WO2018058314A1 - 控制方法、控制装置及电子装置 - Google Patents
控制方法、控制装置及电子装置 Download PDFInfo
- Publication number
- WO2018058314A1 WO2018058314A1 PCT/CN2016/100369 CN2016100369W WO2018058314A1 WO 2018058314 A1 WO2018058314 A1 WO 2018058314A1 CN 2016100369 W CN2016100369 W CN 2016100369W WO 2018058314 A1 WO2018058314 A1 WO 2018058314A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- display
- control
- progress bar
- aircraft
- remaining
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims abstract description 54
- 238000004891 communication Methods 0.000 claims abstract description 22
- 230000000694 effects Effects 0.000 claims description 11
- 239000004984 smart glass Substances 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 12
- 230000006870 function Effects 0.000 description 8
- 230000007423 decrease Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000003491 array Methods 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000003190 augmentative effect Effects 0.000 description 1
- TZCXTZWJZNENPQ-UHFFFAOYSA-L barium sulfate Chemical compound [Ba+2].[O-]S([O-])(=O)=O TZCXTZWJZNENPQ-UHFFFAOYSA-L 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000012447 hatching Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
- G05D1/0022—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement characterised by the communication link
-
- 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
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/004—Indicating the operating range of the engine
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/008—Registering or indicating the working of vehicles communicating information to a remotely located station
Definitions
- the present invention relates to consumer electronics technology, and more particularly to a control method, a control device, and an electronic device.
- Embodiments of the present invention aim to solve at least one of the technical problems existing in the prior art. To this end, embodiments of the present invention are required to provide a control method, a control device, and an electronic device.
- the present invention provides a control method for controlling an electronic device;
- the electronic device includes a display and a communication module, the communication module is configured to communicate with an aircraft; and the control method includes the following steps:
- the feedback information includes the remaining flight time
- the step of acquiring the remaining flight time of the aircraft according to the feedback information is by reading the remaining flight time in the feedback information to realise.
- the aircraft includes a battery
- the feedback information includes remaining battery capacity and flight parameters of the battery
- the step of acquiring the remaining flight time of the aircraft based on the feedback information includes the following sub-steps:
- the remaining flight time is estimated based on the remaining power and the flight parameters.
- the progress bar is stepped and becomes shorter as the remaining flight time is shortened.
- the progress bar changes in a gradation.
- the step of controlling the display to display a progress bar and displaying the remaining flight time in conjunction with the progress bar comprises the following sub-steps:
- the step of controlling the display to display a progress bar and displaying the remaining flight time in conjunction with the progress bar further comprises the following sub-steps:
- the step of controlling the display to display a progress bar and displaying the remaining flight time in conjunction with the progress bar further comprises the following sub-steps:
- Controlling the display proximate to the progress icon displays a time icon corresponding to the remaining flight time.
- control method comprises the steps of:
- the step of controlling the display to cooperate with the progress bar to display the safe return time includes:
- the display is controlled to display a return icon at a position corresponding to the progress bar and the safe return time.
- the step of controlling the display to display the return icon at the position corresponding to the progress bar and the safe return time includes:
- the safe return time of the aircraft is estimated in real time according to the current flight environment of the aircraft and the current condition of the aircraft, and the return icon is displayed at a corresponding position of the progress bar.
- the aircraft includes a battery
- the feedback information includes a remaining amount of the battery.
- the control method further includes:
- the display is controlled to display the remaining power.
- the present invention also provides a control device for controlling an electronic device, the electronic device comprising a display and a communication module, the communication module for communicating with an aircraft; the control device comprising:
- a first acquiring module configured to acquire feedback information of the aircraft received by the communication module
- a second acquiring module configured to acquire, according to the feedback information, a remaining flight time of the aircraft
- a first control module configured to control the display to display a progress bar and display the remaining flight time in conjunction with the progress bar.
- the feedback information includes the remaining flight time
- the second acquisition module is configured to read the remaining flight time in the feedback information to implement acquiring the aircraft according to the feedback information. The remaining flight time.
- the aircraft includes a battery
- the feedback information includes remaining battery capacity and flight parameters of the battery
- the first control module includes:
- An estimation submodule for estimating the remaining flight time based on the remaining power and the flight parameters.
- the progress bar is stepped and becomes shorter as the remaining flight time is shortened.
- the progress bar changes in a gradation.
- the first control module comprises:
- a first control submodule configured to control the display to display an outline of the progress bar
- a second control submodule configured to control the display to display a dynamic effect icon moving along a length direction of the progress bar within a contour of the progress bar.
- the first control module further includes:
- a third control submodule configured to control the display to display a progress icon at a position corresponding to the remaining flight time under the progress bar.
- the first control module further includes:
- a fourth control submodule configured to control the display to display a time icon corresponding to the remaining flight time near the progress icon.
- control device further includes:
- a third acquiring module configured to acquire a safe return time of the aircraft according to the feedback information
- a second control module configured to control the display to display the safe return time in conjunction with the progress bar.
- the second control module comprises:
- a first control submodule configured to control the display to display a return navigation icon at a position corresponding to the progress bar and the safe return time.
- the first control sub-module is configured to estimate a safe return time of the aircraft in real time according to the current flight environment of the aircraft and the current condition of the aircraft, and display the corresponding position of the progress bar.
- the return flight icon is configured to estimate a safe return time of the aircraft in real time according to the current flight environment of the aircraft and the current condition of the aircraft, and display the corresponding position of the progress bar. The return flight icon.
- the aircraft includes a battery
- the feedback information includes a remaining amount of the battery
- the control device further includes:
- a third control module configured to control the display to display the remaining power.
- the invention also provides an electronic device comprising:
- a communication module for communicating with the aircraft
- the electronic device includes one or more of a remote control, a mobile phone, a tablet, a smart watch, smart glasses, and a smart helmet.
- control method, the control device, and the electronic device control display in the embodiment of the present invention intelligently display the remaining flight time of the monitored or manipulated aircraft, so that the user can effectively plan the route according to the remaining flight time. Improve the user experience.
- FIG. 1 is a flow chart of a control method of some embodiments of the present invention.
- FIG. 2 is a schematic diagram of functional modules of an electronic device and a control device according to some embodiments of the present invention.
- FIG. 3 is a schematic diagram of an electronic device and an aircraft of some embodiments of the present invention.
- FIG. 4 is a flow chart of a control method of some embodiments of the present invention.
- FIG. 5 is a schematic diagram of functional modules of an electronic device and a control device according to some embodiments of the present invention.
- FIG. 6 is a flow chart of a control method of some embodiments of the present invention.
- FIG. 7 is a functional block diagram of an electronic device and a control device according to some embodiments of the present invention.
- FIG. 8 is a flow chart of a control method of some embodiments of the present invention.
- FIG. 9 is a schematic diagram of functional modules of an electronic device and a control device according to some embodiments of the present invention.
- FIG. 10 is a flow chart of a control method of some embodiments of the present invention.
- FIG. 11 is a schematic diagram of functional modules of an electronic device and a control device according to some embodiments of the present invention.
- FIG. 12 is a flow chart of a control method of some embodiments of the present invention.
- FIG. 13 is a schematic diagram of functional blocks of an electronic device and a control device according to some embodiments of the present invention.
- FIG. 14 is a flow diagram of a control method of some embodiments of the present invention.
- 15 is a functional block diagram of an electronic device and a control device according to some embodiments of the present invention.
- 16 is a flow chart of a control method of some embodiments of the present invention.
- 17 is a functional block diagram of an electronic device and a control device according to some embodiments of the present invention.
- FIG. 18 is a schematic diagram of a display interface of a display of an electronic device according to some embodiments of the present invention.
- 19 is a schematic diagram of a control display display progress bar and a progress bar showing remaining flight time in accordance with some embodiments of the present invention.
- 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.
- features defining “first” or “second” may include one or more of the described features either explicitly or implicitly.
- the meaning of "a plurality" is two or more unless specifically and specifically defined otherwise.
- connection 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 integrally connected; may be mechanically connected, or may be electrically connected or may communicate with each other; may be directly connected or indirectly connected through an intermediate medium, may be internal communication of two elements or interaction of two elements relationship. 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.
- a control method is used to control an electronic device 100 .
- the electronic device 100 includes a display 101 and a communication module 102 , and the communication module 102 is configured to communicate with the aircraft 200 .
- Control methods include:
- control display 101 displays the progress bar 103 and the progress bar 103 to display the remaining flight time.
- the control device 110 includes a first obtaining module 111, a second obtaining module 112, and a first control module 113, which can be used to implement S1, S2, and S3, respectively. That is, the first obtaining module 111 is configured to acquire feedback information of the aircraft 200 received by the communication module 102.
- the second acquisition module 112 is configured to acquire the remaining flight time of the aircraft 200 according to the feedback information.
- the first control module 113 is configured to control the display 101 to display the progress bar 103 and the progress bar 103 to display the remaining flight time.
- the control device 110 of the embodiment of the present invention can be applied to the electronic device 100 of the embodiment of the present invention.
- the electronic device 100 in this embodiment is a tablet computer.
- the electronic device 100 may further include a mobile phone, a remote controller, a smart watch, smart glasses, One or more of display terminals having display functions such as smart helmets, other virtual reality wearable devices, and other augmented reality wearable devices.
- the display 101 is used to display information related to monitoring or operating the aircraft 200, such as parameter information of the aircraft itself, flight information, images taken by the aircraft 200, or video pictures.
- the user can visually understand the remaining flight time of the aircraft 200 being monitored or manipulated by observing the progress bar 103 displayed in the display 101 and the remaining flight time displayed in conjunction with the progress bar 103.
- control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 101 to intelligently display the remaining flight time of the aircraft 200 being monitored or manipulated, so that the user can effectively plan the route and the task according to the remaining flight time, and improve The user experience.
- the feedback information includes the remaining time of flight
- the step of acquiring the remaining time of flight of the aircraft 200 based on the feedback information is accomplished by reading the remaining time of flight in the feedback information.
- the aircraft 200 includes a battery
- the feedback information includes the remaining battery capacity and flight parameters
- the step of acquiring the remaining flight time of the aircraft 200 according to the feedback information includes the following: step:
- the second obtaining module 112 of the control device 110 includes an estimating submodule 1121, which can be used to implement S201. That is, the estimation sub-module 1121 is configured to estimate the remaining flight time based on the remaining power and flight parameters.
- the progress bar 103 is stepped and becomes shorter as the remaining flight time is shortened.
- the progress bar 103 includes three rectangles that are sequentially connected, and the height of each rectangle is sequentially shortened.
- the progress bar 103 can also have other shapes, such as a long column, a triangle, an arrow, and the like.
- the progress bar 103 changes in a gradation.
- the color of the progress bar 103 changes from light to dark, or from deep to light, or from one color to another.
- the colors of the three rectangles in FIG. 18 may be yellow, orange, or red, respectively.
- the step of controlling the display 101 to display the progress bar 103 and the progress bar 103 to display the remaining flight time includes the following sub-steps:
- control display 101 displays the outline of the progress bar 103.
- the control display 101 displays a dynamic effect icon moving in the longitudinal direction of the progress bar 103 within the outline of the progress bar 103.
- the first control module 113 of the control device 110 includes a first control submodule 1131 and a second control submodule 1132, which can be used to implement S301 and S302, respectively. That is, the first control sub-module 1131 is for controlling the display 101 to display the outline of the progress bar 103.
- the second control sub-module 1132 is for controlling the display 101 to display the dynamic effect of moving along the length direction of the progress bar 103 within the outline of the progress bar 103. icon.
- the dynamic effect icon can be simply a columnar fill that moves from left to right, similar to a bar when installing a file on a computer.
- the dynamic effect icon may also be a plurality of oblique lines (similar to the hatching within the contour) which are distributed parallel to each other in parallel with each other, and the first control sub-module 1131 controls a plurality of oblique lines to exhibit a dynamic movement effect, especially in When the progress bar 103 changes in a gradient color, the dynamic movement effect is more obvious.
- control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 101 to intelligently display the remaining flight time of the monitored or manipulated aircraft 200 and present a dynamic effect, further improving the user experience.
- the step of controlling the display 101 to display the progress bar 103 and the progress progress bar 103 to display the remaining flight time further includes the following sub-steps:
- the control display 101 displays the progress icon 104 at a position corresponding to the remaining flight time under the progress bar 103.
- the first control module 113 of the control device 110 includes a third control sub-module 1133, which can be used to implement S303. That is, the third control sub-module 1133 is for controlling the display 101 to display the progress icon 104 at a position corresponding to the remaining flight time under the progress bar 103.
- the progress icon 104 in this embodiment is a triangle. It can be understood that in other embodiments, the progress icon 104 can also be an arrow, a finger shape, a long rectangle, a circle, an ellipse, and the like.
- the progress icon 104 moves along the length direction of the progress bar 103 as the remaining flight time decreases. In the present embodiment, the progress icon 104 shifts to the right along the length direction of the progress bar 103 as the remaining flight time decreases.
- the step of controlling the display 101 to display the progress bar 103 and the matching progress bar 103 to display the remaining flight time further includes the following sub-steps:
- control display 101 displays a time icon 105 corresponding to the remaining flight time near the progress icon 104.
- the first control module 113 of the control device 110 includes a fourth control sub-module 1134, which can be used to implement S304. That is, the fourth control sub-module 1134 is for controlling the display 101 to display the time icon 105 corresponding to the remaining flight time near the progress icon 104.
- the time icon 105 in the present embodiment includes the remaining time value.
- the user can learn from the progress bar and the remaining flight time in FIG. 18 that the aircraft 200 monitored or controlled by the user can continue to fly. 9:29 second.
- the time icon 105 is located to the right of the progress icon 104 and gradually becomes smaller as the time of flight of the drone 200 increases. It can be understood that in other embodiments, the time icon 105 can also be disposed at a position on the left side, above or below the progress icon 104. The time icon 105 moves along the length direction of the progress bar 103 as the remaining flight time decreases. In the present embodiment, the time icon 105 moves right along with the progress icon 104 along the length direction of the progress bar 103 as the remaining flight time decreases. .
- the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 101 to intelligently display the remaining flight time of the monitored or manipulated aircraft 200 and present a time icon 105 reflecting the specific remaining flight time, further improving The user experience.
- control method further includes:
- control display 101 cooperates with the progress bar 103 to display the safe return time.
- the control device 110 further includes a third obtaining module 114 and a second control module 115, which can be used to implement S4 and S5, respectively. That is, the third obtaining module 114 is configured to acquire the safe return time of the aircraft 200 according to the feedback information.
- the second control module 115 is configured to control the display 101 to display the safe return time in conjunction with the progress bar 103.
- the third rectangle in the stepped strip 103 indicates the safe return time.
- the safe return time of the aircraft 200 of each model is a fixed value, and the safe return time is determined by factors such as the maximum flight range and maximum flight power of the aircraft 200 from the control point where the user is located.
- the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 101 to intelligently display the remaining flight time of the aircraft 200 being monitored or manipulated, and intelligently display the safe return time of the aircraft 200 to remind The user can return to the flight as quickly as possible to avoid a crash or insufficient power to return to the takeoff point, further enhancing the user experience.
- the step of controlling the display 101 to cooperate with the progress bar 103 to display the safe return time includes the following sub-steps:
- the control display 101 displays the return icon 106 at a position corresponding to the safe return time of the progress bar 103.
- the display display 101 displays the returning icon 106 at the position corresponding to the safe returning time of the progress bar 103.
- the safety returning time of the aircraft 200 may be estimated in real time according to the current flight environment of the aircraft 200 and the current condition of the aircraft 200, and the corresponding in the progress bar 103.
- the location displays the return icon 106.
- the second control module 115 of the control device 110 includes a second control sub-module 1151, which can be used to implement S501. That is, the second control sub-module 1151 is configured to control the display 101 to display the return icon 106 at a position corresponding to the progress bar 103 and the safe return time. Further, the second control sub-module 1151 is configured to estimate the safe return time of the aircraft 200 in real time according to the current flight environment of the aircraft 200 and the current condition of the aircraft 200, and display the return icon 106 at the corresponding position of the progress bar 103.
- the return icon 106 is a circle and a letter H in the circle, which is defined as the HOME point. Since the safe return time of the aircraft 200 of each model is a fixed value, the position of the returning icon 106 does not change, that is, the position of the HOME point does not change. When the progress icon 104 moves below the HOME point, it indicates that the user needs to return to the flight. If the flight is not returned, the aircraft 200 is not enough to fly back to the user's control. Point, prone to crashes. The remaining time value displayed by the time icon 105 at this time is the safe return time.
- the aircraft 200 includes a battery, and the feedback information includes a remaining battery power.
- the control method further includes:
- control display 101 displays the remaining power.
- the control device 110 further includes a third control module 116, which can be used to implement S6. That is, the third control module 116 is used to control the display 101 to display the remaining power.
- the third control module 116 is configured to control the display 101 to display the remaining power in the upper right corner, which is 50%.
- control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 101 to intelligently display the remaining flight time of the aircraft 200 being monitored or manipulated, and intelligently display the remaining power of the aircraft 200, thereby further improving The user experience.
- 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.
- 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).
- the computer readable medium may even be a paper or other suitable medium on which the program can be printed. Quality, because the program can be obtained electronically, for example by optical scanning of paper or other media, followed by editing, interpretation or, if necessary, processing in other suitable manner, and then storing it in a computer memory.
- portions of the invention may be implemented in hardware, software, firmware or a combination thereof.
- multiple steps or methods may be implemented in software or firmware stored in a memory and executed by a suitable instruction execution system.
- a suitable instruction execution system For example, if implemented in hardware, as in another embodiment, it can be implemented by any one or combination of the following techniques well known in the art: having logic gates for implementing 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.
- 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 modules can be implemented in the form of hardware or in the form of software functional modules.
- the integrated modules, if implemented in the form of software functional modules and sold or used as stand-alone 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.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- General Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Human Computer Interaction (AREA)
- User Interface Of Digital Computer (AREA)
- Traffic Control Systems (AREA)
Abstract
一种控制方法、控制装置(110)及电子装置(100)。控制方法用于控制电子装置(100)。电子装置(100)包括显示器(101)及通信模块(102)。通信模块(102)用于与飞行器(200)通信。控制方法包括:(S1)获取通信模块(102)接收的飞行器(200)的反馈信息;(S2)根据反馈信息获取飞行器(200)的剩余飞行时间;及(S3)控制显示器(101)显示进度条(103)及配合进度条(103)显示剩余飞行时间。
Description
本发明涉及消费性电子技术,特别涉及一种控制方法、控制装置及电子装置。
随着科技的不断发展,手机、平板电脑等电子设备的应用越来越广泛,如应用于远程监控或操控飞行器等。目前,在电子设备远程监控或操控飞行器时,只能从电子设备的显示界面中观察到飞行器的剩余电量,比如电量只剩下70%、60%、或50%等,而从飞行器的剩余电量并不能知道飞行器还能继续飞行的时间(剩余飞行时间),用户也就无法有效地规划航线及任务,导致用户体验不佳。
发明内容
本发明的实施方式旨在至少解决现有技术中存在的技术问题之一。为此,本发明的实施方式需要提供一种控制方法、控制装置及电子装置。
本发明提供一种控制方法,用于控制电子装置;所述电子装置包括显示器及通信模块,所述通信模块用于与飞行器通信;所述控制方法包括以下步骤:
获取所述通信模块接收的所述飞行器的反馈信息;
根据所述反馈信息获取所述飞行器的剩余飞行时间;及
控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间。
在某些实施方式中,所述反馈信息包括所述剩余飞行时间,所述根据所述反馈信息获取所述飞行器的剩余飞行时间的步骤是通过在所述反馈信息中读取所述剩余飞行时间来实现。
在某些实施方式中,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量及飞行参数,所述根据所述反馈信息获取所述飞行器的剩余飞行时间的步骤包括以下子步骤:
根据所述剩余电量及所述飞行参数估算所述剩余飞行时间。
在某些实施方式中,所述进度条呈阶梯状,并随着所述剩余飞行时间缩短逐阶变矮。
在某些实施方式中,所述进度条呈渐变色变化。
在某些实施方式中,所述控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间的步骤包括以下子步骤:
控制所述显示器显示所述进度条的轮廓;及
控制所述显示器在所述进度条的轮廓内显示沿所述进度条的长度方向移动的动态效果
图标。
在某些实施方式中,所述控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间的步骤还包括以下子步骤:
控制所述显示器在所述进度条下与所述剩余飞行时间对应的位置显示进度图标。
在某些实施方式中,所述控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间的步骤还包括以下子步骤:
控制所述显示器靠近所述进度图标显示与所述剩余飞行时间对应的时间图标。
在某些实施方式中,所述控制方法包括以下步骤:
根据所述反馈信息获取所述飞行器的安全返航时间;及
控制所述显示器配合所述进度条显示所述安全返航时间。
在某些实施方式中,所述控制所述显示器配合所述进度条显示所述安全返航时间的步骤包括:
控制所述显示器在所述进度条与所述安全返航时间对应的位置显示返航图标。
所述控制所述显示器在所述进度条与所述安全返航时间对应的位置显示返航图标的步骤包括:
根据所述飞行器当前飞行环境以及所述飞行器当前的状况实时估算所述飞行器的安全返航时间,并在所述进度条的对应位置显示所述返航图标。
在某些实施方式中,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量,所述控制方法还包括:
控制所述显示器显示所述剩余电量。
本发明还提供一种控制装置,用于控制电子装置,所述电子装置包括显示器及通信模块,所述通信模块用于与飞行器通信;所述控制装置包括:
第一获取模块,用于获取所述通信模块接收的所述飞行器的反馈信息;
第二获取模块,用于根据所述反馈信息获取所述飞行器的剩余飞行时间;及
第一控制模块,用于控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间。
在某些实施方式中,所述反馈信息包括所述剩余飞行时间,所述第二获取模块用于在所述反馈信息中读取所述剩余飞行时间以实现根据所述反馈信息获取所述飞行器的剩余飞行时间。
在某些实施方式中,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量及飞行参数,所述第一控制模块包括:
估算子模块,用于根据所述剩余电量及所述飞行参数估算所述剩余飞行时间。
在某些实施方式中,所述进度条呈阶梯状,并随着所述剩余飞行时间缩短逐阶变矮。
在某些实施方式中,所述进度条呈渐变色变化。
在某些实施方式中,所述第一控制模块包括:
第一控制子模块,用于控制所述显示器显示所述进度条的轮廓;及
第二控制子模块,用于控制所述显示器在所述进度条的轮廓内显示沿所述进度条的长度方向移动的动态效果图标。
在某些实施方式中,所述第一控制模块还包括:
第三控制子模块,用于控制所述显示器在所述进度条下与所述剩余飞行时间对应的位置显示进度图标。
在某些实施方式中,所述第一控制模块还包括:
第四控制子模块,用于控制所述显示器靠近所述进度图标显示与所述剩余飞行时间对应的时间图标。
在某些实施方式中,所述控制装置还包括:
第三获取模块,用于根据所述反馈信息获取所述飞行器的安全返航时间;及
第二控制模块,用于控制所述显示器配合所述进度条显示所述安全返航时间。
在某些实施方式中,所述第二控制模块包括:
第一控制子模块,用于控制所述显示器在所述进度条与所述安全返航时间对应的位置显示返航图标。
在某些实施方式中,所述第一控制子模块用于根据所述飞行器当前飞行环境以及所述飞行器当前的状况实时估算所述飞行器的安全返航时间,并在所述进度条的对应位置显示所述返航图标。
在某些实施方式中,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量,所述控制装置还包括:
第三控制模块,用于控制所述显示器显示所述剩余电量。
本发明还提供一种电子装置,包括:
显示器;
用于与飞行器通信的通信模块;及
如上实施方式所述的控制装置。
在某些实施方式中,所述电子装置包括遥控器、手机、平板电脑、智能手表、智能眼镜及智能头盔的一种或者多种。
本发明实施方式中的控制方法、控制装置、及电子装置控制显示器智能地显示被监控或操控的飞行器的剩余飞行时间,使得用户能够根据剩余飞行时间有效地规划航线及任
务,提升了用户体验。
本发明的实施方式的附加方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本发明的实施方式的实践了解到。
本发明的上述和/或附加的方面和优点从结合下面附图对实施方式的描述中将变得明显和容易理解,其中:
图1是本发明某些实施方式的控制方法的流程示意图。
图2是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图3是本发明某些实施方式的电子装置及飞行器的实物示意图。
图4是本发明某些实施方式的控制方法的流程示意图。
图5是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图6是本发明某些实施方式的控制方法的流程示意图。
图7是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图8是本发明某些实施方式的控制方法的流程示意图。
图9是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图10是本发明某些实施方式的控制方法的流程示意图。
图11是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图12是本发明某些实施方式的控制方法的流程示意图。
图13是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图14是本发明某些实施方式的控制方法的流程示意图。
图15是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图16是本发明某些实施方式的控制方法的流程示意图。
图17是本发明某些实施方式的电子装置及控制装置的功能模块示意图。
图18是本发明某些实施方式的电子装置的显示器显示界面的示意图。
图19是本发明某些实施方式的控制显示器显示进度条及配合进度条显示剩余飞行时间的示意图。
下面详细描述本发明的实施方式,所述实施方式的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施方式是示例性的,仅用于解释本发明,而不能理解为对本发明的限制。
在本发明的描述中,需要理解的是,术语“第一”、“第二”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括一个或者更多个所述特征。在本发明的描述中,“多个”的含义是两个或两个以上,除非另有明确具体的限定。
在本发明的描述中,需要说明的是,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是机械连接,也可以是电连接或可以相互通信;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明中的具体含义。
下文的公开提供了许多不同的实施方式或例子用来实现本发明的不同结构。为了简化本发明的公开,下文中对特定例子的部件和设置进行描述。当然,它们仅仅为示例,并且目的不在于限制本发明。此外,本发明可以在不同例子中重复参考数字和/或参考字母,这种重复是为了简化和清楚的目的,其本身不指示所讨论各种实施方式和/或设置之间的关系。此外,本发明提供了的各种特定的工艺和材料的例子,但是本领域普通技术人员可以意识到其他工艺的应用和/或其他材料的使用。
下面详细描述本发明的实施方式,所述实施方式的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施方式是示例性的,仅用于解释本发明,而不能理解为对本发明的限制。
请一并参阅图1-3及图18,本发明实施方式的控制方法,用于控制电子装置100,电子装置100包括显示器101及通信模块102,通信模块102用于与飞行器200通信。控制方法包括:
S1,获取通信模块102接收的飞行器200的反馈信息;
S2,根据反馈信息获取飞行器200的剩余飞行时间;及
S3,控制显示器101显示进度条103及配合进度条103显示剩余飞行时间。
请参阅图2,在本发明实施方式的控制装置110中,控制装置110包括第一获取模块111、第二获取模块112、及第一控制模块113,可分别用于实现S1、S2及S3。也就是说,第一获取模块111用于获取通信模块102接收的飞行器200的反馈信息。第二获取模块112用于根据反馈信息获取飞行器200的剩余飞行时间。第一控制模块113用于控制显示器101显示进度条103及配合进度条103显示剩余飞行时间。
在本发明实施方式的控制装置110可应用于本发明实施方式的电子装置100。请参阅图3,本实施方式中的电子装置100为平板电脑。
在某些实施方式中,电子装置100还可包括手机、遥控器、智能手表、智能眼镜、
智能头盔、其他虚拟现实穿戴设备、其他增强现实穿戴设备等具有显示功能的显示终端中的一种或多种。显示器101用于显示监控或操作飞行器200的相关信息,例如飞行器自身的参数信息、飞行信息、经飞行器200拍摄的图像或视频画面。
请结合图18,用户可以通过观察显示器101中显示的进度条103及配合进度条103显示的剩余飞行时间来直观地了解被其监控或操控的飞行器200的剩余飞行时间。
本发明实施方式中的控制方法、控制装置110、及电子装置100控制显示器101智能地显示被监控或操控的飞行器200的剩余飞行时间,使得用户能够根据剩余飞行时间有效地规划航线及任务,提升了用户体验。
在某些实施方式中,反馈信息包括剩余飞行时间,根据反馈信息获取飞行器200的剩余飞行时间的步骤是通过在反馈信息中读取剩余飞行时间来实现的。
请一并参阅图4-5及图18,在某些实施方式中,飞行器200包括电池,反馈信息包括电池的剩余电量及飞行参数,根据反馈信息获取飞行器200的剩余飞行时间的步骤包括以下子步骤:
S201,根据剩余电量及飞行参数估算剩余飞行时间。
请参阅图5,在本发明实施方式的控制装置110中,控制装置110的第二获取模块112包括估算子模块1121,可用于实现S201。即估算子模块1121用于根据剩余电量及飞行参数估算剩余飞行时间。
请结合图18,在某些实施方式中,进度条103呈阶梯状,并随着剩余飞行时间缩短逐阶变矮。例如,进度条103包括顺序相接的三个长方形,每个长方形的高度依次变矮。请结合图19,进度条103还可呈其他形状,例如长条柱状、三角形、箭头形等。
在某些实施方式中,进度条103呈渐变色变化。换句话说,从左至右,进度条103的颜色从明到暗、或由深转浅、或是从一个色彩缓慢过渡到另一个色彩。例如,图18中的三个长方形的颜色可以分别为黄色、橙色、红色。
请一并参阅图3及图6-7,在某些实施方式中,控制显示器101显示进度条103及配合进度条103显示剩余飞行时间的步骤包括以下子步骤:
S301,控制显示器101显示进度条103的轮廓。
S302,控制显示器101在进度条103的轮廓内显示沿进度条103的长度方向移动的动态效果图标。
请参阅图7,在本发明实施方式的控制装置110中,控制装置110的第一控制模块113包括第一控制子模块1131及第二控制子模块1132,可分别用于实现S301及S302。也就是说,第一控制子模块1131用于控制显示器101显示进度条103的轮廓。第二控制子模块1132用于控制显示器101在进度条103的轮廓内显示沿进度条103的长度方向移动的动态效果
图标。
动态效果图标可以单纯的从左至右移动的柱状填充体,类似于在电脑上安装文件时的柱状条。动态效果图标还可以是若干彼此平行分布在轮廓内的斜线(类似于在轮廓内的剖面线),第一控制子模块1131控制若干斜线转动,便能呈现处动态的移动效果,尤其在进度条103呈渐变色变化时,动态的移动效果更为明显。
本发明实施方式中的控制方法、控制装置110、及电子装置100控制显示器101智能地显示被监控或操控的飞行器200的剩余飞行时间并呈现出动态效果,进一步地提升了用户体验。
请一并参阅图3、图8-9及图18,在某些实施方式中,控制显示器101显示进度条103及配合进度条103显示剩余飞行时间的步骤还包括以下子步骤:
S303,控制显示器101在进度条103下与剩余飞行时间对应的位置显示进度图标104。
请参阅图9,在本发明实施方式的控制装置110中,控制装置110的第一控制模块113包括第三控制子模块1133,可用于实现S303。也就是说,第三控制子模块1133用于控制显示器101在进度条103下与剩余飞行时间对应的位置显示进度图标104。
请结合图18,本实施方式中的进度图标104是三角形,可以理解,在其他实施方式中,进度图标104还可以是箭头、手指形、长条矩形、圆形、椭圆形等等形状。进度图标104随着剩余飞行时间的减少沿着进度条103的长度方向移动,本实施方式中,进度图标104随着剩余飞行时间的减少沿着进度条103的长度方向右移。
请一并参阅图3、图10-11及图18,在某些实施方式中,控制显示器101显示进度条103及配合进度条103显示剩余飞行时间的步骤还包括以下子步骤:
S304,控制显示器101靠近进度图标104显示与剩余飞行时间对应的时间图标105。
请参阅图11,在本发明实施方式的控制装置110中,控制装置110的第一控制模块113包括第四控制子模块1134,可用于实现S304。也就是说,第四控制子模块1134用于控制显示器101靠近进度图标104显示与剩余飞行时间对应的时间图标105。
请结合图18,本实施方式中的时间图标105包括剩余时间数值,例如,用户可以从图18中的进度条及剩余飞行时间了解到被其监控或操控的飞行器200还能继续飞行9分29秒。
时间图标105位于进度图标104的右侧,并随着无人机200的正在飞行的时间的增加而逐渐变小。可以理解,在其他实施方式中,时间图标105还可以设置在进度图标104的左侧、上方或下方等位置。时间图标105随着剩余飞行时间的减少沿着进度条103的长度方向移动,本实施方式中,时间图标105随着剩余飞行时间的减少沿着进度条103的长度方向与进度图标104一起右移。
本发明实施方式中的控制方法、控制装置110、及电子装置100控制显示器101智能地显示被监控或操控的飞行器200的剩余飞行时间并呈现出体现具体剩余飞行时间的时间图标105,进一步地提升了用户体验。
请一并参阅图3、图12-13及图18,在某些实施方式中,所述控制方法还包括:
S4,根据反馈信息获取飞行器200的安全返航时间;及
S5,控制显示器101配合进度条103显示安全返航时间。
请参阅图13,在本发明实施方式的控制装置110中,控制装置110还包括第三获取模块114及第二控制模块115,可分别用于实现S4及S5。也就是说,第三获取模块114用于根据反馈信息获取飞行器200的安全返航时间。第二控制模块115用于控制显示器101配合进度条103显示安全返航时间。
请结合图18,阶梯状的进图条103中的第三个长方形标示安全返航时间。在正常的飞行环境下,每种机型的飞行器200的安全返航时间为一固定值,安全返航时间由飞行器200距离用户所在的控制点的最大飞行范围与最大飞行功率等因素来决定。
本发明实施方式中的控制方法、控制装置110、及电子装置100控制显示器101除了智能地显示被监控或操控的飞行器200的剩余飞行时间,还能智能地显示飞行器200的安全返航时间,以提醒用户尽快返航以避免坠机或不够电量回到起飞点,从而进一步提升了用户体验。
请一并参阅图3、图14-15及图18,在某些实施方式中,控制显示器101配合进度条103显示安全返航时间的步骤包括以下子步骤:
S501,控制显示器101在进度条103与安全返航时间对应的位置显示返航图标106。
其中,控制显示器101在进度条103与安全返航时间对应的位置显示返航图标106可以是根据飞行器200当前飞行环境以及飞行器200当前的状况实时估算飞行器200的安全返航时间,并在进度条103的对应位置显示返航图标106。
请参阅图15,在本发明实施方式的控制装置110中,控制装置110的第二控制模块115包括第二控制子模块1151,可用于实现S501。即第二控制子模块1151用于控制显示器101在进度条103与安全返航时间对应的位置显示返航图标106。进一步地,第二控制子模块1151用于根据飞行器200当前飞行环境以及飞行器200当前的状况实时估算飞行器200的安全返航时间,并在进度条103的对应位置显示返航图标106。
请结合图18,在某些实施方式中,返航图标106为圆圈及位于圆圈内的字母标识H,此点定义为HOME点。由于每种机型的飞行器200的安全返航时间为一固定值,则返航图标106的位置不变,即HOME点的位置不变。当进度图标104移动到HOME点下方时,则表明用户需要返航了,若不返航,飞行器200就不够电量飞回用户所在的控制
点,容易发生坠机事故。此时时间图标105显示的剩余时间数值则是安全返航时间。
请一并参阅图3及图16-18,在某些实施方式中,飞行器200包括电池,反馈信息包括电池的剩余电量;所述控制方法还包括:
S6,控制显示器101显示剩余电量。
请参阅图17,在本发明实施方式的控制装置110中,控制装置110还包括第三控制模块116,可用于实现S6。也就是说,第三控制模块116用于控制显示器101显示剩余电量。
请结合图18,第三控制模块116用于控制显示器101显示剩余电量在右上角,为50%。
本发明实施方式中的控制方法、控制装置110、及电子装置100控制显示器101除了智能地显示被监控或操控的飞行器200的剩余飞行时间,还能智能地显示飞行器200的剩余电量,从而进一步提升了用户体验。
本发明实施方式的电子装置100中未展开的其它部分,可参阅以上实施方式的控制方法或控制装置110的对应部分,在此不再详细展开。
在本说明书的描述中,参考术语“一个实施方式”、“一些实施方式”、“示意性实施方式”、“示例”、“具体示例”、或“一些示例”等的描述意指结合所述实施方式或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施方式或示例中。在本说明书中,对上述术语的示意性表述不一定指的是相同的实施方式或示例。而且,描述的具体特征、结构、材料或者特点可以在任何的一个或多个实施方式或示例中以合适的方式结合。
流程图中或在此以其他方式描述的任何过程或方法描述可以被理解为,表示包括一个或更多个用于实现特定逻辑功能或过程的步骤的可执行指令的代码的模块、片段或部分,并且本发明的优选实施方式的范围包括另外的实现,其中可以不按所示出或讨论的顺序,包括根据所涉及的功能按基本同时的方式或按相反的顺序,来执行功能,这应被本发明的实施例所属技术领域的技术人员所理解。
在流程图中表示或在此以其他方式描述的逻辑和/或步骤,例如,可以被认为是用于实现逻辑功能的可执行指令的定序列表,可以具体实现在任何计算机可读介质中,以供指令执行***、装置或设备(如基于计算机的***、包括处理器的***或其他可以从指令执行***、装置或设备取指令并执行指令的***)使用,或结合这些指令执行***、装置或设备而使用。就本说明书而言,"计算机可读介质"可以是任何可以包含、存储、通信、传播或传输程序以供指令执行***、装置或设备或结合这些指令执行***、装置或设备而使用的装置。计算机可读介质的更具体的示例(非穷尽性列表)包括以下:具有一个或多个布线的电连接部(电子装置),便携式计算机盘盒(磁装置),随机存取存储器(RAM),只读存储器(ROM),可擦除可编辑只读存储器(EPROM或闪速存储器),光纤装置,以及便携式光盘只读存储器(CDROM)。另外,计算机可读介质甚至可以是可在其上打印所述程序的纸或其他合适的介
质,因为可以例如通过对纸或其他介质进行光学扫描,接着进行编辑、解译或必要时以其他合适方式进行处理来以电子方式获得所述程序,然后将其存储在计算机存储器中。
应当理解,本发明的各部分可以用硬件、软件、固件或它们的组合来实现。在上述实施方式中,多个步骤或方法可以用存储在存储器中且由合适的指令执行***执行的软件或固件来实现。例如,如果用硬件来实现,和在另一实施方式中一样,可用本领域公知的下列技术中的任一项或他们的组合来实现:具有用于对数据信号实现逻辑功能的逻辑门电路的离散逻辑电路,具有合适的组合逻辑门电路的专用集成电路,可编程门阵列(PGA),现场可编程门阵列(FPGA)等。
本技术领域的普通技术人员可以理解实现上述实施方法携带的全部或部分步骤是可以通过程序来指令相关的硬件完成,所述的程序可以存储于一种计算机可读存储介质中,该程序在执行时,包括方法实施例的步骤之一或其组合。
此外,在本发明各个实施例中的各功能单元可以集成在一个处理模块中,也可以是各个单元单独物理存在,也可以两个或两个以上单元集成在一个模块中。上述集成的模块既可以采用硬件的形式实现,也可以采用软件功能模块的形式实现。所述集成的模块如果以软件功能模块的形式实现并作为独立的产品销售或使用时,也可以存储在一个计算机可读取存储介质中。
上述提到的存储介质可以是只读存储器,磁盘或光盘等。尽管上面已经示出和描述了本发明的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本发明的限制,本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型。
Claims (26)
- 一种控制方法,用于控制电子装置,所述电子装置包括显示器及通信模块,所述通信模块用于与飞行器通信,其特征在于,所述控制方法包括以下步骤:获取所述通信模块接收的所述飞行器的反馈信息;根据所述反馈信息获取所述飞行器的剩余飞行时间;及控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间。
- 如权利要求1所述的控制方法,其特征在于,所述反馈信息包括所述剩余飞行时间,所述根据所述反馈信息获取所述飞行器的剩余飞行时间的步骤是通过在所述反馈信息中读取所述剩余飞行时间来实现。
- 如权利要求1所述的控制方法,其特征在于,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量及飞行参数,所述根据所述反馈信息获取所述飞行器的剩余飞行时间的步骤包括以下子步骤:根据所述剩余电量及所述飞行参数估算所述剩余飞行时间。
- 如权利要求1所述的控制方法,其特征在于,所述进度条呈阶梯状,并随着所述剩余飞行时间缩短逐阶变矮。
- 如权利要求1所述的控制方法,其特征在于,所述进度条呈渐变色变化。
- 如权利要求1-5任意一项所述的控制方法,其特征在于,所述控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间的步骤包括以下子步骤:控制所述显示器显示所述进度条的轮廓;及控制所述显示器在所述进度条的轮廓内显示沿所述进度条的长度方向移动的动态效果图标。
- 如权利要求6所述的控制方法,其特征在于,所述控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间的步骤还包括以下子步骤:控制所述显示器在所述进度条下与所述剩余飞行时间对应的位置显示进度图标。
- 如权利要求7所述的控制方法,其特征在于,所述控制所述显示器显示进度条及配 合所述进度条显示所述剩余飞行时间的步骤还包括以下子步骤:控制所述显示器靠近所述进度图标显示与所述剩余飞行时间对应的时间图标。
- 如权利要求1-5任意一项所述的控制方法,其特征在于,所述控制方法包括以下步骤:根据所述反馈信息获取所述飞行器的安全返航时间;及控制所述显示器配合所述进度条显示所述安全返航时间。
- 如权利要求9所述的控制方法,其特征在于,所述控制所述显示器配合所述进度条显示所述安全返航时间的步骤包括:控制所述显示器在所述进度条与所述安全返航时间对应的位置显示返航图标。
- 如权利要求10所述的控制方法,其特征在于,所述控制所述显示器在所述进度条与所述安全返航时间对应的位置显示返航图标的步骤包括:根据所述飞行器当前飞行环境以及所述飞行器当前的状况实时估算所述飞行器的安全返航时间,并在所述进度条的对应位置显示所述返航图标。
- 如权利要求1-5任意一项所述的控制方法,其特征在于,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量,所述控制方法还包括:控制所述显示器显示所述剩余电量。
- 一种控制装置,用于控制电子装置,所述电子装置包括显示器及通信模块,所述通信模块用于与飞行器通信,其特征在于,所述控制装置包括:第一获取模块,用于获取所述通信模块接收的所述飞行器的反馈信息;第二获取模块,用于根据所述反馈信息获取所述飞行器的剩余飞行时间;及第一控制模块,用于控制所述显示器显示进度条及配合所述进度条显示所述剩余飞行时间。
- 如权利要求13所述的控制装置,其特征在于,所述反馈信息包括所述剩余飞行时间,所述第二获取模块用于在所述反馈信息中读取所述剩余飞行时间以实现根据所述反馈信息获取所述飞行器的剩余飞行时间。
- 如权利要求13所述的控制装置,其特征在于,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量及飞行参数,所述第一控制模块包括:估算子模块,用于根据所述剩余电量及所述飞行参数估算所述剩余飞行时间。
- 如权利要求13所述的控制装置,其特征在于,所述进度条呈阶梯状,并随着所述剩余飞行时间缩短逐阶变矮。
- 如权利要求13所述的控制装置,其特征在于,所述进度条呈渐变色变化。
- 如权利要求13-17任意一项所述的控制装置,其特征在于,所述第一控制模块包括:第一控制子模块,用于控制所述显示器显示所述进度条的轮廓;及第二控制子模块,用于控制所述显示器在所述进度条的轮廓内显示沿所述进度条的长度方向移动的动态效果图标。
- 如权利要求18所述的控制装置,其特征在于,所述第一控制模块还包括:第三控制子模块,用于控制所述显示器在所述进度条下与所述剩余飞行时间对应的位置显示进度图标。
- 如权利要求19所述的控制装置,其特征在于,所述第一控制模块还包括:第四控制子模块,用于控制所述显示器靠近所述进度图标显示与所述剩余飞行时间对应的时间图标。
- 如权利要求13-17任意一项所述的控制装置,其特征在于,所述控制装置还包括:第三获取模块,用于根据所述反馈信息获取所述飞行器的安全返航时间;及第二控制模块,用于控制所述显示器配合所述进度条显示所述安全返航时间。
- 如权利要求21所述的控制装置,其特征在于,所述第二控制模块包括:第一控制子模块,用于控制所述显示器在所述进度条与所述安全返航时间对应的位置显示返航图标。
- 如权利要求22所述的控制装置,其特征在于,所述第一控制子模块用于根据所述飞行器当前飞行环境以及所述飞行器当前的状况实时估算所述飞行器的安全返航时间,并 在所述进度条的对应位置显示所述返航图标。
- 如权利要求13-17任意一项所述的控制装置,其特征在于,所述飞行器包括电池,所述反馈信息包括所述电池的剩余电量,所述控制装置还包括:第三控制模块,用于控制所述显示器显示所述剩余电量。
- 一种电子装置,其特征在于,所述电子装置包括:显示器;用于与飞行器通信的通信模块;及如权利要求13-24任意一项所述的控制装置。
- 如权利要求26所述的电子装置,其特征在于,所述电子装置包括遥控器、手机、平板电脑、智能手表、智能眼镜及智能头盔的一种或者多种。
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2016/100369 WO2018058314A1 (zh) | 2016-09-27 | 2016-09-27 | 控制方法、控制装置及电子装置 |
CN201680002544.9A CN107077762A (zh) | 2016-09-27 | 2016-09-27 | 控制方法、控制装置及电子装置 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2016/100369 WO2018058314A1 (zh) | 2016-09-27 | 2016-09-27 | 控制方法、控制装置及电子装置 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2018058314A1 true WO2018058314A1 (zh) | 2018-04-05 |
Family
ID=59624181
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2016/100369 WO2018058314A1 (zh) | 2016-09-27 | 2016-09-27 | 控制方法、控制装置及电子装置 |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN107077762A (zh) |
WO (1) | WO2018058314A1 (zh) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109709976B (zh) * | 2017-10-26 | 2022-04-05 | 杭州海康机器人技术有限公司 | 一种可飞行区域确定方法、装置、无人机及存储介质 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103124942A (zh) * | 2011-01-27 | 2013-05-29 | 索尼公司 | 用于显示交互信息的***和方法 |
CN103581323A (zh) * | 2013-11-11 | 2014-02-12 | 惠州Tcl移动通信有限公司 | 一种通过手机姿势控制飞行器的方法及*** |
CN105093130A (zh) * | 2015-09-17 | 2015-11-25 | 杨珊珊 | 一种无人飞行器续航能力监测***及方法 |
US20160101872A1 (en) * | 2013-08-30 | 2016-04-14 | Insitu, Inc. | Systems and methods for fuel monitoring |
CN105518487A (zh) * | 2014-10-27 | 2016-04-20 | 深圳市大疆创新科技有限公司 | 飞行器的位置提示方法及装置 |
CN105539843A (zh) * | 2015-12-03 | 2016-05-04 | 杨珊珊 | 一种电动无人机及其续航能力估计方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101866180A (zh) * | 2010-06-23 | 2010-10-20 | 清华大学 | 一种飞行控制*** |
US9205931B1 (en) * | 2014-07-16 | 2015-12-08 | Honeywell International Inc. | System and method for increasing pilot awareness during non-normal flight situations |
CN205353772U (zh) * | 2016-01-11 | 2016-06-29 | 谭圆圆 | 一种无人飞行器的控制器 |
-
2016
- 2016-09-27 CN CN201680002544.9A patent/CN107077762A/zh active Pending
- 2016-09-27 WO PCT/CN2016/100369 patent/WO2018058314A1/zh active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103124942A (zh) * | 2011-01-27 | 2013-05-29 | 索尼公司 | 用于显示交互信息的***和方法 |
US20160101872A1 (en) * | 2013-08-30 | 2016-04-14 | Insitu, Inc. | Systems and methods for fuel monitoring |
CN103581323A (zh) * | 2013-11-11 | 2014-02-12 | 惠州Tcl移动通信有限公司 | 一种通过手机姿势控制飞行器的方法及*** |
CN105518487A (zh) * | 2014-10-27 | 2016-04-20 | 深圳市大疆创新科技有限公司 | 飞行器的位置提示方法及装置 |
CN105093130A (zh) * | 2015-09-17 | 2015-11-25 | 杨珊珊 | 一种无人飞行器续航能力监测***及方法 |
CN105539843A (zh) * | 2015-12-03 | 2016-05-04 | 杨珊珊 | 一种电动无人机及其续航能力估计方法 |
Also Published As
Publication number | Publication date |
---|---|
CN107077762A (zh) | 2017-08-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10484597B2 (en) | Emotional/cognative state-triggered recording | |
US10449673B2 (en) | Enhanced configuration and control of robots | |
US10762429B2 (en) | Emotional/cognitive state presentation | |
US10268266B2 (en) | Selection of objects in three-dimensional space | |
WO2018058311A1 (zh) | 控制方法、控制装置及电子装置 | |
CN104904229A (zh) | 显示装置及其控制方法 | |
WO2018058309A1 (zh) | 控制方法、控制装置、电子装置及飞行器控制*** | |
CN108885856A (zh) | 信息处理设备、信息处理方法和程序 | |
WO2018086129A1 (zh) | 控制方法、控制装置及电子装置 | |
CN104076921A (zh) | 显示控制设备、显示控制方法和程序 | |
US9142003B2 (en) | Adaptive frame rate control | |
US10776943B2 (en) | System and method for 3D association of detected objects | |
WO2018058314A1 (zh) | 控制方法、控制装置及电子装置 | |
WO2018058313A1 (zh) | 控制方法、控制装置及电子装置 | |
US20150029209A1 (en) | Method and system for adjusting display unit | |
US10216289B2 (en) | Laser pointer emulation via a mobile device | |
WO2018053853A1 (zh) | 控制方法、控制装置、电子装置及飞行器控制*** | |
WO2018058312A1 (zh) | 控制方法、控制装置及电子装置 | |
KR102452973B1 (ko) | 영상 처리 방법 및 이를 지원하는 전자 장치 | |
CN108509010B (zh) | 供电方法和供电*** | |
US11796810B2 (en) | Indication of presence awareness | |
CN112381708A (zh) | 滤镜切换方法、电子设备和计算机可读存储介质 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 16917074 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 16917074 Country of ref document: EP Kind code of ref document: A1 |