CN106796481B - Control method, control device and electronic device - Google Patents
Control method, control device and electronic device Download PDFInfo
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- CN106796481B CN106796481B CN201680002582.4A CN201680002582A CN106796481B CN 106796481 B CN106796481 B CN 106796481B CN 201680002582 A CN201680002582 A CN 201680002582A CN 106796481 B CN106796481 B CN 106796481B
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- return voyage
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
- G05D1/0044—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement by providing the operator with a computer generated representation of the environment of the vehicle, e.g. virtual reality, maps
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
- G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
- G06F3/048—Interaction techniques based on graphical user interfaces [GUI]
- G06F3/0481—Interaction techniques based on graphical user interfaces [GUI] based on specific properties of the displayed interaction object or a metaphor-based environment, e.g. interaction with desktop elements like windows or icons, or assisted by a cursor's changing behaviour or appearance
- G06F3/04817—Interaction techniques based on graphical user interfaces [GUI] based on specific properties of the displayed interaction object or a metaphor-based environment, e.g. interaction with desktop elements like windows or icons, or assisted by a cursor's changing behaviour or appearance using icons
Abstract
The invention discloses a kind of control methods, for controlling electronic device (100).Electronic device (100) includes display (101) and communication module (102).Communication module (102) with aircraft (200) for communicating.Control method includes：(S1) control display (101) shows posture dynamic icon (103)；(S2) feedback information for the aircraft (200) that communication module (102) receives is obtained；(S3) flight attitude of aircraft (200) is obtained according to feedback information；And (S4) adjusts the display of posture dynamic icon (103) according to flight attitude.The invention also discloses a kind of control device (110) and a kind of electronic devices (100).
Description
Technical field
The present invention relates to consumer electronics technology, more particularly to a kind of control method, control device and electronic device.
Background technology
With the continuous development of science and technology, the application of the electronic equipments such as mobile phone, tablet computer is more and more extensive, is such as applied to remote
Range monitoring or manipulation aircraft etc..Currently, in electronic equipment remote monitoring or manipulation aircraft, it can not be from the aobvious of electronic equipment
Show the flight attitude for observing aircraft in interface, causes user experience bad.
Invention content
Embodiments of the present invention aim to solve at least one of the technical problems existing in the prior art.For this purpose, of the invention
Embodiment need to provide a kind of control method, control device and electronic device.
The present invention provides a kind of control method, for controlling electronic device；The electronic device includes display and communication
Module, the communication module is used for and aircraft communication；The control method includes the following steps：
It controls the display and shows posture dynamic icon；
Obtain the feedback information for the aircraft that the communication module receives；
The flight attitude of the aircraft is obtained according to the feedback information；And
The display of the posture dynamic icon is adjusted according to the flight attitude.
In some embodiments, the posture dynamic icon includes aircraft sub-icon, and the flight attitude includes described
The step of head direction of aircraft, the display that the posture dynamic icon is adjusted according to the flight attitude includes：
The direction of the aircraft sub-icon is adjusted according to head direction.
In some embodiments, the posture dynamic icon includes horizontal line sub-icon, and the flight attitude includes institute
The fuselage inclined direction and standard of fuselage degree of aircraft are stated, it is described that the posture dynamic icon is adjusted according to the flight attitude
The step of display includes：
According to the fuselage inclined direction and the standard of fuselage degree adjust the inclined direction of the horizontal line sub-icon with
Inclined degree.
In some embodiments, the posture dynamic icon includes data sub-icon, and the flight attitude includes described
The step of height and distance of aircraft, the display that the posture dynamic icon is adjusted according to the flight attitude includes：
It controls the display and shows the data sub-icon in predefined conditions；And
According to the height and apart from the display for adjusting the data sub-icon.
In some embodiments, the predetermined condition includes taking off, landing and the height and distance change are more than pre-
It is one or more when determining threshold value.
In some embodiments, the posture dynamic icon include for indicate the aircraft sub-icon of the aircraft,
For showing the fuselage inclined direction of the aircraft and the horizontal line sub-icon of standard of fuselage degree and the idea icon that makes a return voyage, institute
It includes left line and right line to state horizontal line sub-icon, and the aircraft sub-icon is between the left line and the right line, the appearance
State dynamic icon includes the idea icon that makes a return voyage, and the flight attitude includes the aircraft current location and the phase maked a return voyage a little
To direction and/distance, the step of display that the posture dynamic icon is adjusted according to the flight attitude, includes：
Control the display shown on the horizontal line sub-icon described in make a return voyage idea icon；And
According to the aircraft and makes a return voyage and relative direction a little and/or apart from the dot map that makes a return voyage described in adjusting be marked on the water
Position on horizontal line sub-icon.
In some embodiments, described according to the aircraft and relative direction a little and/or apart from adjusting institute of making a return voyage
The step of stating the position that the dot map that makes a return voyage is marked on the horizontal line sub-icon include：
It makes a return voyage described in judgement and a little whether is overlapped with the aircraft in the horizontal direction；
If described make a return voyage a little overlaps with the aircraft in the horizontal direction, control is folded in the position of the aircraft sub-icon
Add the idea icon that makes a return voyage described in display；Otherwise
According to the direction of a little relatively described aircraft of making a return voyage, shown on the left line or right line of the horizontal line sub-icon
Show the idea icon that makes a return voyage；And/or the distance according to a little relatively described aircraft of making a return voyage, according to predetermined ratio,
Away from the dot map that makes a return voyage described in display at the aircraft sub-icon respective distance on the left line or right line of the horizontal line sub-icon
Mark.
In some embodiments, described to return when the idea icon that makes a return voyage is with the aircraft sub-icon Overlapping display
Destination sub-icon is shown in the form of identifying letter or mark word in the aircraft sub-icon；
Otherwise, the idea icon that makes a return voyage includes figure and the mark letter in the figure or mark word.
In some embodiments, the posture dynamic icon includes angle sub-icon, and the flight attitude includes described
The step of pitch angle of the holder of aircraft, the display that the posture dynamic icon is adjusted according to the flight attitude, wraps
It includes：
The angle sub-icon is adjusted according to the pitch angle of the holder.
In some embodiments, the angle sub-icon includes graduation mark and angle number corresponding with the graduation mark
Value, the angular values are shown in the side of the graduation mark.
In some embodiments, the graduation mark includes solid line and dotted line, and the angular values include positive-angle numerical value
And negative angle numerical value, the solid line is corresponding with the positive-angle numerical value, and the dotted line is corresponding with the negative angle numerical value.
In some embodiments, the angle sub-icon includes a datum line, and the solid line is parallel with the dotted line
In the datum line, as the length of the increase solid line of the positive-angle numerical value is gradually shortened, with the negative angle number of degrees
The length of the increase dotted line of value is gradually shortened.
In some embodiments, the posture dynamic icon includes aircraft sub-icon, horizontal line sub-icon and angle
Icon, the flight attitude include the direction of the aircraft, the fuselage inclined direction of the aircraft and standard of fuselage degree with
And the pitch angle of the holder of the aircraft, the display that the posture dynamic icon is adjusted according to the flight attitude
Step includes：
The angle sub-icon is adjusted according to the pitch angle of the holder；
Adjust being oriented towards front for the aircraft sub-icon；And
The horizontal line subgraph is adjusted to be designated as fully horizontally.
The present invention provides a kind of control device, and for controlling electronic device, the electronic device includes display and communication
Module, the communication module is used for and aircraft communication；The control device includes：
First control module shows posture dynamic icon for controlling the display；
First acquisition module, the feedback information for obtaining the aircraft that the communication module receives；
Second acquisition module, the flight attitude for obtaining the aircraft according to the feedback information；And
The first adjustment module, the display for adjusting the posture dynamic icon according to the flight attitude.
In some embodiments, the posture dynamic icon includes aircraft sub-icon, and the flight attitude includes described
The direction of aircraft, the first adjustment module include：
The first adjustment submodule, the direction for adjusting the aircraft sub-icon according to the direction of the aircraft.
In some embodiments, the posture dynamic icon includes horizontal line sub-icon, and the flight attitude includes institute
The fuselage inclined direction and standard of fuselage degree of aircraft are stated, the first adjustment module includes：
Second adjustment submodule, for adjusting the horizontal line according to the fuselage inclined direction and the standard of fuselage degree
The inclined direction and inclined degree of sub-icon.
In some embodiments, the posture dynamic icon includes data sub-icon, and the flight attitude includes described
The height and distance of aircraft, the first adjustment module include：
First control submodule shows the data sub-icon in predefined conditions for controlling the display；And
Third adjusts submodule, for according to the height and apart from the display for adjusting the data sub-icon.
In some embodiments, the predetermined condition includes taking off, landing and the height and distance change are more than pre-
It is one or more when determining threshold value.
In some embodiments, the posture dynamic icon include for indicate the aircraft sub-icon of the aircraft,
For showing the fuselage inclined direction of the aircraft and the horizontal line sub-icon of standard of fuselage degree and the idea icon that makes a return voyage, institute
It includes left line and right line to state horizontal line sub-icon, and the aircraft sub-icon is between the left line and the right line, the appearance
State dynamic icon includes the idea icon that makes a return voyage, and the flight attitude includes the aircraft current location and the phase maked a return voyage a little
To direction and/distance, the first adjustment module includes：
Second control submodule, show for controlling the display on the horizontal line sub-icon described in make a return voyage idea
Icon；And
4th control submodule, for according to the aircraft and the relative direction a little and/or apart from described in adjusting of making a return voyage
The dot map that makes a return voyage is marked on the position on the horizontal line sub-icon.
In some embodiments, the 4th control submodule includes：
Judging unit, for judging whether described make a return voyage a little overlaps with the aircraft in the horizontal direction；
First control unit, for it is described make a return voyage a little overlapped in the horizontal direction with the aircraft when control it is described fly
Make a return voyage idea icon described in the position Overlapping display of loom icon；And
Second control unit, for it is described make a return voyage a little misaligned with the aircraft in the horizontal direction when, according to described
It makes a return voyage the direction of a little relatively described aircraft, make a return voyage on the left line or right line of the horizontal line sub-icon described in display dot map
Mark；And/or the distance according to a little relatively described aircraft of making a return voyage, according to predetermined ratio, in the horizontal line subgraph
Away from the idea icon that makes a return voyage described in display at the aircraft sub-icon respective distance on the left line of target or right line.
In some embodiments, described to return when the idea icon that makes a return voyage is with the aircraft sub-icon Overlapping display
Destination sub-icon is shown in the form of identifying letter or mark word in the aircraft sub-icon；
Otherwise, the idea icon that makes a return voyage includes figure and the mark letter in the figure or mark word.
In some embodiments, the posture dynamic icon includes angle sub-icon, and the flight attitude includes described
The pitch angle of the holder of aircraft, the first adjustment module include：
5th adjustment submodule, for adjusting the angle sub-icon according to the pitch angle of the holder.
In some embodiments, the angle sub-icon includes graduation mark and angle number corresponding with the graduation mark
Value, the angular values are shown in the side of the graduation mark.
In some embodiments, the graduation mark includes solid line and dotted line, and the angular values include positive-angle numerical value
And negative angle numerical value, the solid line is corresponding with the positive-angle numerical value, and the dotted line is corresponding with the negative angle numerical value.
In some embodiments, the angle sub-icon includes a datum line, and the solid line is parallel with the dotted line
In the datum line, as the length of the increase solid line of the positive-angle numerical value is gradually shortened, with the negative angle number of degrees
The length of the increase dotted line of value is gradually shortened.
In some embodiments, the posture dynamic icon includes aircraft sub-icon, horizontal line sub-icon and angle
Icon, the flight attitude include the direction of the aircraft, the fuselage inclined direction of the aircraft and standard of fuselage degree with
And the pitch angle of the holder of the aircraft, the first adjustment module include：
5th adjustment submodule, for adjusting the angle sub-icon according to the pitch angle of the holder；
6th adjustment submodule, for adjusting being oriented towards front of the aircraft sub-icon；And
7th adjustment submodule, adjusts the horizontal line subgraph and is designated as fully horizontally.
The present invention provides a kind of electronic device, including：
Display；
For the communication module with aircraft communication；And
Control device described in embodiment as above.
In some embodiments, the electronic device includes remote controler, mobile phone, tablet computer, smartwatch, Brilliant Eyes
The one or more of mirror and intelligent helmet.
Control method, control device and electronic device control display in embodiment of the present invention intelligently show appearance
State dynamic icon so that user can be visually known the flight appearance of aircraft according to the different displays of posture dynamic icon
State, the user experience is improved.
The additional aspect and advantage of embodiments of the present invention will be set forth in part in the description, partly will be from following
Description in become apparent, or the practice of embodiment through the invention is recognized.
Description of the drawings
The above-mentioned and/or additional aspect and advantage of the present invention is from combining in description of the following accompanying drawings to embodiment by change
It obtains obviously and is readily appreciated that, wherein：
Fig. 1 is the flow diagram of the control method of certain embodiments of the present invention.
Fig. 2 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Fig. 3 is the electronic device of certain embodiments of the present invention and the schematic diagram in kind of aircraft.
Fig. 4 is the flow diagram of the control method of certain embodiments of the present invention.
Fig. 5 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Fig. 6 is the flow diagram of the control method of certain embodiments of the present invention.
Fig. 7 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Fig. 8 is the flow diagram of the control method of certain embodiments of the present invention.
Fig. 9 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Figure 10 is the flow diagram of the control method of certain embodiments of the present invention.
Figure 11 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Figure 12 is the flow diagram of the control method of certain embodiments of the present invention.
Figure 13 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Figure 14 is the flow diagram of the control method of certain embodiments of the present invention.
Figure 15 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Figure 16 is the flow diagram of the control method of certain embodiments of the present invention.
Figure 17 is the electronic device of certain embodiments of the present invention and the high-level schematic functional block diagram of control device.
Figure 18 is the schematic diagram of the display display interface of the electronic device of certain embodiments of the present invention.
Figure 19 is that posture dynamic icon adjusts in the display display interface of the electronic device of certain embodiments of the present invention
The schematic diagram of display.
Figure 20 is that posture dynamic icon adjusts in the display display interface of the electronic device of certain embodiments of the present invention
The schematic diagram of display.
Figure 21 is that posture dynamic icon adjusts in the display display interface of the electronic device of certain embodiments of the present invention
The schematic diagram of display.
Figure 22 is that posture dynamic icon adjusts in the display display interface of the electronic device of certain embodiments of the present invention
The schematic diagram of display.
Figure 23 is that posture dynamic icon adjusts in the display display interface of the electronic device of certain embodiments of the present invention
The schematic diagram of display.
Specific implementation mode
Embodiments of the present invention are described below in detail, the example of the embodiment is shown in the accompanying drawings, wherein from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining the present invention, and is not considered as limiting the invention.
In the description of the present invention, it is to be understood that, term " first ", " second " are used for description purposes only, and cannot
It is interpreted as indicating or implies relative importance or implicitly indicate the quantity of indicated technical characteristic.Define as a result, " the
One ", the feature of " second " can explicitly or implicitly include one or more feature.In description of the invention
In, the meaning of " plurality " is two or more, unless otherwise specifically defined.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be to be electrically connected or can be in communication with each other to be mechanical connection；It can be directly connected, it can also be by between intermediary
It connects connected, can be the interaction relationship of the connection or two elements inside two elements.For the ordinary skill of this field
For personnel, the specific meanings of the above terms in the present invention can be understood according to specific conditions.
Following disclosure provides many different embodiments or example is used for realizing the different structure of the present invention.In order to
Simplify disclosure of the invention, hereinafter the component of specific examples and setting are described.Certainly, they are merely examples, and
And it is not intended to limit the present invention.In addition, the present invention can in different examples repeat reference numerals and/or reference letter,
This repetition is for purposes of simplicity and clarity, itself not indicate between discussed various embodiments and/or setting
Relationship.In addition, the present invention provides various specific techniques and material example, but those of ordinary skill in the art can be with
Recognize the application of other techniques and/or the use of other materials.
Embodiments of the present invention are described below in detail, the example of the embodiment is shown in the accompanying drawings, wherein from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining the present invention, and is not considered as limiting the invention.
Also referring to Fig. 1-3 and Figure 18, the control method of embodiment of the present invention is electric for controlling electronic device 100
Sub-device 100 includes display 101 and communication module 102, and communication module 102 with aircraft 200 for communicating.Control method packet
It includes：
S1, control display 101 show posture dynamic icon 103；
S2 obtains the feedback information for the aircraft 200 that communication module 102 receives；
S3 obtains the flight attitude of aircraft 200 according to feedback information；And
S4 adjusts the display of posture dynamic icon 103 according to flight attitude.
Referring to Fig. 2, in the control device 110 of embodiment of the present invention, control device 110 includes the first control module
111, the first acquisition module 112, the second acquisition module 113 and the first adjustment module 114, can be respectively used to realize S1, S2, S3 and
S4.That is, the first control module 111 shows posture dynamic icon 103 for controlling display 101.First acquisition module
The feedback information of 112 aircraft 200 for obtaining the reception of communication module 102.Second acquisition module 113 is used for according to feedback letter
Breath obtains the flight attitude of aircraft 200.The first adjustment module 114 is used to adjust posture dynamic icon 103 according to flight attitude
Display.
The electronic device 100 of embodiment of the present invention is can be applied in the control device 110 of embodiment of the present invention.It please join
Fig. 3 is read, the electronic device 100 in present embodiment is tablet computer.
In some embodiments, electronic device 100 may also include mobile phone, remote controler, smartwatch, intelligent glasses, intelligence
In the display terminals with display function such as the energy helmet, other virtual reality wearable devices, other augmented reality wearable devices
It is one or more.Display 101 is used for display monitoring or operates the relevant information of aircraft 200, such as the ginseng of aircraft itself
Number information, flight information, the image or video pictures shot through aircraft 200.
Incorporated by reference to Figure 18, user can be by observing the different displays of the posture dynamic icon 103 in display 101 come straight
See the flight attitude that ground understands aircraft 200.
Control method, control device 110 and electronic device 100 in embodiment of the present invention control 101 intelligence of display
Ground shows posture dynamic icon 103 so that user can be winged to be visually known according to the different displays of posture dynamic icon 103
The flight attitude of row device 200, the user experience is improved.
Also referring to Fig. 3-5 and Figure 18-19, in some embodiments, posture dynamic icon 103 includes aircraft subgraph
Mark 1031, flight attitude includes the head direction of aircraft 200, and the display of posture dynamic icon 103 is adjusted according to flight attitude
The step of include：
S401, according to the direction of head direction adjustment aircraft sub-icon 1031.
Referring to Fig. 5, in the control device 110 of embodiment of the present invention, the first adjustment module of control device 110
114 include the first adjustment submodule 1141, can be used for realizing S401.I.e. the first adjustment submodule 1141 is used for according to head direction
Adjust the direction of aircraft sub-icon 1031.
9 are please referred to Fig.1, when the head of aircraft 200 is towards front, then aircraft sub-icon 1031 is also towards front；
When the head of aircraft 200 towards it is right when, then aircraft sub-icon 1031 is also towards the right side；When the head of aircraft 200 towards it is left when, then aircraft
Sub-icon 1031 is also towards a left side.In present embodiment, aircraft sub-icon 1031 is triangle, and the direction of aircraft sub-icon 1031 is by three
The direction on angular vertex determines.It is appreciated that aircraft sub-icon 1031 can also be other shapes, such as rectangle, pentagon,
Hexagon, heptagon, finger-shaped etc..
Control method, control device 110 and electronic device 100 in embodiment of the present invention control 101 intelligence of display
Ground shows aircraft sub-icon 1031 so that user can fly according to the different of aircraft sub-icon 1031 towards to be visually known
The head direction of device 200, the user experience is improved.
Also referring to Fig. 3, Fig. 6-7, Figure 18 and Figure 20, in some embodiments, posture dynamic icon 103 includes water
Horizontal line sub-icon 1032, flight attitude includes the fuselage inclined direction and standard of fuselage degree of aircraft 200, according to flight attitude tune
The step of display of whole posture dynamic icon 103 includes：
S402, according to the inclined direction and inclination of fuselage inclined direction and standard of fuselage degree adjustment horizontal line sub-icon 1032
Degree.
Referring to Fig. 7, in the control device 110 of embodiment of the present invention, the first adjustment module of control device 110
114 include second adjustment submodule 1142, can be used for realizing S402.I.e. second adjustment submodule 1142 according to fuselage for tilting
The inclined direction and inclined degree of direction and standard of fuselage degree adjustment horizontal line sub-icon 1032.
Figure 20 is please referred to, when the standard of fuselage of aircraft 200, then horizontal line sub-icon 1032 is also horizontal；When
The fuselage of aircraft 200 is towards (with left lower than right) when left bank, then horizontal line sub-icon 1032 is also towards left bank (with left lower than right)；When
The fuselage of aircraft 200 is towards (right low left high, such as the middle graph of Figure 20) when right bank, then horizontal line sub-icon 1032 is also towards Right deviation
Tiltedly (right low left high, such as most figure below of Figure 20).The inclined degree of horizontal line sub-icon 1032 is bigger, shows that the levelness of fuselage is got over
It is low, that is, to show that the inclined degree of fuselage is also bigger.For example, horizontal line sub-icon 1032 is higher towards left-oblique degree, fuselage
More towards left bank, the levelness of fuselage is lower；Horizontal line sub-icon 1032 is higher towards right-oblique degree, and fuselage is also more towards Right deviation
Tiltedly, the levelness of fuselage is lower.
Control method, control device 110 and electronic device 100 in embodiment of the present invention control 101 intelligence of display
Ground display horizontal line sub-icon 1032 so that user can be according to the different inclined directions and difference of horizontal line sub-icon 1032
Inclined degree is visually known the fuselage inclined direction of aircraft 200 and standard of fuselage degree, and the user experience is improved.
Also referring to Fig. 3, Fig. 8-9 and Figure 18-20, in some embodiments, posture dynamic icon 103 includes data
Sub-icon 1033, flight attitude include the height and distance of aircraft 200, and posture dynamic icon 103 is adjusted according to flight attitude
Display the step of include：
S403 controls the display data sub-icon 1033 in predefined conditions of display 101；And
S404, the display according to height and apart from adjustment data sub-icon 1033.
Referring to Fig. 9, in the control device 110 of embodiment of the present invention, the first adjustment module of control device 110
114 include that the first control submodule 1143 and third adjust submodule 1144, can be respectively used to realize S403 and S404.I.e. first
Control submodule 1143 is for controlling the display data sub-icon 1033 in predefined conditions of display 101.Third adjusts submodule
1144 for the display according to height and apart from adjustment data sub-icon 1033.
Also referring to Figure 18-20, predetermined condition includes taking off, landing and when height or distance change are more than predetermined threshold
It is one or more.In other words, when aircraft 200 takes off with landing, data sub-icon 1033 will necessarily be shown.Aircraft
200 in flight course, and data sub-icon 1033 just can when only the height or distance change of aircraft 200 are more than predetermined threshold
It shows, if the height or distance change of aircraft 200 are not above predetermined threshold, data sub-icon 1033 will not be shown
Out.
Control method, control device 110 and electronic device 100 in embodiment of the present invention control 101 intelligence of display
Ground display data sub-icon 1033 in predefined conditions so that user can read the height and distance of aircraft 200, improve
User experience.
Also referring to Fig. 3, Figure 10-11, Figure 18-20, in some embodiments, posture dynamic icon 103 includes using
In the aircraft sub-icon 1031 of expression aircraft 200, fuselage inclined direction and standard of fuselage degree for showing aircraft 200
Horizontal line sub-icon 1032 and the idea icon 1034 that makes a return voyage, the horizontal line sub-icon 1032 include left line and right line, aircraft
For icon 1031 between left line and the right line, flight attitude includes that the current location of the aircraft 200 is maked a return voyage with described
The relative direction of point and/distance include according to the step of display of flight attitude adjustment posture dynamic icon 103：
S405, control display 101 show the idea icon 1034 that makes a return voyage on horizontal line sub-icon 1032；And
S406 according to aircraft 200 and makes a return voyage and relative direction a little and/or apart from adjusting makes a return voyage idea icon 1034 in water
Position on horizontal line sub-icon 1032.
1 is please referred to Fig.1, in the control device 110 of embodiment of the present invention, the first adjustment module of control device 110
114 include that the second control submodule 1145 and the 4th adjusts submodule 1146, can be respectively used to realize S405 and S406.I.e. second
Control submodule 1145 shows the idea icon 1034 that makes a return voyage for controlling display 101 on horizontal line sub-icon 1032.4th
Adjustment submodule 1146 is used to relative direction a little and/or be maked a return voyage idea icon apart from adjusting according to aircraft 200 and making a return voyage
1034 position on horizontal line sub-icon 1032.
Incorporated by reference to Figure 18-20, idea of making a return voyage icon 1034 is remoter apart from aircraft sub-icon 1031, then the distance that shows to make a return voyage is got over
Far；Idea of making a return voyage icon 1034 is closer apart from aircraft sub-icon 1031, then shows to make a return voyage apart from closer.
Control method, control device 110 and electronic device 100 in embodiment of the present invention control 101 intelligence of display
It makes a return voyage idea icon 1034 in display on ground so that user can read the distance of making a return voyage of aircraft 200, and the user experience is improved.
Also referring to Figure 12-13, Figure 18-21, in some embodiments, according to aircraft 200 and the phase maked a return voyage a little
Include following son to direction and/or apart from the idea icon 1034 that makes a return voyage is adjusted in the step of position on horizontal line sub-icon 1032
Step：
S4061, whether judgement is maked a return voyage a little overlaps with aircraft 200 in the horizontal direction；
S4062 is a little overlapped with aircraft 200 in the horizontal direction if making a return voyage, and is controlled in the position of aircraft sub-icon 1031
Overlapping display makes a return voyage idea icon 1034；And
S4063, if it is a little misaligned with aircraft 200 in the horizontal direction to make a return voyage, according to the relative flight device 200 that makes a return voyage
Direction shows the idea icon 1034 that makes a return voyage on the left line or right line of horizontal line sub-icon 1032；And/or according to making a return voyage a little
The distance of relative flight device 200, according to predetermined ratio, away from aircraft sub-icon on the left line or right line of horizontal line sub-icon 1032
The idea icon 1034 that makes a return voyage is shown at 1031 respective distances.
3 are please referred to Fig.1, in the control device 110 of embodiment of the present invention, the 4th adjustment submodule of control device 110
Block 1146 includes judging unit 11461, the first control unit 11462 and the second control unit 11463, can be respectively used to realize
S4061, S4062 and S4063.I.e. judging unit 11461 is for judging to make a return voyage a little whether weighed with aircraft 200 in the horizontal direction
It closes.First control unit 11462 is used to control in aircraft sub-icon when making a return voyage and a little overlapping with aircraft 200 in the horizontal direction
1031 position Overlapping display makes a return voyage idea icon 1034.Second control unit 11463 be used for make a return voyage a little in the horizontal direction with
When aircraft 200 is misaligned, according to a direction for relative flight device 200 of making a return voyage, on the left line of horizontal line sub-icon 1032 or the right side
The idea icon 1034 that makes a return voyage is shown on line；And/or according to a horizontal distance for relative flight device 200 of making a return voyage, according to predetermined
Ratio is maked a return voyage dot map on the left line or right line of horizontal line sub-icon 1032 away from display at 1031 respective distance of aircraft sub-icon
Mark 1034.
When the idea icon 1034 that makes a return voyage is with aircraft 1031 Overlapping display of sub-icon, idea of making a return voyage icon 1034 is with identifier word
Female or mark word form is shown in aircraft sub-icon 1031；Otherwise, idea of making a return voyage icon 1034 includes figure and position
In mark letter or mark word in figure.
Concrete example illustrates, refers to Figure 21, and idea of making a return voyage in upper figure icon 1034 includes circle and in circle
Mark letter be H, and positioned at horizontal line sub-icon 1032 right line and with aircraft sub-icon 1031 exist distance M, thus use
Known to family：Aircraft 200 does not overlap a little with making a return voyage at this time, aircraft 200 be located at make a return voyage left a little and with make a return voyage a little in water
Square upwards there are certain level distance, this horizontal distance can be calculated according to distance M and predetermined ratio.
Idea of making a return voyage in figure below of Figure 21 icon 1034 only includes that mark letter is H, and is shown in aircraft sub-icon 1031
It is interior.Thus known to user：Aircraft 200 is overlapped with making a return voyage at this time, that is, aircraft 200, which has returned to, to make a return voyage a little.
It is appreciated that the figure in the idea icon 1034 that makes a return voyage can be the circle in present embodiment, three are can also be
The other arbitrary shapes such as angular, oval, rectangle, pentagon.The mark letter and mark word of idea of making a return voyage icon 1034
It can also arbitrary form, it is not limited to be H in present embodiment.
Also referring to Fig. 3, Figure 14-15 and Figure 22, in some embodiments, posture dynamic icon 103 includes angle
Sub-icon 1035, flight attitude include the pitch angle of the holder of aircraft 200, and posture dynamic icon is adjusted according to flight attitude
The step of 103 display includes：
S407 adjusts the angle sub-icon 1035 according to the pitch angle of holder.
5 are please referred to Fig.1, in the control device 110 of embodiment of the present invention, the first adjustment module of control device 110
114 include the 5th adjustment submodule 1147, can be used for realizing S407.I.e. the 5th adjustment submodule 1147 is used for bowing according to holder
Elevation angle degree adjusts the angle sub-icon 1035.
Figure 22 is please referred to, angle sub-icon 1035 includes graduation mark and angular values corresponding with graduation mark, angular values
It is shown in the side of graduation mark.Graduation mark includes datum line, solid line and dotted line, and solid line is parallel to datum line with dotted line.Angle number
Value includes positive-angle numerical value and negative angle numerical value, and solid line is corresponding with positive-angle numerical value, and dotted line is corresponding with negative angle numerical value, 0 ° of correspondence
The difference of solid line, the corresponding angular values of each two graduation mark is 10 °.As the length of the increase solid line of positive-angle numerical value gradually contracts
It is short, as the length of the increase dotted line of negative angle numerical value is gradually shortened.After the elevation-depression angle for adjusting holder, angle sub-icon 1035
In graduation mark will and then adjustment display, specifically, solid line and dotted line can relative datum line move up or move down, in fact by observation
The relative position of line and dotted line relative datum line, and the differential seat angle for reading solid line or dotted line relative datum line can learn aircraft
The pitch angle of 200 holder.If for example, the display of angle sub-icon 1035 by Figure 22 upper figure variation be figure below when, table
The pitch angle of bright holder is 10 ° by 0 ° of variation；If the display of angle sub-icon 1035 by Figure 22 figure below variation be upper figure when,
It is 0 ° then to show that the pitch angle of holder is changed by 10 °.In present embodiment, graduation mark mirror image is arranged in aircraft sub-icon 1031
Both sides.
Control method, control device 110 and electronic device 100 in embodiment of the present invention control 101 intelligence of display
Ground angles of display sub-icon 1035 so that user can be visually known the cloud of aircraft 200 according to angle sub-icon 1035
The pitch angle of platform, the user experience is improved.
Also referring to Fig. 3, Figure 16-17 and Figure 23, in some embodiments, posture dynamic icon 103 includes aircraft
Sub-icon 1031, horizontal line sub-icon 1032 and angle sub-icon 1035.Flight attitude includes the direction of aircraft 200, flight
The fuselage inclined direction of device 200 and standard of fuselage degree and the pitch angle of the holder of aircraft 200, adjust according to flight attitude
The step of display of posture dynamic icon 103 includes：
S407 adjusts the angle sub-icon 1035 according to the pitch angle of holder；
S408, adjustment aircraft sub-icon 1031 are oriented towards front；And
S409, adjustment horizontal line sub-icon 1032 is fully horizontal.
7 are please referred to Fig.1, in the control device 110 of embodiment of the present invention, the first adjustment module of control device 110
114 include that the 5th adjustment submodule the 1147, the 6th adjusts the adjustment submodule 1149 of submodule 1148 and the 7th, can be respectively used to reality
Existing S407, S408 and S409.I.e. the 5th adjustment submodule 1147 is used to adjust the angle sub-icon according to the pitch angle of holder
1035.6th adjustment submodule 1148 is used to adjust being oriented towards front of aircraft sub-icon 1031；7th adjustment submodule
Block 1149 is fully horizontal for adjusting horizontal line sub-icon 1032.
Please refer to Figure 23, after the pitch angle of holder is adjusted to 10 ° (as above figure), the display interface on display 101 is aobvious
Show being oriented towards front for aircraft sub-icon 1031, horizontal line sub-icon 1032 is fully horizontal (such as figure below), this state
For default conditions.
Not deployed other parts, see the control of embodiment of above in the electronic device 100 of embodiment of the present invention
The corresponding part of method processed or control device 110, is no longer developed in details herein.
In the description of this specification, reference term " embodiment ", " some embodiments ", " schematically implementation
What the description of mode ", " example ", " specific example " or " some examples " etc. meant to describe in conjunction with the embodiment or example
Particular features, structures, materials, or characteristics are contained at least one embodiment or example of the present invention.In this specification
In, schematic expression of the above terms are not necessarily referring to identical embodiment or example.Moreover, the specific spy of description
Sign, structure, material or feature can be combined in any suitable manner in any one or more embodiments or example.
Any process described otherwise above or method description are construed as in flow chart or herein, and expression includes
It is one or more for realizing specific logical function or process the step of executable instruction code module, segment or portion
Point, and the range of the preferred embodiment of the present invention includes other realization, wherein can not press shown or discuss suitable
Sequence, include according to involved function by it is basic simultaneously in the way of or in the opposite order, to execute function, this should be of the invention
Embodiment person of ordinary skill in the field understood.
Expression or logic and/or step described otherwise above herein in flow charts, for example, being considered use
In the order list for the executable instruction for realizing logic function, may be embodied in any computer-readable medium, for
Instruction execution system, device or equipment (system of such as computer based system including processor or other can be held from instruction
The instruction fetch of row system, device or equipment and the system executed instruction) it uses, or combine these instruction execution systems, device or set
It is standby and use.For the purpose of this specification, " computer-readable medium " can any can be included, store, communicating, propagating or passing
Defeated program is for instruction execution system, device or equipment or the dress used in conjunction with these instruction execution systems, device or equipment
It sets.The more specific example (non-exhaustive list) of computer-readable medium includes following：Electricity with one or more wiring
Interconnecting piece (electronic device), portable computer diskette box (magnetic device), random access memory (RAM), read-only memory
(ROM), erasable edit read-only storage (EPROM or flash memory), fiber device and portable optic disk is read-only deposits
Reservoir (CDROM).In addition, computer-readable medium can even is that the paper that can print described program on it or other are suitable
Medium, because can be for example by carrying out optical scanner to paper or other media, then into edlin, interpretation or when necessary with it
His suitable method is handled electronically to obtain described program, is then stored in computer storage.
It should be appreciated that each section of the present invention can be realized with hardware, software, firmware or combination thereof.Above-mentioned
In embodiment, software that multiple steps or method can in memory and by suitable instruction execution system be executed with storage
Or firmware is realized.It, and in another embodiment, can be under well known in the art for example, if realized with hardware
Any one of row technology or their combination are realized：With the logic gates for realizing logic function to data-signal
Discrete logic, with suitable combinational logic gate circuit application-specific integrated circuit, programmable gate array (PGA), scene
Programmable gate array (FPGA) etc..
Those skilled in the art are appreciated that realize all or part of step that above-mentioned implementation carries
It is that relevant hardware can be instructed to complete by program, the program can be stored in a kind of computer readable storage medium
In, which includes the steps that one or a combination set of embodiment of the method when being executed.
In addition, each functional unit in each embodiment of the present invention can be integrated in a processing module, it can also
That each unit physically exists alone, can also two or more units be integrated in a module.Above-mentioned integrated mould
The form that hardware had both may be used in block is realized, can also be realized in the form of software function module.The integrated module is such as
Fruit is realized in the form of software function module and when sold or used as an independent product, can also be stored in a computer
In read/write memory medium.
Storage medium mentioned above can be read-only memory, disk or CD etc..Although having been shown and retouching above
The embodiment of the present invention is stated, it is to be understood that above-described embodiment is exemplary, and should not be understood as the limit to the present invention
System, those skilled in the art can be changed above-described embodiment, change, replace and become within the scope of the invention
Type.
Claims (26)
1. a kind of control method, for controlling electronic device, the electronic device includes display and communication module, the communication
Module is used for and aircraft communication, which is characterized in that the control method includes the following steps：
It controls the display and shows posture dynamic icon；
Obtain the feedback information for the aircraft that the communication module receives；
The flight attitude of the aircraft is obtained according to the feedback information；And
The display of the posture dynamic icon is adjusted according to the flight attitude；
The posture dynamic icon includes for indicating the aircraft sub-icon of the aircraft, the machine for showing the aircraft
Body inclined direction and the horizontal line sub-icon and the idea icon that makes a return voyage, the horizontal line sub-icon of standard of fuselage degree include left line
And right line, for the aircraft sub-icon between the left line and the right line, the posture dynamic icon includes idea of making a return voyage
Icon, the flight attitude include the aircraft current location and the relative direction maked a return voyage a little and/distance, the basis
The flight attitude adjusts the step of display of the posture dynamic icon and includes：
Control the display shown on the horizontal line sub-icon described in make a return voyage idea icon；And
According to the aircraft and makes a return voyage and relative direction a little and/or apart from the dot map that makes a return voyage described in adjusting be marked on the horizontal line
Position on sub-icon.
2. control method as described in claim 1, which is characterized in that the posture dynamic icon includes aircraft sub-icon, institute
The head direction that flight attitude includes the aircraft is stated, it is described that the posture dynamic icon is adjusted according to the flight attitude
The step of display includes：
The direction of the aircraft sub-icon is adjusted according to head direction.
3. control method as described in claim 1, which is characterized in that the posture dynamic icon includes horizontal line sub-icon,
The flight attitude includes the fuselage inclined direction and standard of fuselage degree of the aircraft, described to be adjusted according to the flight attitude
The step of display of the posture dynamic icon includes：
Inclined direction and the inclination of the horizontal line sub-icon are adjusted according to the fuselage inclined direction and the standard of fuselage degree
Degree.
4. control method as described in claim 1, which is characterized in that the posture dynamic icon includes data sub-icon, institute
The height and distance that flight attitude includes the aircraft are stated, it is described that the posture dynamic icon is adjusted according to the flight attitude
Display the step of include：
It controls the display and shows the data sub-icon in predefined conditions；And
According to the height and apart from the display for adjusting the data sub-icon.
5. control method as claimed in claim 4, which is characterized in that the predetermined condition includes taking off, landing and the height
It is one or more when degree and distance change are more than predetermined threshold.
6. control method as described in claim 1, which is characterized in that described according to the aircraft and the contra to make a return voyage a little
To and/or apart from make a return voyage described in adjusting position that dot map is marked on the horizontal line sub-icon the step of include：
It makes a return voyage described in judgement and a little whether is overlapped with the aircraft in the horizontal direction；
If described make a return voyage a little overlaps with the aircraft in the horizontal direction, control aobvious in the superposition of the position of the aircraft sub-icon
Show the idea icon that makes a return voyage；Otherwise
According to the direction of a little relatively described aircraft of making a return voyage, institute is shown on the left line or right line of the horizontal line sub-icon
State the idea icon that makes a return voyage；And/or the distance according to a little relatively described aircraft of making a return voyage, according to predetermined ratio, in institute
It states on the left line or right line of horizontal line sub-icon away from the idea icon that makes a return voyage described in display at the aircraft sub-icon respective distance.
7. control method as claimed in claim 6, which is characterized in that
When it is described make a return voyage idea icon and the aircraft sub-icon Overlapping display when, the dot map that makes a return voyage be marked with mark letter or
The form of mark word is shown in the aircraft sub-icon；
Otherwise, the idea icon that makes a return voyage includes figure and the mark letter in the figure or mark word.
8. control method as described in claim 1, which is characterized in that the posture dynamic icon includes angle sub-icon, institute
The pitch angle that flight attitude includes the holder of the aircraft is stated, it is described that the posture dynamic is adjusted according to the flight attitude
The step of display of icon includes：
The angle sub-icon is adjusted according to the pitch angle of the holder.
9. control method as claimed in claim 8, which is characterized in that the angle sub-icon include graduation mark and with the quarter
The corresponding angular values of line are spent, the angular values are shown in the side of the graduation mark.
10. control method as claimed in claim 9, which is characterized in that the graduation mark includes solid line and dotted line, the angle
Numerical value includes positive-angle numerical value and negative angle numerical value, and the solid line is corresponding with the positive-angle numerical value, and the dotted line is born with described
Angular values correspond to.
11. control method as claimed in claim 10, which is characterized in that the angle sub-icon includes a datum line, institute
It states solid line and is parallel to the datum line with the dotted line, as the length of the increase solid line of the positive-angle numerical value gradually contracts
It is short, as the length of the increase dotted line of the negative angle numerical value is gradually shortened.
12. control method as described in claim 1, which is characterized in that the posture dynamic icon includes aircraft sub-icon, water
Horizontal line sub-icon and angle sub-icon, the flight attitude include the fuselage inclination of the direction of the aircraft, the aircraft
Direction and standard of fuselage degree and the pitch angle of the holder of the aircraft, it is described that the appearance is adjusted according to the flight attitude
The step of display of state dynamic icon includes：
The angle sub-icon is adjusted according to the pitch angle of the holder；
Adjust being oriented towards front for the aircraft sub-icon；And
The horizontal line subgraph is adjusted to be designated as fully horizontally.
13. a kind of control device, for controlling electronic device, the electronic device includes display and communication module, described logical
Letter module is used for and aircraft communication, which is characterized in that the control device includes：
First control module shows posture dynamic icon for controlling the display；
First acquisition module, the feedback information for obtaining the aircraft that the communication module receives；
Second acquisition module, the flight attitude for obtaining the aircraft according to the feedback information；And
The first adjustment module, the display for adjusting the posture dynamic icon according to the flight attitude；
The posture dynamic icon includes for indicating the aircraft sub-icon of the aircraft, the machine for showing the aircraft
Body inclined direction and the horizontal line sub-icon and the idea icon that makes a return voyage, the horizontal line sub-icon of standard of fuselage degree include left line
And right line, for the aircraft sub-icon between the left line and the right line, the posture dynamic icon includes idea of making a return voyage
Icon, the flight attitude include the aircraft current location and the relative direction maked a return voyage a little and/distance, and described first
Adjusting module includes：
Second control submodule, show for controlling the display on the horizontal line sub-icon described in make a return voyage dot map
Mark；And
4th control submodule, for according to the aircraft and the relative direction a little and/or apart from making a return voyage described in adjusting of making a return voyage
Dot map is marked on the position on the horizontal line sub-icon.
14. control device as claimed in claim 13, which is characterized in that the posture dynamic icon includes aircraft sub-icon,
The flight attitude includes the direction of the aircraft, and the first adjustment module includes：
The first adjustment submodule, the direction for adjusting the aircraft sub-icon according to the direction of the aircraft.
15. control device as claimed in claim 13, which is characterized in that the posture dynamic icon includes horizontal line subgraph
Mark, the flight attitude includes the fuselage inclined direction of the aircraft and standard of fuselage degree, the first adjustment module include：
Second adjustment submodule, for adjusting the horizontal line subgraph according to the fuselage inclined direction and the standard of fuselage degree
Target inclined direction and inclined degree.
16. control device as claimed in claim 13, which is characterized in that the posture dynamic icon includes data sub-icon,
The flight attitude includes the height and distance of the aircraft, and the first adjustment module includes：
First control submodule shows the data sub-icon in predefined conditions for controlling the display；And
Third adjusts submodule, for according to the height and apart from the display for adjusting the data sub-icon.
17. control device as claimed in claim 16, which is characterized in that the predetermined condition includes taking off, landing and described
It is one or more when height and distance change are more than predetermined threshold.
18. control device as claimed in claim 13, which is characterized in that the 4th control submodule includes：
Judging unit, for judging whether described make a return voyage a little overlaps with the aircraft in the horizontal direction；
First control unit, for it is described make a return voyage a little overlapped in the horizontal direction with the aircraft when control the aircraft
Make a return voyage idea icon described in the position Overlapping display of icon；And
Second control unit, for it is described make a return voyage a little misaligned with the aircraft in the horizontal direction when, maked a return voyage according to described
The direction of the relatively described aircraft of point, make a return voyage on the left line or right line of the horizontal line sub-icon described in display idea icon；
And/or the distance according to a little relatively described aircraft of making a return voyage, according to predetermined ratio, in the horizontal line sub-icon
Away from the idea icon that makes a return voyage described in display at the aircraft sub-icon respective distance on left line or right line.
19. control device as claimed in claim 18, which is characterized in that
When it is described make a return voyage idea icon and the aircraft sub-icon Overlapping display when, the dot map that makes a return voyage be marked with mark letter or
The form of mark word is shown in the aircraft sub-icon；
Otherwise, the idea icon that makes a return voyage includes figure and the mark letter in the figure or mark word.
20. control device as claimed in claim 13, which is characterized in that the posture dynamic icon includes angle sub-icon,
The flight attitude includes the pitch angle of the holder of the aircraft, and the first adjustment module includes：
5th adjustment submodule, for adjusting the angle sub-icon according to the pitch angle of the holder.
21. control device as claimed in claim 20, which is characterized in that the angle sub-icon include graduation mark and with it is described
The corresponding angular values of graduation mark, the angular values are shown in the side of the graduation mark.
22. control device as claimed in claim 21, which is characterized in that the graduation mark includes solid line and dotted line, the angle
Number of degrees value includes positive-angle numerical value and negative angle numerical value, and the solid line is corresponding with the positive-angle numerical value, the dotted line with it is described
Negative angle numerical value corresponds to.
23. control device as claimed in claim 22, which is characterized in that the angle sub-icon includes a datum line, institute
It states solid line and is parallel to the datum line with the dotted line, as the length of the increase solid line of the positive-angle numerical value gradually contracts
It is short, as the length of the increase dotted line of the negative angle numerical value is gradually shortened.
24. control device as claimed in claim 13, which is characterized in that the posture dynamic icon include aircraft sub-icon,
Horizontal line sub-icon and angle sub-icon, the flight attitude include the direction of the aircraft, the aircraft fuselage incline
The pitch angle of the holder of tilted direction and standard of fuselage degree and the aircraft, the first adjustment module include：
5th adjustment submodule, for adjusting the angle sub-icon according to the pitch angle of the holder；
6th adjustment submodule, for adjusting being oriented towards front of the aircraft sub-icon；And
7th adjustment submodule, adjusts the horizontal line subgraph and is designated as fully horizontally.
25. a kind of electronic device, which is characterized in that the electronic device includes：
Display；
For the communication module with aircraft communication；And
Control device as described in claim 13-24 any one.
26. electronic device as claimed in claim 25, which is characterized in that the electronic device includes remote controler, mobile phone, tablet
The one or more of computer, smartwatch, intelligent glasses and intelligent helmet.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2016/100366 WO2018058311A1 (en) | 2016-09-27 | 2016-09-27 | Control method, control device, and electronic device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106796481A CN106796481A (en) | 2017-05-31 |
| CN106796481B true CN106796481B (en) | 2018-09-07 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201680002582.4A Expired - Fee Related CN106796481B (en) | 2016-09-27 | 2016-09-27 | Control method, control device and electronic device |
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| Country | Link |
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| CN (1) | CN106796481B (en) |
| WO (1) | WO2018058311A1 (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107168355A (en) * | 2017-06-22 | 2017-09-15 | 李宇昊 | Unmanned vehicle course line determines method and apparatus |
| CN108304244B (en) * | 2018-02-24 | 2021-12-28 | 北京车和家信息技术有限公司 | Method and device for displaying vehicle-mounted system interface |
| US10964106B2 (en) * | 2018-03-30 | 2021-03-30 | Cae Inc. | Dynamically modifying visual rendering of a visual element comprising pre-defined characteristics |
| DE102018120675A1 (en) * | 2018-08-23 | 2020-02-27 | Autel Robotics Europe Gmbh | Method, device and system for operating a waypoint, ground station and computer-readable storage medium |
| CN110223565B (en) * | 2019-06-25 | 2022-02-22 | 深圳市道通智能航空技术股份有限公司 | Flight simulation method, device, equipment and storage medium |
| CN110730301B (en) * | 2019-10-14 | 2021-06-04 | 深圳市施罗德工业集团有限公司 | Head adjusting method and device, electronic equipment and storage medium |
| CN112752119B (en) * | 2019-10-31 | 2023-12-01 | 中兴通讯股份有限公司 | Delay error correction method, terminal equipment, server and storage medium |
| CN112540708A (en) * | 2020-12-17 | 2021-03-23 | 中国联合网络通信集团有限公司 | Network information display method and device, electronic equipment and storage medium |
| CN114035600A (en) * | 2021-11-30 | 2022-02-11 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle monitoring method, terminal and readable storage medium |
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| CN101493699A (en) * | 2009-03-04 | 2009-07-29 | 北京航空航天大学 | Aerial unmanned plane ultra-viewing distance remote control method |
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| EP0224278B1 (en) * | 1985-11-20 | 1991-05-08 | The Boeing Company | Apparatus for generating an aircraft situation display |
| JP2004268730A (en) * | 2003-03-07 | 2004-09-30 | Yamaha Motor Co Ltd | Attitude control method for unmanned helicopter |
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| CN102854887A (en) * | 2012-09-06 | 2013-01-02 | 北京工业大学 | Unmanned plane route planning and remote synchronous control method |
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| CN101493699A (en) * | 2009-03-04 | 2009-07-29 | 北京航空航天大学 | Aerial unmanned plane ultra-viewing distance remote control method |
| US8917322B2 (en) * | 2011-04-01 | 2014-12-23 | Lockheed Martin Corporation | Method and apparatus for digital video latency reduction by real-time warping |
| CN105912288A (en) * | 2016-04-12 | 2016-08-31 | 上海易天无人飞行器科技有限公司 | Method and system for comprehensive processing display capable of monitoring flight state of unmanned aerial vehicle |
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| WO2018058311A1 (en) | 2018-04-05 |
| CN106796481A (en) | 2017-05-31 |
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