WO2018227623A1

WO2018227623A1 - Control method, aircraft system, and display terminal

Info

Publication number: WO2018227623A1
Application number: PCT/CN2017/088793
Authority: WO
Inventors: 谢卓; 陈一
Original assignee: 深圳市大疆创新科技有限公司
Priority date: 2017-06-16
Filing date: 2017-06-16
Publication date: 2018-12-20
Also published as: CN108513647A

Abstract

A control method for an aircraft system (1000). The aircraft system (1000) comprises a display terminal (100) and an aircraft (200). The display terminal (100) communicates with the aircraft (200). The display terminal (100) comprises a primary display window (122) and a secondary display window (124). The aircraft (200) comprises a first data collection device (220) for collecting first data and a second data collection device (240) for collecting the second data. The control method for the aircraft system (1000) comprises the steps of: (S312) controlling a primary display window (122) to displays first data and an operation option related to a first data collection device (220), and controlling a secondary display window (124) to display second data; and; (S314) receiving a switching instruction, and controlling, according to the switching instruction, the primary display window (122) to display the second data and an operation option related to the second data collection device (240), and controlling the secondary display window (124) to display the first data. Also disclosed are an aircraft system (1000), a control method for the display terminal (100), and the display terminal (100).

Description

Control method, aircraft system and display terminal

Technical field

The present invention relates to the field of consumer electronics, and in particular, to a control method, an aircraft system, and a display terminal.

Background technique

In the related art, a display terminal (such as a mobile phone) displays a plurality of image frames obtained by a plurality of cameras of an aircraft in an inappropriate manner, resulting in an image display of only one of the cameras being temporarily enlarged and performing a simple operation.

Summary of the invention

Embodiments of the present invention provide a control method, an aircraft system, and a display terminal.

A control method provided by an embodiment of the present invention is for an aircraft system, the aircraft system includes a display terminal and an aircraft, the display terminal is in communication with the aircraft, and the display terminal includes a main display window and a secondary display window. The aircraft includes a first data collection device and a second data collection device; the control method includes:

Controlling the main display window to display first data collected by the first data collection device and operation options related to the first data collection device, and controlling the auxiliary display window to display the second data collection device The second data collected; and

Receiving a switching instruction, and controlling, according to the switching instruction, the main display window to display the second data collected by the second data collection device and an operation option related to the second data collection device, and controlling the The auxiliary display window displays the first data collected by the first data collection device.

An aircraft system provided by an embodiment of the present invention includes:

a display terminal, the display terminal including a main display window and a secondary display window;

An aircraft, the display terminal being in communication with the aircraft, the aircraft comprising a first data collection device and a second data acquisition device;

a processor for:

A control method provided by an embodiment of the present invention is used for a display terminal, where the display terminal communicates with an aircraft, The display terminal includes a main display window and a secondary display window, and the aircraft includes a first data collection device and a second data collection device; the control method includes:

The embodiment of the present invention provides a display terminal, the display terminal is in communication with an aircraft, and the aircraft includes a first data collection device and a second data collection device, and the display terminal includes:

Main display window;

Auxiliary display window; and

a processor for:

The control method, the aircraft system and the display terminal of the embodiment of the present invention use the main display window to display the data collected by one data acquisition device and the operation options related to the data collection device, and display the data collected by another data acquisition device by using the auxiliary display window. The data to be obtained, so that the main display window can display the function options related to the data collection device regardless of which data acquisition device displays the main display window, so that the plurality of data collection devices have the same status, enriching the user pair How multiple data acquisition devices operate.

The additional aspects and advantages of the embodiments of the present invention will be set forth in part in the description which follows.

DRAWINGS

The above and/or additional aspects and advantages of the present invention will become apparent and readily understood from

1 is a schematic flow chart of a control method according to an embodiment of the present invention;

2 is a schematic block diagram of an aircraft system according to an embodiment of the present invention;

3 is another schematic flowchart of a control method according to an embodiment of the present invention;

4 is a schematic flow chart of still another control method according to an embodiment of the present invention;

FIG. 5 is still another schematic flowchart of a control method according to an embodiment of the present invention; FIG.

6 is another schematic flowchart of a control method according to an embodiment of the present invention;

7 is a schematic plan view of a display terminal according to an embodiment of the present invention;

FIG. 8 is still another schematic flowchart of a control method according to an embodiment of the present invention; FIG.

FIG. 9 is still another schematic flowchart of a control method according to an embodiment of the present invention; FIG.

FIG. 10 is still another schematic flowchart of a control method according to an embodiment of the present invention; FIG.

11 is a schematic diagram of a connection between an aircraft system and a cloud in an embodiment of the present invention;

12 is another schematic plan view of a display terminal according to an embodiment of the present invention;

FIG. 13 is still another schematic flowchart of a control method according to an embodiment of the present invention; FIG.

14 is another schematic diagram of another module of an aircraft system according to an embodiment of the present invention;

FIG. 15 is still another schematic flowchart of a control method according to an embodiment of the present invention; FIG.

16 is another schematic flowchart of a control method according to an embodiment of the present invention;

Figure 17 is a block diagram showing still another module of the aircraft system of the embodiment of the present invention;

18 is a schematic diagram of the connection of an aircraft system and a computer readable storage medium in accordance with an embodiment of the present invention.

The main component symbol drawing description:

Aircraft system 1000, display terminal 100, display area 120, main display window 122, auxiliary display window 124, first auxiliary display window 1242, second auxiliary display window 1244, aircraft 200, first data collection device 220, second data collection The device 240, the third data collection device 260, the processor 300, the communication module 500, the memory 700, the cloud 8000, and the computer readable storage medium 9000.

detailed description

The embodiments of the present invention are described in detail below, and the examples of the embodiments are illustrated in the drawings, wherein the same or similar reference numerals indicate the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the drawings are intended to be illustrative of the invention and are not to be construed as limiting.

In the description of the present invention, it is to be understood that the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, features defining "first" or "second" may include one or more of the described features either explicitly or implicitly. In the description of the present invention, the meaning of "a plurality" is two or more unless specifically and specifically defined otherwise.

In the description of the present invention, it should be noted that the terms "installation", "connected", and "connected" are to be understood broadly, and may be fixed or detachable, for example, unless otherwise explicitly defined and defined. Connected, or connected in one piece; Therefore, they may be mechanically connected, or may be electrically connected or may communicate with each other; they may be directly connected or indirectly connected through an intermediate medium, and may be internal communication of two elements or an interaction relationship of two elements. For those skilled in the art, the specific meanings of the above terms in the present invention can be understood on a case-by-case basis.

The following disclosure provides many different embodiments or examples for implementing different structures of the present invention. In order to simplify the disclosure of the present invention, the components and arrangements of the specific examples are described below. Of course, they are merely examples and are not intended to limit the invention. In addition, the present invention may be repeated with reference to the numerals and/or reference numerals in the various examples, which are for the purpose of simplicity and clarity, and do not indicate the relationship between the various embodiments and/or arrangements discussed. Moreover, the present invention provides examples of various specific processes and materials, but one of ordinary skill in the art will recognize the use of other processes and/or the use of other materials.

Referring to FIG. 1 and FIG. 2 together, the control method of the embodiment of the present invention can be applied to the aircraft system 1000. The aircraft system 1000 includes a display terminal 100 and an aircraft 200 in communication with the aircraft 200. The display terminal 100 includes a main display window 122 and a secondary display window 124. The aircraft 200 includes a first data collection device 220 and a second data collection device 240; the control method includes:

Step S312: The control main display window 122 displays the first data collected by the first data collection device 220 and the operation options related to the first data collection device 220, and controls the auxiliary display window 124 to display the second data collection device 240. The second data to; and

Step S314: Receive a switching instruction, and control the main display window 122 to display the second data collected by the second data collection device 240 and the operation options related to the second data collection device 240 according to the switching instruction, and control the auxiliary display window 124 to display The first data collected by the first data collection device 220.

Referring again to FIG. 2, an aircraft system 1000 in accordance with an embodiment of the present invention includes a display terminal 100, an aircraft 200, and a processor 300. The display terminal 100 includes a main display window 122 and a secondary display window 124. Display terminal 100 is in communication with aircraft 200, which includes first data acquisition device 220 and second data acquisition device 240. The processor 300 is configured to:

The control main display window 122 displays the first data collected by the first data collection device 220 and the operation options associated with the first data collection device 220, and controls the auxiliary display window 124 to display the second data collection device 240. Two data; and

Receiving a switching instruction, and controlling the main display window 122 to display the second data collected by the second data collection device 240 and the operation options related to the second data collection device 240 according to the switching instruction, and controlling the auxiliary display window 124 to display the first data. The first data collected by the collection device 220.

That is, the control method of the embodiment of the present invention may be implemented by the aircraft system 1000 of the embodiment of the present invention, wherein steps S312 and S314 may be implemented by the processor 300 of the aircraft system 1000.

In some embodiments, the control method of the embodiment of the present invention may be implemented by the display terminal 100, that is, the processor 300 may be applied to the display terminal 100 of the embodiment of the present invention, or the display of the embodiment of the present invention. The terminal 100 includes a processor 300.

The control method, the aircraft system 1000 and the display terminal 100 of the embodiment of the present invention display the data collected by one data collection device and the operation options related to the data collection device by using the main display window 122, and display another data by using the auxiliary display window 124. Collecting the data collected by the device such that regardless of which data acquisition device the main display window 122 displays, the main display window 122 can display the functional options associated with the data acquisition device, thereby enabling the status of the plurality of data acquisition devices. The same, enriching the user's operation of multiple data acquisition devices.

In certain embodiments, aircraft 200 includes an unmanned aerial vehicle.

In some embodiments, the display terminal 100 includes at least one of a remote controller and/or a smart terminal (such as a mobile phone, a tablet computer, a notebook computer, etc.). Specifically, the display terminal 100 may be a remote controller with a display screen. It can also be a smart terminal, or a remote control and a smart terminal.

In some embodiments, the data collection device includes a camera and the data includes an image. In this way, the display terminal 100 can be used to properly display a plurality of images acquired by the plurality of cameras, and the main display window 122 can be controlled to display operation options related to the camera, thereby achieving the same status of the plurality of cameras. In one embodiment, the first data collection device 220 can be a camera with a zoom function, and the second data collection device 240 can be a camera with temperature measurement capability.

In some embodiments, the data collection device may also include other data acquisition devices such as a mapper, a pressure sensor, and a temperature sensor, which are not specifically limited herein.

In some embodiments, the operational options include parameters and functionality of the data acquisition device. In one embodiment, the first data acquisition device 220 has a zoom function camera, and the parameters include a series of parameters such as an operation mode (such as recording, photographing, etc.), white balance control, and flash control, and the function is to have a zoom function. Image acquisition device.

In some embodiments, the area of the primary display window 122 is greater than the area of the secondary display window 124. As such, the area that the main display window 122 can use for display can be made larger than the area that the auxiliary display window 124 can display, thereby allowing the main display window 122 to display operational options of the data collection device corresponding to more detailed data and data.

Referring to FIG. 3, in some embodiments, the switching instruction includes a preset switching instruction, and step S314 includes:

Step S3142: Receive a preset switching instruction, and control the main display window 122 to display the second data collected by the second data collection device 240 and the operation options related to the second data collection device 240 according to the preset switching instruction, and control the auxiliary The display window 124 displays the first data collected by the first data collection device 220.

Referring again to FIG. 2, in some embodiments, the switching instruction includes a preset switching instruction, and the processor 300 is configured to:

Receiving a preset switching instruction, and controlling the main display window 122 to display the second data collection device according to the preset switching instruction The second data collected by 240 and the operation options associated with the second data collection device 240 are controlled, and the auxiliary display window 124 is displayed to display the first data collected by the first data collection device 220.

That is, step S3142 can be implemented by the processor 300.

As such, the display terminal 100 can switch the display contents of the main display window 122 and the auxiliary display window 124 according to the preset switching instruction.

It can be understood that, in order to simplify the control of the user and realize the intelligence of the display terminal 100, the display terminal 100 or the aircraft system 1000 may store a preset switching instruction in advance, so that the display terminal 100 may perform the pre-operation without the user performing the operation. The switching instruction switches the display contents of the main display window 122 and the auxiliary display window 124. In one embodiment, the preset switching instruction switches the display content of the main display window 122 and the auxiliary display window 124 every 10 seconds, and the main display window 122 displays the first data and the first data collection in the first 10 seconds. The auxiliary display window corresponding to the device 220 displays the second data; in the second 10 seconds, the main display window 122 displays the second data and the operation option corresponding to the second data collection device 240, and the auxiliary display window displays the first data; In the third 10 seconds, the main display window 122 displays the first data and the operation option corresponding to the first data collection device 220, and the auxiliary display window displays the second data, so that the loop is repeated, so that the user can not operate the display terminal 100 or In the case of the aircraft system 1000, full control of the data collected by the plurality of data acquisition devices is achieved.

Referring to FIG. 4, in some embodiments, the switching instruction includes a user input instruction, and step S314 includes:

Step S3144: Receive a user input instruction, and control the main display window 122 to display the second data collected by the second data collection device 240 and the operation options related to the second data collection device 240 according to the user input instruction, and control the auxiliary display window. 124 displays the first data collected by the first data collection device 220.

Referring again to FIG. 2, in some embodiments, the switching instructions include user input instructions, and the processor 300 is configured to:

Receiving a user input instruction, and controlling the main display window 122 to display the second data collected by the second data collection device 240 and the operation options related to the second data collection device 240 according to the user input instruction, and controlling the auxiliary display window 124 to display the first The first data collected by the data collection device 220.

That is, step S3144 can be implemented by the processor 300.

In this way, the user can control the display terminal 100 to correctly display the data required by the user.

Specifically, the user can input the user input instruction through a physical button or a virtual button on the aircraft system 1000, such as a physical button or a virtual button on the display terminal 100. When the user wants to display the data of the auxiliary display window 124 and the operation option of the corresponding data collection device by using the main display window 122, the user can input a user input instruction, thereby causing the display terminal 100 to switch the main display window 122 and the auxiliary according to the user input instruction. The display content of the window 124 is displayed. In one embodiment, the main display window 122 displays the first data and the operation option corresponding to the first data collection device 220, and the auxiliary display window displays the second data, and the user operates to view the second data and the second data collection device 240. Option, the user input instruction can be input, so that the display terminal 100 receives the user input command and controls The master display window 122 displays the second data and the operation options corresponding to the second data collection device 240, and controls the secondary display window to display the first data.

Referring to FIG. 5, in some embodiments, the control method includes:

Step S316: Control the aircraft 200 to transmit the data displayed by the main display window 122 having the first data amount to the display terminal 100;

Step S318: The control aircraft 200 transmits to the display terminal 100 the data displayed by the auxiliary display window 124 having the second data amount, the first data amount being greater than the second data amount.

Referring again to FIG. 2, in some embodiments, processor 300 is configured to:

Controlling the aircraft 200 to transmit the data displayed by the main display window 122 having the first amount of data to the display terminal 100;

The control aircraft 200 transmits data displayed by the secondary display window 124 having the second amount of data to the display terminal 100, the first amount of data being greater than the second amount of data.

That is, steps S316 and S318 can be implemented by the processor 300.

In some embodiments, when steps S316 and S318 are implemented by display terminal 100, it can be converted to:

Step S317: receiving data displayed by the main display window 122 having the first data amount transmitted by the aircraft 200; and

Step S319: Receive data displayed by the auxiliary display window 124 having the second data amount transmitted by the aircraft 200, the first data amount being greater than the second data amount.

Steps S317 and S319 can be implemented by the processor 300.

In this way, the main display window 122 can be made to display the data collected by the data acquisition device more accurately and more efficiently.

It can be understood that when the aircraft 200 transmits data to the display terminal 100, due to technical and cost constraints, the general transmission bandwidth cannot cause a plurality of data to be transmitted in real time and completely, so that the display of the main display window 122 can be transmitted with the first data amount. The data is transmitted in the second data amount to display the data displayed by the auxiliary display window 124, and the first data amount is greater than the second data amount, so that the data displayed by the main display window 122 is more accurate and accurate, thereby ensuring multiple data. One of the data can be transmitted relatively completely.

Referring to FIG. 6 and FIG. 7 together, in some embodiments, the aircraft system 1000 includes a map, and the auxiliary display window 124 includes a first auxiliary display window 1242 and a second auxiliary display window 1244. The control method includes:

Step S322: controlling the main display window 122 to display the first data and the first auxiliary display window 1242 to display the second data, or controlling the main display window 122 to display the second data and the first auxiliary display window 1242 to display the first data;

Step S324: Control the second auxiliary display window 1244 to display the map.

Referring again to FIG. 7, in some embodiments, the aircraft system 1000 includes a map, the secondary display window 124 includes a first secondary display window 1242 and a second secondary display window 1244, and the processor 300 is configured to:

Controlling the main display window 122 to display the first data and the first auxiliary display window 1242 to display the second data, or controlling the main display window 122 to display the second data and the first auxiliary display window 1242 to display the first data;

The second secondary display window 1244 is controlled to display the map.

That is, steps S322 and S324 can be implemented by the processor 300.

As such, the map can be displayed using the second secondary display window 1244.

It can be understood that in order to accurately obtain the geographical position of the aircraft 200, the general aircraft system 1000 includes a map so that after the aircraft 200 is positioned, it can be displayed in the map, and the map can be displayed in one of the auxiliary display windows 124, such as the second secondary display. Window 1244.

In some embodiments, the second auxiliary display window 1244 displays a map, and since the first data and the second data can be switched between the main display window 122 and the first auxiliary display window 1242, the main display window 122 can be controlled to be displayed. The first data and the first auxiliary display window 1242 display the second data, and the main display window 122 displays the second data and the first auxiliary display window 1242 displays the first data, which is not specifically limited herein.

Referring to FIG. 8, in some embodiments, the aircraft system 1000 includes a map, and the auxiliary display window 124 includes a first auxiliary display window 1242 and a second auxiliary display window 1244. The control method includes:

Step S326: Control the main display window 122 to display the map; and

Step S328: Control the first secondary display window 1242 to display the first data and the second secondary display window 1244 to display the second data, or control the first secondary display window 1242 to display the second data and the second secondary display window 1244 to display the first data.

Controlling the main display window 122 to display a map; and

The first auxiliary display window 1242 is displayed to display the first data and the second auxiliary display window 1244 to display the second data, or to control the first secondary display window 1242 to display the second data and the second secondary display window 1244 to display the first data.

That is, steps S326 and S328 can be implemented by the processor 300.

As such, the main display window 122 can be controlled to display a map to make the map clearer and more specific.

It can be appreciated that the main display window 122 is generally larger than the secondary display window 124, so displaying the map using the main display window 122 can make the map clearer and more specific. In some embodiments, the map is switched to the second secondary display window 1244 at a previous moment of the main display window 122, and the main display window 122 at the previous moment displays the second data, then the switched main display window 122. The map is displayed. The first secondary display window 1242 displays the first data, and the second secondary display window 1244 displays the second data. In some embodiments, the map is switched to the second secondary display at a previous moment when the primary display window 122 is switched. The window 1244, and the main display window 122 at the previous moment displays the first data, then the switched main display window 122 displays the map, the first secondary display window 1242 displays the second data, and the second secondary display window 1244 displays the first data.

In some embodiments, the first secondary display window 1242 and the second secondary display window 1244 are located at different preset locations in the primary display window 122. As such, it is convenient for the first secondary display window 1242 and the second secondary display window 1244 to display different content.

It should be noted that, in some embodiments, in order to conform to the user's usage habits or ensure the appearance of the display interface, the map may be displayed in the preset position of the main display window 122 when the map is displayed in the auxiliary display window 124, that is, fixedly displayed. A secondary display window 1242 or a second secondary display window 1244. In one embodiment, the main display window 122 displays a map, the first secondary display window 1242 displays the first data, and the second secondary display window 1244 displays the second data, at which time the first data and the display position of the map are switched, due to the map display. When the auxiliary display window 124 is fixedly displayed in the preset position, such as the first auxiliary display window 1242, the position can be directly switched, that is, after the switching, the main display window 122 displays the first data, and the first auxiliary display window 1242 displays the map. The second secondary display window 1244 displays the second data. In another embodiment, the main display window 122 displays a map, the first secondary display window 1242 displays the first data, and the second secondary display window 1244 displays the second data, at which time the second data and the display position of the map are switched, due to the map When displayed in the auxiliary display window 124, it is fixedly displayed in a preset position, such as the first auxiliary display window 1242, so that the display position of the map and the second data can be switched first, and then the display position of the map and the first data is exchanged, that is, the main result is The display window 122 displays the second data, the first secondary display window 1242 displays the map, and the second secondary display window 1244 displays the second data.

Referring to FIG. 9, in some embodiments, the aircraft system 1000 includes a map, and the control method includes:

Step S332: Control the main display window 122 to display the map; and

Step S334: The control auxiliary display window 124 displays the first data or the second data.

Referring again to FIG. 2, in some embodiments, aircraft system 1000 includes a map and processor 300 is used to:

Controlling the main display window 122 to display a map; and

The control auxiliary display window 124 displays the first data or the second data.

That is, steps S332 and S334 can be implemented by the processor 300.

This makes it easy to switch the map to a preset location.

In some embodiments, the secondary display window 124 is located at a preset location in the primary display window 122. In this way, if the display position is switched when the main display window 122 displays the map, the map will be directly switched to the position of the auxiliary display window 124, that is, the map will be directly switched to the preset position. In one embodiment, if the main display window 122 displays the first data before the map is switched to the main display window 122, the main display window 122 displays the map after the switch, and the auxiliary display window 124 displays the first data. In another embodiment, before the map is switched to the main display window 122, if the main display window 122 displays the second data, the main display window 122 displays the map after the switch, and the secondary display window 124 displays the second data.

In some embodiments, the map is preset in the aircraft system 1000.

In this way, the map can be obtained quickly.

Specifically, the map may be preset in the display terminal 100. When the user selects the map display, the display terminal 100 directly uses the preset map, so that the map can be quickly displayed, thereby facilitating the user to view the detailed position of the aircraft 200.

Referring to FIG. 10 and FIG. 11 together, in some embodiments, the aircraft system 1000 includes a communication module 500 that communicates with the cloud 8000. The control method includes:

Step S336: The communication module 500 is controlled to communicate with the cloud 8000 to obtain a map.

Referring again to FIG. 11, in some embodiments, the aircraft system 1000 includes a communication module 500 in communication with the cloud 8000, the processor 300 for:

The control communication module 500 communicates with the cloud 8000 to obtain a map.

That is, step S336 can be implemented by the processor 300.

In this way, the map can be obtained through the cloud 8000.

In some embodiments, display terminal 100 includes a communication module 500. Since the map requires a certain storage space, and generally requires a relatively large storage space, in order to reduce the storage space occupied by the map, the communication module 500 can be used to directly obtain the map from the cloud 8000, so that the entire map does not need to be stored in the display terminal 100 at all times. Or in the aircraft system 1000. In addition, the communication module 500 can be used to update the map in real time, thereby enabling the map to more accurately show changes in terrain or architecture, etc. in real life.

Referring to FIG. 12, in some embodiments, display terminal 100 includes a single display area 120 that includes a primary display window 122 and a secondary display window 124.

As such, the data of the plurality of data collection devices can be reasonably displayed using a single display area 120.

It can be understood that when the display terminal 100 has only a single display area 120, the data display of the plurality of data collection devices is relatively inconvenient, so the display area 120 can be divided into a main display window 122 and a secondary display window 124, and the data is displayed by using the main display window. Operation options related to the data acquisition device, using the secondary display window to display data.

Referring to FIG. 13 and FIG. 14, the aircraft 200 includes a third data collection device 260, and the control method includes:

Step S338: Control the main display window 122 to display the first data; and

Step S342: The control auxiliary display window 124 displays the third data and/or the second data collected by the third data collection device 260.

Referring again to FIG. 14, in some embodiments, aircraft 200 includes a third data collection device 260 for:

Controlling the main display window 122 to display the first data; and

The control auxiliary display window 124 displays the third data and/or the second data collected by the third data collection device 260.

That is, steps S338 and S342 can be implemented by the processor 300.

In this way, the first data, the second data, and the first data can be reasonably displayed by using the main display window 122 and the auxiliary display window 124. Three data.

Specifically, when the first display window 122 displays the first data, the aircraft 200 may transmit only the data of the two data collection devices to the display terminal 100 due to the transmission bandwidth limitation of the aircraft 200 and the display terminal 100, that is, the display terminal 100 includes a single auxiliary. The display window 124, the auxiliary display window 124 can be used to display the second data or the third data; if the aircraft simultaneously transmits the data of the three data collection devices to the display terminal 100, the display terminal 100 includes two auxiliary display windows 124, two The secondary display window 124 can be used to display the second data and the third data simultaneously.

Referring to FIG. 15, in some embodiments, the aircraft 200 includes a third data collection device 260, and the control method includes:

Step S344: Control the main display window 122 to display the second data; and

Step S346: The control auxiliary display window 124 displays the third data and/or the first data collected by the third data collection device 260.

Controlling the main display window 122 to display the second data; and

The control auxiliary display window 124 displays the third data and/or the first data collected by the third data collection device 260.

That is, steps S344 and S346 can be implemented by the processor 300.

As such, the first data, the second data, and the third data can be reasonably displayed using the main display window 122 and the auxiliary display window 124.

Specifically, when the second display data is displayed in the main display window 122, the aircraft 200 may transmit only the data of the two data collection devices to the display terminal 100 due to the transmission bandwidth limitation of the aircraft 200 and the display terminal 100, and the display terminal 100 includes a single auxiliary display. The window 124, the auxiliary display window 124 can be used to display the first data or the third data; if the aircraft simultaneously transmits the data of the three data collection devices to the display terminal 100, the display terminal 100 includes two auxiliary display windows 124, and two auxiliary displays. Window 124 can be used to display the first data and the third data simultaneously.

Referring to FIG. 16, in some embodiments, the aircraft 200 includes a third data collection device 260, and the control method includes:

Step S348: Control the main display window 122 to display the third data collected by the third data collection device 260; and

Step S352: The control auxiliary display window 124 displays the first data and/or the second data.

Controlling the main display window 122 to display the third data collected by the third data collection device 260; and

The control auxiliary display window 124 displays the first data and/or the second data.

That is, steps S348 and S352 can be implemented by the processor 300.

Specifically, when the third display data is displayed in the main display window 122, due to the transmission bandwidth limitation of the aircraft 200 and the display terminal 100, the aircraft 200 may transmit only data of two data collection devices to the display terminal 100, and the display terminal 100 includes a single auxiliary display. The window 124, the auxiliary display window 124 may be used to display the first data or the second data; if the aircraft simultaneously transmits the data of the three data collection devices to the display terminal 100, the display terminal 100 includes two auxiliary display windows 124, and two auxiliary displays. Window 124 can be used to display both the first data and the second data.

Referring to Figure 17, an aircraft system 1000 in accordance with an embodiment of the present invention includes a display terminal 100, an aircraft 200, one or more processors 300, a memory 700, and one or more programs. One or more of the programs are stored in memory 700 and are configured to be executed by one or more processors 300 for executing instructions of the control method of any of the above-described embodiments of the present invention.

As an example, a program can be used to execute instructions for the following control methods:

Referring to Figure 18, a computer readable storage medium 9000, in accordance with an embodiment of the present invention, includes a computer program for use with aircraft system 1000 that can be executed by processor 300 to perform the control method of any of the above-described embodiments of the present invention.

For one example, a computer program can be executed by processor 300 to perform the following control methods:

It should be noted that the computer readable storage medium 9000 may be a storage medium built in the aircraft system 1000, such as the display terminal 100, or may be a storage medium that is pluggably inserted in the aircraft system 1000, such as the display terminal 100.

In the description of the present specification, reference is made to the terms "one embodiment", "some embodiments", "illustrative implementation" A description of a formula, a "example", "a specific example", or "some examples" and the like means that a particular feature, structure, material or characteristic described in connection with the described embodiments or examples is included in at least one embodiment or example of the invention. In the present specification, the schematic representation of the above terms does not necessarily mean the same embodiment or example. Moreover, the specific features, structures, materials or features described may be in any one or more embodiments or examples. Combine in a suitable way.

Any process or method description in the flowcharts or otherwise described herein may be understood to represent a module, segment or portion of code that includes one or more executable instructions for performing the steps of a particular logical function or process. And the scope of the preferred embodiments of the invention includes additional implementations, which may be performed in a substantially simultaneous manner or in the reverse order, depending on the functions involved, in the order shown or discussed, which should It will be understood by those skilled in the art to which the embodiments of the present invention pertain.

The logic and/or steps represented in the flowchart or otherwise described herein, for example, may be considered as an ordered list of executable instructions for performing logical functions, and may be embodied in any computer readable medium, Used in conjunction with, or in conjunction with, an instruction execution system, apparatus, or device (eg, a computer-based system, a system including a processor, or other system that can fetch instructions and execute instructions from an instruction execution system, apparatus, or device) Or use with equipment. For the purposes of this specification, a "computer-readable medium" can be any apparatus that can contain, store, communicate, propagate, or transport a program for use in an instruction execution system, apparatus, or device, or in conjunction with the instruction execution system, apparatus, or device. More specific examples (non-exhaustive list) of computer readable media include the following: electrical connections (electronic devices) having one or more wires, portable computer disk cartridges (magnetic devices), random access memory (RAM), Read only memory (ROM), erasable editable read only memory (EPROM or flash memory), fiber optic devices, and portable compact disk read only memory (CDROM). In addition, the computer readable medium may even be a paper or other suitable medium on which the program can be printed, as it may be optically scanned, for example by paper or other medium, followed by editing, interpretation or, if appropriate, other suitable The method is processed to obtain the program electronically and then stored in computer memory.

It should be understood that portions of the invention may be implemented in hardware, software, firmware or a combination thereof. In the above-described embodiments, multiple steps or methods may be performed by software or firmware stored in a memory and executed by a suitable instruction execution system. For example, if executed in hardware, as in another embodiment, it can be performed by any one of the following techniques or combinations thereof known in the art: having logic gates for performing logic functions on data signals Discrete logic circuits, application specific integrated circuits with suitable combinational logic gates, programmable gate arrays (PGAs), field programmable gate arrays (FPGAs), etc.

Those skilled in the art can understand that all or part of the steps carried in carrying out the above implementation method can be completed by a program to instruct related hardware, and the program can be stored in a computer readable storage medium, and the program is executed. Including one or a combination of the steps of the method embodiments.

In addition, each functional unit in each embodiment of the present invention may be integrated into one processing module, or each unit may exist physically separately, or two or more units may be integrated into one module. The above integrated module is It can be executed in the form of hardware or in the form of a software function module. The integrated modules, if executed in the form of software functional modules and sold or used as separate products, may also be stored in a computer readable storage medium.

The above mentioned storage medium may be a read only memory, a magnetic disk or an optical disk or the like. Although the embodiments of the present invention have been shown and described, it is understood that the above-described embodiments are illustrative and are not to be construed as limiting the scope of the invention. The embodiments are subject to variations, modifications, substitutions and variations.

Claims

A control method for an aircraft system, characterized in that the aircraft system comprises a display terminal and an aircraft, the display terminal is in communication with the aircraft, the display terminal comprising a main display window and a secondary display window, the aircraft The first data collection device and the second data collection device are included; the control method includes:

Controlling the main display window to display first data collected by the first data collection device and operation options related to the first data collection device, and controlling the auxiliary display window to display the second data collection device The second data collected; and

Receiving a switching instruction, and controlling, according to the switching instruction, the main display window to display the second data collected by the second data collection device and an operation option related to the second data collection device, and controlling the The auxiliary display window displays the first data collected by the first data collection device.
The control method according to claim 1, wherein the switching instruction comprises a preset switching instruction, the receiving switching instruction, and controlling the main display window to display the second data collecting device according to the switching instruction The second data collected and the operation option associated with the second data collection device, and controlling the auxiliary display window to display the first data collected by the first data collection device includes:

Receiving the preset switching instruction, and controlling, according to the preset switching instruction, the main display window to display the second data collected by the second data collection device and related to the second data collection device Operating the option, and controlling the auxiliary display window to display the first data collected by the first data collection device.
The control method according to claim 1, wherein the switching instruction comprises a user input instruction, the receiving switching instruction, and controlling the main display window to display the second data collection device according to the switching instruction The collecting the second data and the operation option associated with the second data collection device, and controlling the auxiliary display window to display the first data collected by the first data collection device includes:

Receiving the user input instruction, and controlling, according to the user input instruction, the main display window to display the second data collected by the second data collection device and operation options related to the second data collection device And controlling the auxiliary display window to display the first data collected by the first data collection device.
The control method according to claim 1, wherein said control method comprises:

Controlling the aircraft to transmit data displayed by the main display window having a first amount of data to the display terminal; and

Controlling the aircraft to transmit data displayed by the secondary display window having a second amount of data to the display terminal, the first amount of data being greater than the second amount of data.
The control method of claim 1 wherein said operational options include parameters and functions of the data collection device.
The control method according to claim 1, wherein said aircraft system includes a map, said auxiliary display The display window includes a first auxiliary display window and a second auxiliary display window, and the control method includes:

Controlling the main display window to display the first data and the first auxiliary display window to display the second data, or controlling the main display window to display the second data and the first auxiliary display window display The first data; and

Controlling the second secondary display window displays the map.
The control method according to claim 1, wherein the aircraft system comprises a map, the auxiliary display window comprises a first auxiliary display window and a second auxiliary display window, and the control method comprises:

Controlling the main display window to display the map; and

Controlling the first secondary display window to display the first data and the second secondary display window to display the second data, or controlling the first secondary display window to display the second data and the second secondary The display window displays the first data.
The control method according to claim 6 or 7, wherein the first secondary display window and the second secondary display window are located at different preset positions in the main display window.
The control method according to claim 1, wherein said aircraft system comprises a map, and said control method comprises:

Controlling the main display window to display the map; and

Controlling the secondary display window to display the first data or the second data.
The control method according to claim 9, wherein the auxiliary display window is located at a preset position in the main display window.
The control method according to claim 6, 7 or 9, wherein the map is preset in the aircraft system.
The control method according to claim 6, 7 or 9, wherein the aircraft system comprises a communication module that communicates with the cloud, and the control method comprises:

The communication module is controlled to communicate with the cloud to obtain the map.
The control method according to claim 1, wherein said display terminal comprises a single display area, and said display area includes said main display window and said auxiliary display window.
The control method according to claim 1, wherein an area of the main display window is larger than an area of the auxiliary display window.
The control method according to claim 1, wherein the aircraft comprises a third data collection device, and the control method comprises:

Controlling the main display window to display the first data; and

Controlling the auxiliary display window to display third data and/or second data collected by the third data collection device.
The control method according to claim 1, wherein said aircraft comprises a third data collection device, The control method includes:

Controlling the main display window to display the second data; and

Controlling the auxiliary display window to display third data and/or first data collected by the third data collection device.
The control method according to claim 1, wherein the aircraft comprises a third data collection device, and the control method comprises:

Controlling the main display window to display third data collected by the third data collection device; and

Controlling the secondary display window to display the first data and/or the second data.
The control method of claim 1 wherein said data acquisition device comprises a camera and said data comprises an image.
An aircraft system, comprising:

a display terminal, the display terminal including a main display window and a secondary display window;

An aircraft, the display terminal being in communication with the aircraft, the aircraft comprising a first data collection device and a second data acquisition device;

a processor for:

Controlling the main display window to display first data collected by the first data collection device and operation options related to the first data collection device, and controlling the auxiliary display window to display the second data collection device The second data collected; and

Receiving a switching instruction, and controlling, according to the switching instruction, the main display window to display the second data collected by the second data collection device and an operation option related to the second data collection device, and controlling the The auxiliary display window displays the first data collected by the first data collection device.
The aircraft system according to claim 19, wherein said switching instruction comprises a preset switching instruction, said processor is operative to:

Receiving the preset switching instruction, and controlling, according to the preset switching instruction, the main display window to display the second data collected by the second data collection device and related to the second data collection device Operating the option, and controlling the auxiliary display window to display the first data collected by the first data collection device.
The aircraft system of claim 19 wherein said switching instructions comprise user input instructions and said processor is operative to:

Receiving the user input instruction, and controlling, according to the user input instruction, the main display window to display the second data collected by the second data collection device and operation options related to the second data collection device And controlling the auxiliary display window to display the first data collected by the first data collection device.
The aircraft system of claim 19 wherein said processor is operative to:

Controlling the aircraft to transmit to the display terminal the number displayed by the main display window having the first amount of data According to; and

Controlling the aircraft to transmit data displayed by the secondary display window having a second amount of data to the display terminal, the first amount of data being greater than the second amount of data.
The aircraft system of claim 19 wherein said operational options include parameters and functions of the data collection device.
The aircraft system of claim 19, wherein the aircraft system comprises a map, the secondary display window comprising a first secondary display window and a second secondary display window, the processor for:

Controlling the main display window to display the first data and the first auxiliary display window to display the second data, or controlling the main display window to display the second data and the first auxiliary display window display The first data; and

Controlling the second secondary display window displays the map.
The aircraft system of claim 19, wherein the aircraft system comprises a map, the secondary display window comprising a first secondary display window and a second secondary display window, the processor for:

Controlling the main display window to display the map; and

Controlling the first secondary display window to display the first data and the second secondary display window to display the second data, or controlling the first secondary display window to display the second data and the second secondary The display window displays the first data.
The aircraft system of claim 24 or 25, wherein the first secondary display window and the second secondary display window are located at different preset positions in the primary display window.
The aircraft system of claim 19 wherein said aircraft system includes a map, said processor for:

Controlling the main display window to display the map; and

Controlling the secondary display window to display the first data or the second data.
The aircraft system of claim 27, wherein the secondary display window is located at a preset location in the primary display window.
The aircraft system of claim 24, 25 or 27 wherein said map is preset in said aircraft system.
The aircraft system of claim 24, 25 or 27, wherein said aircraft system comprises a communication module in communication with the cloud, said processor for:

The communication module is controlled to communicate with the cloud to obtain the map.
The aircraft system of claim 19 wherein said display terminal comprises a single display area, said display area comprising said primary display window and said secondary display window.
The aircraft system of claim 19 wherein said main display window has an area greater than said The area of the secondary display window.
The aircraft system of claim 19 wherein said aircraft comprises a third data collection device, said processor for:

Controlling the main display window to display the first data; and

Controlling the auxiliary display window to display third data and/or second data collected by the third data collection device.
The aircraft system of claim 19 wherein said aircraft comprises a third data collection device, said processor for:

Controlling the main display window to display the second data; and

Controlling the auxiliary display window to display third data and/or first data collected by the third data collection device.
The aircraft system of claim 19 wherein said aircraft comprises a third data collection device, said processor for:

Controlling the main display window to display third data collected by the third data collection device; and

Controlling the secondary display window to display the first data and/or the second data.
The aircraft system of claim 19 wherein said data acquisition device comprises a camera and said data comprises an image.
A control method for a display terminal, wherein the display terminal is in communication with an aircraft, the display terminal includes a main display window and a secondary display window, and the aircraft includes a first data collection device and a second data acquisition device The control method includes:

Controlling the main display window to display first data collected by the first data collection device and operation options related to the first data collection device, and controlling the auxiliary display window to display the second data collection device The second data collected; and

Receiving a switching instruction, and controlling, according to the switching instruction, the main display window to display the second data collected by the second data collection device and an operation option related to the second data collection device, and controlling the The auxiliary display window displays the first data collected by the first data collection device.
The control method according to claim 37, wherein the switching instruction comprises a preset switching instruction, the receiving switching instruction, and controlling the main display window to display the second data collecting device according to the switching instruction The second data collected and the operation option associated with the second data collection device, and controlling the auxiliary display window to display the first data collected by the first data collection device includes:

Receiving the preset switching instruction, and controlling, according to the preset switching instruction, the main display window to display the second data collected by the second data collection device and related to the second data collection device Operating the option, and controlling the auxiliary display window to display the first data collected by the first data collection device.
The control method according to claim 37, wherein said switching instruction comprises a user inputting an instruction, Receiving a switching instruction, and controlling, according to the switching instruction, the main display window to display the second data collected by the second data collection device and an operation option related to the second data collection device, and Controlling the auxiliary display window to display the first data collected by the first data collection device includes:

Receiving the user input instruction, and controlling, according to the user input instruction, the main display window to display the second data collected by the second data collection device and operation options related to the second data collection device And controlling the auxiliary display window to display the first data collected by the first data collection device.
The control method according to claim 37, wherein said control method comprises:

Receiving data displayed by the main display window having a first amount of data transmitted by the aircraft; and

Receiving data displayed by the auxiliary display window having a second amount of data transmitted by the aircraft, the first amount of data being greater than the second amount of data.
The control method according to claim 37, wherein said operation option comprises parameters and functions of the data collection device.
The control method according to claim 37, wherein the display terminal comprises a map, the secondary display window comprises a first secondary display window and a second secondary display window, and the control method comprises:

Controlling the main display window to display the first data and the first auxiliary display window to display the second data, or controlling the main display window to display the second data and the first auxiliary display window display The first data; and

Controlling the second secondary display window displays the map.
The control method according to claim 37, wherein the display terminal comprises a map, the secondary display window comprises a first secondary display window and a second secondary display window, and the control method comprises:

Controlling the main display window to display the map; and

Controlling the first secondary display window to display the first data and the second secondary display window to display the second data, or controlling the first secondary display window to display the second data and the second secondary The display window displays the first data.
The control method according to claim 42 or 43, wherein the first secondary display window and the second secondary display window are located at different preset positions in the main display window.
The control method according to claim 37, wherein the display terminal comprises a map, and the control method comprises:

Controlling the main display window to display the map; and

Controlling the secondary display window to display the first data or the second data.
The control method according to claim 45, wherein said auxiliary display window is located at a preset position in said main display window.
The control method according to claim 42, 43 or 45, wherein said map is preset in said display In the terminal.
The control method according to claim 42, 43 or 45, wherein the display terminal comprises a communication module that communicates with the cloud, and the control method comprises:

The communication module is controlled to communicate with the cloud to obtain the map.
The control method according to claim 37, wherein said display terminal comprises a single display area, and said display area includes said main display window and said auxiliary display window.
The control method according to claim 37, wherein an area of said main display window is larger than an area of said auxiliary display window.
The control method according to claim 37, wherein the aircraft comprises a third data collection device, and the control method comprises:

Controlling the main display window to display the first data; and

Controlling the auxiliary display window to display third data and/or second data collected by the third data collection device.
The control method according to claim 37, wherein the aircraft comprises a third data collection device, and the control method comprises:

Controlling the main display window to display the second data; and

Controlling the auxiliary display window to display third data and/or first data collected by the third data collection device.
The control method according to claim 37, wherein the aircraft comprises a third data collection device, and the control method comprises:

Controlling the main display window to display third data collected by the third data collection device; and

Controlling the secondary display window to display the first data and/or the second data.
The control method according to claim 37, wherein said data collection means comprises a camera, said data comprising an image.
A display terminal, wherein the display terminal is in communication with an aircraft, the aircraft includes a first data collection device and a second data collection device, and the display terminal comprises:

Main display window;

Auxiliary display window; and

a processor for:

Controlling the main display window to display first data collected by the first data collection device and operation options related to the first data collection device, and controlling the auxiliary display window to display the second data collection device The second data collected; and

Receiving a switching instruction, and controlling, according to the switching instruction, the main display window to display the second data collected by the second data collection device and an operation option related to the second data collection device, and controlling the Supplementary display The window displays the first data collected by the first data collection device.
The display terminal according to claim 55, wherein the switching instruction comprises a preset switching instruction, and the processor is configured to:

Receiving the preset switching instruction, and controlling, according to the preset switching instruction, the main display window to display the second data collected by the second data collection device and related to the second data collection device Operating the option, and controlling the auxiliary display window to display the first data collected by the first data collection device.
The display terminal according to claim 55, wherein said switching instruction comprises a user input instruction, and said processor is configured to:

Receiving the user input instruction, and controlling, according to the user input instruction, the main display window to display the second data collected by the second data collection device and operation options related to the second data collection device And controlling the auxiliary display window to display the first data collected by the first data collection device.
The display terminal of claim 55, wherein the processor is configured to:

Controlling the aircraft to transmit data displayed by the main display window having a first amount of data to the display terminal; and

Controlling the aircraft to transmit data displayed by the secondary display window having a second amount of data to the display terminal, the first amount of data being greater than the second amount of data.
A display terminal according to claim 55, wherein said operational options include parameters and functions of the data collection device.
The display terminal according to claim 55, wherein the display terminal comprises a map, the auxiliary display window comprises a first auxiliary display window and a second auxiliary display window, and the processor is configured to:

Controlling the main display window to display the first data and the first auxiliary display window to display the second data, or controlling the main display window to display the second data and the first auxiliary display window display The first data; and

Controlling the second secondary display window displays the map.
The display terminal according to claim 55, wherein the display terminal comprises a map, the auxiliary display window comprises a first auxiliary display window and a second auxiliary display window, and the processor is configured to:

Controlling the main display window to display the map; and

Controlling the first secondary display window to display the first data and the second secondary display window to display the second data, or controlling the first secondary display window to display the second data and the second secondary The display window displays the first data.
The display terminal according to claim 60 or 61, wherein the first secondary display window and the second secondary display window are located at different preset positions in the main display window.
The display terminal according to claim 55, wherein the display terminal comprises a map, and the processor is configured to:

Controlling the main display window to display the map; and

Controlling the secondary display window to display the first data or the second data.
A display terminal according to claim 63, wherein said auxiliary display window is located at a preset position in said main display window.
A display terminal according to claim 60, 61 or 63, wherein said map is preset in said display terminal.
The display terminal according to claim 60, 61 or 63, wherein the display terminal comprises a communication module that communicates with the cloud, the processor is configured to:

The communication module is controlled to communicate with the cloud to obtain the map.
A display terminal according to claim 55, wherein said display terminal comprises a single display area, said display area comprising said main display window and said auxiliary display window.
A display terminal according to claim 55, wherein an area of said main display window is larger than an area of said auxiliary display window.
The display terminal of claim 55, wherein the aircraft comprises a third data collection device, the processor for:

Controlling the main display window to display the first data; and

Controlling the auxiliary display window to display third data and/or second data collected by the third data collection device.
The display terminal of claim 55, wherein the aircraft comprises a third data collection device, the processor for:

Controlling the main display window to display the second data; and

Controlling the auxiliary display window to display third data and/or first data collected by the third data collection device.
The display terminal of claim 55, wherein the aircraft comprises a third data collection device, the processor for:

Controlling the main display window to display third data collected by the third data collection device; and

Controlling the secondary display window to display the first data and/or the second data.
A display terminal according to claim 55, wherein said data collection means comprises a camera, said data comprising an image.