preset pitching scale is located in the center of the instrument panel, and the virtual aircraft is displayed on the preset pitching scale in a stacked mode.

In the embodiment of the present invention, the method further includes:

and the adjusting module is used for adjusting the virtual flight state of the virtual aircraft according to the flight attitude information.

In summary, in the embodiment of the present invention, the flight attitude data can be displayed in the instrument panel in a graphical form. By adopting the method, the flight attitude of the aircraft can be visually displayed, and the flight driving experience is improved.

For the device embodiment, since it is basically similar to the method embodiment, the description is simple, and for the relevant points, refer to the partial description of the method embodiment.

An embodiment of the present invention further provides an aircraft, including: the flight data display method comprises a processor, a memory and a computer program which is stored in the memory and can run on the processor, wherein when the computer program is executed by the processor, each process of the flight data display method embodiment is realized, the same technical effect can be achieved, and in order to avoid repetition, the description is omitted here.

The embodiment of the present invention further provides a computer-readable storage medium, where a computer program is stored on the computer-readable storage medium, and when the computer program is executed by a processor, the computer program implements each process of the above-mentioned flight data display method embodiment, and can achieve the same technical effect, and in order to avoid repetition, the detailed description is omitted here.

The embodiments in the present specification are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other.

As will be appreciated by one skilled in the art, embodiments of the present invention may be provided as a method, apparatus, or computer program product. Accordingly, embodiments of the present invention may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, embodiments of the present invention may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.

Embodiments of the present invention are described with reference to flowchart illustrations and/or block diagrams of methods, terminal devices (systems), and computer program products according to embodiments of the invention. It will be understood that each flow and/or block of the flow diagrams and/or block diagrams, and combinations of flows and/or blocks in the flow diagrams and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing terminal to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing terminal, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.

These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing terminal to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.

These computer program instructions may also be loaded onto a computer or other programmable data processing terminal to cause a series of operational steps to be performed on the computer or other programmable terminal to produce a computer implemented process such that the instructions which execute on the computer or other programmable terminal provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.

While preferred embodiments of the present invention have been described, additional variations and modifications of these embodiments may occur to those skilled in the art once they learn of the basic inventive concepts. Therefore, it is intended that the appended claims be interpreted as including preferred embodiments and all such alterations and modifications as fall within the scope of the embodiments of the invention.

Finally, it should also be noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or terminal that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or terminal. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other like elements in a process, method, article, or terminal that comprises the element.

The present invention provides a flight data display method and a flight data display device, an aircraft and a computer readable storage medium, which are introduced in detail above, and the principle and the implementation of the present invention are explained herein by applying specific examples, and the description of the above examples is only used to help understanding the method and the core idea of the present invention; meanwhile, for a person skilled in the art, according to the idea of the present invention, there may be variations in the specific embodiments and the application scope, and in summary, the content of the present specification should not be construed as a limitation to the present invention.