WO2018086129A1 - 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 PDF

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Publication number
WO2018086129A1
WO2018086129A1 PCT/CN2016/105770 CN2016105770W WO2018086129A1 WO 2018086129 A1 WO2018086129 A1 WO 2018086129A1 CN 2016105770 W CN2016105770 W CN 2016105770W WO 2018086129 A1 WO2018086129 A1 WO 2018086129A1
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WO
WIPO (PCT)
Prior art keywords
aircraft
trajectory
flight
dynamic icon
dimensional dynamic
Prior art date
Application number
PCT/CN2016/105770
Other languages
English (en)
French (fr)
Inventor
徐普
苏冠华
邹成
朱成伟
吴迪
Original Assignee
深圳市大疆创新科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to CN201680002633.3A priority Critical patent/CN107077150B/zh
Priority to PCT/CN2016/105770 priority patent/WO2018086129A1/zh
Publication of WO2018086129A1 publication Critical patent/WO2018086129A1/zh
Priority to US16/411,343 priority patent/US20190265730A1/en

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    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • 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
    • G05D1/08—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
    • 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
    • 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]
    • G06F3/0484—Interaction techniques based on graphical user interfaces [GUI] for the control of specific functions or operations, e.g. selecting or manipulating an object, an image or a displayed text element, setting a parameter value or selecting a range
    • G06F3/04847—Interaction techniques to control parameter settings, e.g. interaction with sliders or dials
    • 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]
    • G06F3/0487—Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser
    • G06F3/0488—Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser using a touch-screen or digitiser, e.g. input of commands through traced gestures
    • G06F3/04883—Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser using a touch-screen or digitiser, e.g. input of commands through traced gestures for inputting data by handwriting, e.g. gesture or text
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004—Transmission of traffic-related information to or from an aircraft
    • G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0026—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located on the ground
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0052—Navigation or guidance aids for a single aircraft for cruising
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0069—Navigation or guidance aids for a single aircraft specially adapted for an unmanned aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls

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 capable of communicating with an aircraft, the control method comprising the steps of:
  • a three-dimensional dynamic icon corresponding to the flight trajectory is displayed.
  • controlling method further includes:
  • the status information includes a planned trajectory in an autonomous flight mode
  • the step of acquiring a flight trajectory of the aircraft according to the status information is by reading the planned trajectory in the status information to realise.
  • the status information includes a future trajectory predicted by the aircraft in a manual flight mode, the step of acquiring a flight trajectory of the aircraft based on the status information by reading in the status information Take the future trajectory to achieve.
  • the status information includes a real-time trajectory of the aircraft
  • the step of acquiring a flight trajectory of the aircraft according to the status information is performed according to the real-time trajectory after reading the real-time trajectory
  • the future trajectory of the aircraft is predicted to be achieved.
  • the three-dimensional dynamic icon is arrow-shaped and gradually narrows as the display depth direction.
  • the three-dimensional dynamic icon is highlighted.
  • the three-dimensional dynamic icon includes a plurality of sub-arrows arranged in sequence and spaced apart from each other, The sub-arrows at the end of the three-dimensional dynamic icon are displayed one by one in a swallowed manner as the flight direction of the aircraft.
  • the status information includes a flight attitude
  • the control method further includes:
  • the flight attitude includes a pitch angle of the aircraft, and/or a roll angle, and/or a yaw angle
  • the step of adjusting a display pose of the three-dimensional dynamic icon according to the flight attitude include:
  • the yaw angle of the three-dimensional dynamic icon is adjusted according to the yaw angle of the aircraft.
  • controlling method further includes:
  • Text information corresponding to the flight attitude of the aircraft is displayed.
  • the present invention provides a control device for controlling an electronic device, the electronic device being capable of communicating with an aircraft, the control device comprising:
  • a communication unit configured to receive status information of the aircraft
  • a processor configured to acquire a flight trajectory of the aircraft according to the state information
  • a display for displaying a three-dimensional dynamic icon corresponding to the flight trajectory.
  • the processor is further configured to adjust a display trajectory of the three-dimensional dynamic icon according to the flight trajectory.
  • the status information includes a planned trajectory in an autonomous flight mode
  • the processor is configured to acquire a flight trajectory of the aircraft by reading the planned trajectory in the status information.
  • the status information includes a future trajectory predicted by the aircraft in a manual flight mode, the processor implementing acquisition of the aircraft by reading the future trajectory in the status information Flight trajectory.
  • the status information includes a real-time trajectory of the aircraft
  • the processor implements acquisition by predicting a future trajectory of the aircraft according to the real-time trajectory after the communication unit receives the real-time trajectory The flight path of the aircraft.
  • the three-dimensional dynamic icon is arrow-shaped and gradually narrows as the display depth direction.
  • the three-dimensional dynamic icon is highlighted.
  • the three-dimensional dynamic icon includes a plurality of sub-arrows arranged in sequence and spaced apart from one another, the sub-arrows of the three-dimensional dynamic icon end being displayed one by one in a swallowed manner with the flight direction of the aircraft.
  • the status information includes a flight attitude
  • the processor is further configured to:
  • the flight attitude includes a pitch angle, and/or a roll angle, and/or a yaw angle of the aircraft:
  • the processor is configured to adjust a display attitude of the three-dimensional dynamic icon according to a pitch angle of the aircraft to adjust a display posture of the three-dimensional dynamic icon;
  • the processor is configured to adjust a roll angle of the three-dimensional dynamic icon according to a roll angle of the aircraft to adjust a display posture of the three-dimensional dynamic icon;
  • the processor is configured to adjust a display posture of the three-dimensional dynamic icon by adjusting a yaw angle of the three-dimensional dynamic icon according to a yaw angle of the aircraft.
  • the display is further for displaying textual information corresponding to a flight attitude of the aircraft.
  • the present invention provides an electronic device comprising the control device according to any of the above embodiments.
  • the electronic device includes one or more of a remote controller, a mobile phone, a tablet, a smart watch, smart glasses, and a smart helmet.
  • the control method, the control device, and the electronic device control display in the embodiment of the present invention display the three-dimensional dynamic icon embodying the flight path of the aircraft intelligently and deeply, so that the user has a strong sense of depth when monitoring or operating the aircraft. , improved 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 flow chart of a control method 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 flow chart of a control method of 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 a display display interface of an electronic device according to some embodiments of the present invention.
  • FIG. 10 is a schematic diagram of a display interface of a display of an electronic device according to some embodiments of the present invention.
  • FIG. 11 is a schematic diagram of a display interface of a display of an electronic device according to some embodiments of the present invention.
  • FIG. 12 is a schematic diagram of a display display interface of an electronic device according to some embodiments of the present invention.
  • FIG. 13 is a schematic diagram of a display interface of a display of an electronic device according to some embodiments of the present invention.
  • FIG. 14 is a schematic diagram of a display interface of a display of an electronic device according to some embodiments of the present invention.
  • 15 is a schematic diagram of a display interface of a display of an electronic device according to some embodiments of the present invention.
  • 16 is a schematic diagram of a display interface of a display of an electronic device according to 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 by the control device 110 to control the electronic device 100, and the electronic device 100 can communicate with the aircraft 200.
  • the control method includes:
  • the flight path acquisition method includes the following three types:
  • the flight path of the aircraft 200 is planned in advance by the autonomous flight module in the aircraft 200 or by the autonomous flight module located in the electronic device 100.
  • the state information includes autonomous.
  • the flight module advances the planned planning trajectory.
  • the step of acquiring the flight trajectory of the aircraft 200 according to the state information is implemented by directly reading the planned trajectory in the state information.
  • the flight path of the aircraft 200 is predicted by the trajectory prediction module in the aircraft 200 according to the real-time trajectory during the flight.
  • the state information includes the trajectory in the aircraft 200.
  • the future trajectory predicted by the prediction module correspondingly, the step of acquiring the flight trajectory of the aircraft 200 according to the state information is realized by directly reading the future trajectory in the state information.
  • the aircraft 200 records the real-time trajectory during the flight.
  • the state information includes the real-time trajectory of the aircraft 200, and correspondingly, the flight of the aircraft 200 is acquired according to the state information.
  • the step of trajectory is implemented by predicting the future trajectory of the aircraft from the real-time trajectory after reading the real-time trajectory, at which time the trajectory prediction module is outside the aircraft 200.
  • the control device 110 includes a communication unit 111, a processor 112, and a display 113, which can be used to implement S1, S2, and S3, respectively. That is, the communication unit 111 is configured to receive status information of the aircraft 200. The processor 112 is configured to acquire a flight trajectory of the aircraft 200 based on the status information. The display 113 is for displaying a three-dimensional dynamic icon 101 corresponding to a flight trajectory. The manner in which the processor 112 obtains the flight trajectory includes three of the foregoing control methods, and details are not described herein again.
  • the control device 110 of the embodiment of the present invention can be applied to the electronic device 100 of one embodiment of the present invention.
  • the electronic device 100 includes one of a display terminal having a display function, such as a mobile phone, a tablet computer, a remote controller (such as a screen remote controller), a smart watch, smart glasses, a smart helmet, other virtual reality wear devices, and other augmented reality wear devices. Or a variety.
  • the display 113 in the electronic device 100 can display other related information of the aircraft 200 being monitored or operated, such as the model and parameters of the aircraft 200 itself, in addition to displaying the three-dimensional dynamic icon 101 corresponding to the flight path. Information, flight parameters of the aircraft 200, images or video footage taken by the aircraft 200, and interface information for manipulating the aircraft 200, and the like.
  • the three-dimensional dynamic icon 101 is in the shape of an arrow in which the highlight color is displayed, and is gradually narrowed as the display 113 displays the depth direction.
  • the three-dimensional dynamic icon 101 includes a plurality of sub-arrows arranged in sequence and spaced apart from each other.
  • the sub-arrows at the end of the three-dimensional dynamic icon 101 are displayed one by one in a swallowed manner with the flight direction of the aircraft 200.
  • the three-dimensional dynamic icon 101 may not be a high-bright color, and a relatively bright color may be set, for example, red, green, or yellow designed to give a visual impact.
  • the three-dimensional dynamic icon 101 can also be any other color or a simple combination or a gradual combination of a plurality of colors, as long as the user can be prompted.
  • the shape of the three-dimensional dynamic icon 101 is not limited to an arrow shape, and may be a triangle, a trapezoid, a column shape displayed in a scroll, or the like.
  • the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 113 to display the three-dimensional dynamic icon 101 embodying the flight trajectory of the aircraft 200 intelligently and with a sense of depth, so that when the user monitors or operates the aircraft 200, With a strong sense of depth, the user experience is enhanced. If it is displayed together with the images taken by the aircraft 200 and transmitted back, it will give the user an immersive feeling and greatly enhance the user experience.
  • a control method is used by the control device 110 to control the electronic device 100, and the electronic device 100 can communicate with the aircraft 200.
  • the control method includes:
  • the display trajectory of the three-dimensional dynamic icon 101 is adjusted according to the flight trajectory.
  • the flight path acquisition method includes the following three types:
  • the flight path of the aircraft 200 is planned in advance by the autonomous flight module in the aircraft 200 or by the autonomous flight module located in the electronic device 100.
  • the state information includes autonomous.
  • the flight module advances the planned planning trajectory.
  • the step of acquiring the flight trajectory of the aircraft 200 according to the state information is implemented by directly reading the planned trajectory in the state information.
  • the flight path of the aircraft 200 is predicted by the trajectory prediction module in the aircraft 200 according to the real-time trajectory during the flight.
  • the state information includes the trajectory in the aircraft 200.
  • the future trajectory predicted by the prediction module correspondingly, the step of acquiring the flight trajectory of the aircraft 200 according to the state information is realized by directly reading the future trajectory in the state information.
  • the aircraft 200 records the real-time trajectory during the flight.
  • the state information includes the real-time trajectory of the aircraft 200, and correspondingly, the flight of the aircraft 200 is acquired according to the state information.
  • the step of trajectory is implemented by predicting the future trajectory of the aircraft from the real-time trajectory after reading the real-time trajectory, at which time the trajectory prediction module is outside the aircraft 200.
  • the control device 110 includes a communication unit 111, The processor 112 and the display 113, the communication unit 111 is used to implement S1, the processor 112 is used to implement S2 and S4, and the display 113 is used to implement S3. That is, the communication unit 111 is configured to receive status information of the aircraft 200.
  • the processor 112 is configured to acquire a flight trajectory of the aircraft 200 according to the state information, and adjust a display trajectory of the three-dimensional dynamic icon 101 according to the flight trajectory.
  • the display 113 is for displaying a three-dimensional dynamic icon 101 corresponding to a flight trajectory.
  • the manner in which the processor 112 obtains the flight trajectory includes three of the foregoing control methods, and details are not described herein again.
  • 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 includes one of a display terminal having a display function, such as a mobile phone, a tablet computer, a remote controller (such as a screen remote controller), a smart watch, smart glasses, a smart helmet, other virtual reality wear devices, and other augmented reality wear devices. Or a variety.
  • the display 113 in the electronic device 100 can display other related information of the aircraft 200 being monitored or operated, such as the model and parameters of the aircraft 200 itself, in addition to displaying the three-dimensional dynamic icon 101 corresponding to the flight path. Information, flight parameters of the aircraft 200, images or video footage taken by the aircraft 200, and interface information for manipulating the aircraft 200, and the like.
  • the following is an example to illustrate the display of the three-dimensional dynamic icon 101, and to adjust the three-dimensional dynamic icon 101 corresponding to the flight trajectory according to the flight trajectory:
  • the user clicks on any position on the display 113, and the display 113 displays the cursor 102 in the locking direction;
  • the communication unit 111 receives the state information of the aircraft 200, and the processor 112 acquires the flight trajectory of the aircraft 200 according to the state information, and the acquisition mode is any one of the above three modes; then, referring to FIG. 10, the display 113 displays A three-dimensional dynamic icon 101 corresponding to the flight path.
  • the flight trajectory of the aircraft 200 can be immediately known by observing the three-dimensional dynamic icon 101 displayed in the display 113.
  • the display trajectory is adjusted from the linear trajectory in FIG. 10 to the curved trajectory in FIG. 11.
  • the user can intuitively feel that the flight trajectory of the aircraft 200 also changes from a linear trajectory to a curved trajectory.
  • the three-dimensional dynamic icon 101 is in the shape of an arrow in which the highlight color is displayed, and is gradually narrowed as the display 113 displays the depth direction.
  • the three-dimensional dynamic icon 101 includes a plurality of sub-arrows arranged in sequence and spaced apart from each other.
  • the sub-arrows at the end of the three-dimensional dynamic icon 101 are displayed one by one in a swallowed manner with the flight direction of the aircraft 200.
  • the three-dimensional dynamic icon 101 may not be a high-bright color, and a relatively bright color may be set, for example, red, green, or yellow designed to give a visual impact.
  • the three-dimensional dynamic icon 101 can also be any other color or a simple combination or a gradual combination of a plurality of colors, as long as the user can be prompted.
  • the shape of the three-dimensional dynamic icon 101 is not limited to an arrow shape, and may be a triangle, a trapezoid, a column shape displayed in a scroll, or the like.
  • the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 113 to display the three-dimensional dynamic icon 101 embodying the flight trajectory of the aircraft 200 intelligently and with a sense of depth, so that when the user monitors or operates the aircraft 200, With a strong sense of depth, the user experience is enhanced. If it is matched with the aircraft 200, it will be photographed and transmitted. The back images are displayed together, which will give the user an immersive feeling and greatly enhance the user experience.
  • the processor 112 can adjust the display trajectory of the three-dimensional dynamic icon 101 according to the flight trajectory of the aircraft 200, and the user can intuitively feel the flight trajectory of the aircraft 200 through the display trajectory of the three-dimensional dynamic icon 101, thereby further improving the user experience.
  • a control method is used by the control device 110 to control the electronic device 100, and the electronic device 100 can communicate with the aircraft 200.
  • the control method includes:
  • the flight path acquisition method includes the following three types:
  • the flight path of the aircraft 200 is planned in advance by the autonomous flight module in the aircraft 200 or by the autonomous flight module located in the electronic device 100.
  • the state information includes autonomous.
  • the flight module advances the planned planning trajectory.
  • the step of acquiring the flight trajectory of the aircraft 200 according to the state information is implemented by directly reading the planned trajectory in the state information.
  • the flight path of the aircraft 200 is predicted by the trajectory prediction module in the aircraft 200 according to the real-time trajectory during the flight.
  • the state information includes the trajectory in the aircraft 200.
  • the future trajectory predicted by the prediction module correspondingly, the step of acquiring the flight trajectory of the aircraft 200 according to the state information is realized by directly reading the future trajectory in the state information.
  • the aircraft 200 records the real-time trajectory during the flight.
  • the state information includes the real-time trajectory of the aircraft 200, and correspondingly, the flight of the aircraft 200 is acquired according to the state information.
  • the step of trajectory is implemented by predicting the future trajectory of the aircraft from the real-time trajectory after reading the real-time trajectory, at which time the trajectory prediction module is outside the aircraft 200.
  • steps S6 and S7 include the following seven methods:
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a pitch angle of the three-dimensional dynamic icon 101 according to a pitch angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a roll angle of the three-dimensional dynamic icon 101 according to a roll angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting the yaw of the three-dimensional dynamic icon 101 according to the yaw angle of the aircraft 200 angle;
  • the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a three-dimensional dynamic icon according to the pitch angle and the roll angle of the aircraft 200 The pitch angle and roll angle of 101;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to the pitch angle and the yaw angle of the aircraft 200; The pitch angle and yaw angle of the dynamic icon 101;
  • Obtaining a roll angle and a yaw angle of the aircraft 200 according to the state information, and the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to a roll angle and a yaw angle of the aircraft 200; The roll angle and yaw angle of the dynamic icon 101;
  • the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude including: according to the pitch angle and the roll angle of the aircraft 200 And the yaw angle corresponds to adjusting the pitch angle, the roll angle, and the yaw angle of the three-dimensional dynamic icon 101.
  • the specific angles of the above seven cases may be equivalent adjustments, that is, how much the angle of the aircraft 200 changes, and the angle of the three-dimensional dynamic icon 101 changes, for example, the aircraft 200 is up to 60 degrees, the three-dimensional dynamic icon The 101 is also raised 60 degrees, the aircraft 200 is lowered 60 degrees, and the 3D dynamic icon 101 is also lowered 60 degrees.
  • the respective angles corresponding to the adjustment of the three-dimensional dynamic icon 101 may also be adjusted according to a preset ratio, for example, assuming that the predetermined ratio is 2:1, the aircraft 200 is up 60 degrees, the three-dimensional dynamic icon 101 is tilted 30 degrees, and the aircraft 200 The vehicle is tilted by 60 degrees, and the three-dimensional dynamic icon 101 is lowered by 30 degrees.
  • the respective angles of the three-dimensional dynamic icon 101 may be adjusted according to a preset mapping relationship.
  • the aircraft 200 is tilted 60 degrees, according to preset
  • the three-dimensional dynamic icon 101 is tilted by 30 degrees, and the aircraft 200 is tilted by 60 degrees.
  • the three-dimensional dynamic icon 101 is lowered by 30 degrees according to a preset mapping relationship.
  • the respective angles of the three-dimensional dynamic icon 101 may be adjusted correspondingly.
  • the angle is adjusted at a fixed angle. For example, if the elevation angle of the aircraft 200 is 0-30 degrees, the three-dimensional dynamic icon 101 is raised by 15 degrees, and the upward angle of the aircraft 200 is 30-60.
  • the angle of the three-dimensional dynamic icon 101 is 30 degrees, and if the angle of elevation of the aircraft 200 is 60-90 degrees, the three-dimensional dynamic icon 101 is raised by 60 degrees and the like.
  • adjusting the respective angles of the three-dimensional dynamic icon 101 is performed in an equivalent adjustment manner, so that the user can feel the posture change of the aircraft 200 in synchronization.
  • the corresponding adjustment may also be adjusted according to the user's autonomous input of respective corresponding angles, for example, the user inputs a pitch angle of 30 degrees, a roll angle of 50 degrees, and a yaw angle of 60 degrees; then, once the aircraft 200 is pitched, regardless of the pitch angle of the aircraft 200 How many, the three-dimensional dynamic icon 101 is uniformly tilted by 30 degrees; once the aircraft 200 rolls, regardless of the roll angle of the aircraft 200, the three-dimensional dynamic icon 101 is rolled 30 degrees; once flying The yaw 200 is yawed, and the three-dimensional dynamic icon 101 is yawed 30 degrees regardless of the yaw angle of the aircraft 200.
  • the control device 110 includes a communication unit 111, a processor 112, and a display 113.
  • the communication unit 111 is used to implement S1, and the processor 112 is used to implement S2 and S5.
  • the display 113 is used to implement S3. That is, the communication unit 111 is configured to receive status information of the aircraft 200.
  • the processor 112 is configured to acquire a flight trajectory of the aircraft 200 according to the state information, acquire a flight attitude according to the state information, and adjust a display posture of the three-dimensional dynamic icon 101 according to the flight attitude.
  • the display 113 is for displaying a three-dimensional dynamic icon 101 corresponding to a flight trajectory.
  • the manner in which the processor 112 acquires the flight trajectory includes the above three methods, and the manner in which the display posture of the three-dimensional dynamic icon 101 is adjusted according to the flight attitude is the above seven types, and details are not described herein again.
  • the control device 110 of the embodiment of the present invention can be applied to the electronic device 100 of one embodiment of the present invention.
  • the electronic device 100 includes one of a display terminal having a display function, such as a mobile phone, a tablet computer, a remote controller (such as a screen remote controller), a smart watch, smart glasses, a smart helmet, other virtual reality wear devices, and other augmented reality wear devices. Or a variety.
  • the display 113 in the electronic device 100 can display other related information of the aircraft 200 being monitored or operated, such as the model and parameters of the aircraft 200 itself, in addition to displaying the three-dimensional dynamic icon 101 corresponding to the flight path. Information, flight parameters of the aircraft 200, images or video footage taken by the aircraft 200, and interface information for manipulating the aircraft 200, and the like.
  • the following shows an example of displaying the three-dimensional dynamic icon 101 and adjusting the three-dimensional dynamic icon 101 corresponding to the flight trajectory according to the flight attitude:
  • the user clicks on any position of the display 113, and the display 113 displays the cursor 102 in the locking direction;
  • the communication unit 111 receives the status information of the aircraft 200, and the processor 112 acquires the flight trajectory of the aircraft 200 according to the status information, and the acquisition manner is any one of the above three manners; then, referring to FIG. 10, the display 113 displays The three-dimensional dynamic icon 101 corresponding to the flight path.
  • the flight trajectory of the aircraft 200 can be immediately known by observing the three-dimensional dynamic icon 101 displayed in the display 113.
  • the processor 112 adjusts the display posture of the three-dimensional dynamic icon 101 according to the flight attitude. For example, if the aircraft 200 is yawed and the nose of the aircraft 200 is facing the non-flying direction, The processor 112 acquires the yaw angle, and correspondingly, the three-dimensional dynamic icon 101 also has a yaw of the corresponding angle (as shown in FIG. 12). When the yaw angle of the aircraft 200 reaches 180 degrees, correspondingly, the three-dimensional dynamic icon 101 also has a yaw corresponding to 180 degrees (as shown in FIG. 13), and at this time, the display trajectory of the three-dimensional dynamic icon 101 may be according to the aircraft 200.
  • the forward speed information is blanked step by step. Further, if the user controls the remote control throttle down at this time, the original display track transparency of the three-dimensional dynamic icon 101 is lowered, and the downward arrow is looming (this change can be reflected from FIG. 13 to FIG. 14); when the user controls When the remote control throttle is up, the original display track transparency of the three-dimensional dynamic icon 101 is lowered, and the upward arrow is looming.
  • the three-dimensional dynamic icon 101 is in the shape of an arrow in which the highlight color is displayed, and is gradually narrowed as the display 113 displays the depth direction. Specifically, the three-dimensional dynamic icon 101 includes a plurality of sub-arrows arranged in sequence and spaced apart from each other.
  • the child at the end of the three-dimensional dynamic icon 101 The arrows are displayed one by one in a swallowed manner with the flight direction of the aircraft 200.
  • the three-dimensional dynamic icon 101 may not be a high-bright color, and a relatively bright color may be set, for example, red, green, or yellow designed to give a visual impact.
  • the three-dimensional dynamic icon 101 can also be any other color or a simple combination or a gradual combination of a plurality of colors, as long as the user can be prompted.
  • the shape of the three-dimensional dynamic icon 101 is not limited to an arrow shape, and may be a triangle, a trapezoid, a column shape displayed in a scroll, or the like.
  • the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 113 to display the three-dimensional dynamic icon 101 embodying the flight trajectory of the aircraft 200 intelligently and with a sense of depth, so that when the user monitors or operates the aircraft 200, With a strong sense of depth, the user experience is enhanced. If it is displayed together with the images taken by the aircraft 200 and transmitted back, it will give the user an immersive feeling and greatly enhance the user experience.
  • the processor 112 can adjust the display posture of the three-dimensional dynamic icon according to the flight attitude of the aircraft 200, and the user can intuitively feel the flight posture of the aircraft 200 through the display posture of the three-dimensional dynamic icon 101, thereby further improving the user experience.
  • a control method is used by the control device 110 to control the electronic device 100, and the electronic device 100 can communicate with the aircraft 200.
  • the control method includes:
  • the flight path acquisition method includes the following three types:
  • the flight path of the aircraft 200 is planned in advance by the autonomous flight module in the aircraft 200 or by the autonomous flight module located in the electronic device 100.
  • the state information includes autonomous.
  • the flight module advances the planned planning trajectory.
  • the step of acquiring the flight trajectory of the aircraft 200 according to the state information is implemented by directly reading the planned trajectory in the state information.
  • the flight path of the aircraft 200 is predicted by the trajectory prediction module in the aircraft 200 according to the real-time trajectory during the flight.
  • the state information includes the trajectory in the aircraft 200.
  • the future trajectory predicted by the prediction module correspondingly, the step of acquiring the flight trajectory of the aircraft 200 according to the state information is realized by directly reading the future trajectory in the state information.
  • the aircraft 200 records the real-time trajectory during the flight.
  • the state information includes the real-time trajectory of the aircraft 200, and correspondingly, the flight of the aircraft 200 is acquired according to the state information.
  • the step of trajecting is to predict the aircraft according to the real-time trajectory after reading the real-time trajectory
  • the future trajectory is implemented, at which point the trajectory prediction module is outside of the aircraft 200.
  • steps S6 and S7 include the following seven methods:
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a pitch angle of the three-dimensional dynamic icon 101 according to a pitch angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a roll angle of the three-dimensional dynamic icon 101 according to a roll angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting the yaw of the three-dimensional dynamic icon 101 according to the yaw angle of the aircraft 200 angle;
  • the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a three-dimensional dynamic icon according to the pitch angle and the roll angle of the aircraft 200 The pitch angle and roll angle of 101;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to the pitch angle and the yaw angle of the aircraft 200; The pitch angle and yaw angle of the dynamic icon 101;
  • Obtaining a roll angle and a yaw angle of the aircraft 200 according to the state information, and the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to a roll angle and a yaw angle of the aircraft 200; The roll angle and yaw angle of the dynamic icon 101;
  • the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude including: according to the pitch angle and the roll angle of the aircraft 200 And the yaw angle corresponds to adjusting the pitch angle, the roll angle, and the yaw angle of the three-dimensional dynamic icon 101.
  • the specific angles of the above seven cases may be equivalent adjustments, that is, how much the angle of the aircraft 200 changes, and the angle of the three-dimensional dynamic icon 101 changes, for example, the aircraft 200 is up to 60 degrees, the three-dimensional dynamic icon The 101 is also raised 60 degrees, the aircraft 200 is lowered 60 degrees, and the 3D dynamic icon 101 is also lowered 60 degrees.
  • the respective angles of the corresponding three-dimensional dynamic icons 101 may be adjusted according to a preset ratio, for example, assuming that the predetermined ratio is 2:1, the aircraft 200 is up 60 degrees, the three-dimensional dynamic icon 101 is tilted 30 degrees, and the aircraft 200 The vehicle is tilted by 60 degrees, and the three-dimensional dynamic icon 101 is lowered by 30 degrees.
  • the respective angles of the three-dimensional dynamic icon 101 may be adjusted according to a preset mapping relationship.
  • the aircraft 200 is tilted 60 degrees, according to preset
  • the mapping relationship 3D dynamic icon 101 is tilted 30 degrees, and the aircraft 200 is tilted 60 degrees, according to a preset mapping relationship three
  • the dimension dynamic icon 101 is lowered by 30 degrees; or, the corresponding angles of the three-dimensional dynamic icon 101 may be adjusted at a fixed angle according to various angular ranges of the preset aircraft. For example, if the elevation angle of the aircraft 200 is 0- At 30 degrees, the three-dimensional dynamic icon 101 is raised by 15 degrees.
  • the three-dimensional dynamic icon 101 is tilted 30 degrees, and if the elevation angle of the aircraft 200 is 60-90 degrees, the three-dimensional dynamic The icon 101 is raised 60 degrees and the like.
  • adjusting the respective angles of the three-dimensional dynamic icon 101 is performed in an equivalent adjustment manner, so that the user can feel the posture change of the aircraft 200 in synchronization.
  • the corresponding adjustment may also be adjusted according to the user's autonomous input of respective corresponding angles, for example, the user inputs a pitch angle of 30 degrees, a roll angle of 50 degrees, and a yaw angle of 60 degrees; then, once the aircraft 200 is pitched, regardless of the pitch angle of the aircraft 200 How many, the three-dimensional dynamic icon 101 is uniformly tilted by 30 degrees; once the aircraft 200 rolls, regardless of the roll angle of the aircraft 200, the three-dimensional dynamic icon 101 rolls over 30 degrees; once the aircraft 200 yaws, regardless of the yaw of the aircraft 200 The angle of the three-dimensional dynamic icon 101 is yawed by 30 degrees.
  • the control device 110 includes a communication unit 111, a processor 112, and a display 113.
  • the communication unit 111 is used to implement S1, and the processor 112 is used to implement S2 and S5.
  • the display 113 is used to implement S3 and S7. That is, the communication unit 111 is configured to receive status information of the aircraft 200.
  • the processor 112 is configured to acquire a flight trajectory of the aircraft 200 according to the state information, acquire a flight attitude according to the state information, and adjust a display posture of the three-dimensional dynamic icon 101 according to the flight attitude.
  • the display 113 is for displaying a three-dimensional dynamic icon 101 corresponding to a flight trajectory and for displaying text information 103 corresponding to the flight attitude of the aircraft 200.
  • the manner in which the processor 112 acquires the flight trajectory includes the above three methods, and the manner in which the display posture of the three-dimensional dynamic icon 101 is adjusted according to the flight attitude is the above seven types, and details are not described herein again.
  • 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 includes one of a display terminal having a display function, such as a mobile phone, a tablet computer, a remote controller (such as a screen remote controller), a smart watch, smart glasses, a smart helmet, other virtual reality wear devices, and other augmented reality wear devices. Or a variety.
  • the display 113 in the electronic device 100 can display other related information of the aircraft 200 being monitored or operated, such as the aircraft 200, in addition to displaying the three-dimensional dynamic icon 101 and the text information 103 corresponding to the flight path. Its own model and parameter information, flight parameters of the aircraft 200, images or video images taken by the aircraft 200, and interface information for manipulating the aircraft 200, and the like.
  • the following shows an example of displaying the three-dimensional dynamic icon 101, adjusting the three-dimensional dynamic icon 101 corresponding to the flight trajectory according to the flight attitude, and displaying the corresponding text information 103:
  • First referring to FIG. 9, the user clicks on any position of the display 113, and the display 113 displays the lock.
  • the communication unit 111 receives the state information of the aircraft 200, and the processor 112 acquires the flight trajectory of the aircraft 200 according to the state information, and the acquisition mode is any one of the above three modes; then, referring to FIG.
  • the display 113 displays a three-dimensional dynamic icon 101 corresponding to the flight path.
  • the flight trajectory of the aircraft 200 can be immediately known by observing the three-dimensional dynamic icon 101 displayed in the display 113. If the flight attitude of the aircraft 200 changes at this time, the processor 112 adjusts the three-dimensional motion according to the flight attitude.
  • the display gesture of the state icon 101 for example, if the aircraft 200 is yawed and the nose of the aircraft 200 is facing the non-flying direction, the processor 112 acquires the yaw angle, and correspondingly, the three-dimensional dynamic icon 101 also has a corresponding angle deviation. Navigation (as shown in Figure 12). When the yaw angle of the aircraft 200 reaches 180 degrees, correspondingly, the three-dimensional dynamic icon 101 also has a yaw corresponding to 180 degrees (as shown in FIG.
  • the display trajectory of the three-dimensional dynamic icon 101 may be according to the aircraft 200.
  • the forward speed information is blanked step by step.
  • the display 113 also displays the text information 103 corresponding to the yaw to remind the user, for example, that the three-dimensional dynamic icon 101 in FIG. 10 changes to the three-dimensional dynamic icon 101 in which yaw occurs in FIG. 15, and displays "yaw 180 degrees". Text information 103.
  • the user can intuitively feel that the aircraft 200 is yawed and can quickly read the corresponding text information 103 from the display 113. If the text information "up” or "down” is displayed on the display 113, the user can quickly know that the aircraft 200 is "rising" or "falling".
  • the three-dimensional dynamic icon 101 is in the shape of an arrow in which the highlight color is displayed, and is gradually narrowed as the display 113 displays the depth direction.
  • the three-dimensional dynamic icon 101 includes a plurality of sub-arrows arranged in sequence and spaced apart from each other.
  • the sub-arrows at the end of the three-dimensional dynamic icon 101 are displayed one by one in a swallowed manner with the flight direction of the aircraft 200.
  • the three-dimensional dynamic icon 101 may not be a high-bright color, and a relatively bright color may be set, for example, red, green, or yellow designed to give a visual impact.
  • the three-dimensional dynamic icon 101 can also be any other color or a simple combination or a gradual combination of a plurality of colors, as long as the user can be prompted.
  • the shape of the three-dimensional dynamic icon 101 is not limited to an arrow shape, and may be a triangle, a trapezoid, a column shape displayed in a scroll, or the like.
  • the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 113 to display the three-dimensional dynamic icon 101 embodying the flight trajectory of the aircraft 200 intelligently and with a sense of depth, so that when the user monitors or operates the aircraft 200, With a strong sense of depth, the user experience is enhanced. If it is displayed together with the images taken by the aircraft 200 and transmitted back, it will give the user an immersive feeling and greatly enhance the user experience.
  • the processor 112 can adjust the display posture of the three-dimensional dynamic icon according to the flight attitude of the aircraft 200, and the display 113 also displays the text information 103 corresponding to the flight attitude to remind the user that the user can intuitively feel the aircraft through the display posture of the three-dimensional dynamic icon 101.
  • the flight attitude of 200 and the ability to quickly read the corresponding text information 103 from the display 113 further enhances the user experience.
  • a control method is used by the control device 110 to control the electronic device 100, and the electronic device 100 can communicate with the aircraft 200.
  • the control method includes:
  • the flight path acquisition method includes the following three types:
  • the flight path of the aircraft 200 is planned in advance by the autonomous flight module in the aircraft 200 or by the autonomous flight module located in the electronic device 100.
  • the state information includes autonomous.
  • the flight module advances the planned planning trajectory.
  • the step of acquiring the flight trajectory of the aircraft 200 according to the state information is implemented by directly reading the planned trajectory in the state information.
  • the flight path of the aircraft 200 is predicted by the trajectory prediction module in the aircraft 200 according to the real-time trajectory during the flight.
  • the state information includes the trajectory in the aircraft 200.
  • the future trajectory predicted by the prediction module correspondingly, the step of acquiring the flight trajectory of the aircraft 200 according to the state information is realized by directly reading the future trajectory in the state information.
  • the aircraft 200 records the real-time trajectory during the flight.
  • the state information includes the real-time trajectory of the aircraft 200, and correspondingly, the flight of the aircraft 200 is acquired according to the state information.
  • the step of trajectory is implemented by predicting the future trajectory of the aircraft from the real-time trajectory after reading the real-time trajectory, at which time the trajectory prediction module is outside the aircraft 200.
  • steps S6 and S7 include the following seven methods:
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a pitch angle of the three-dimensional dynamic icon 101 according to a pitch angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a roll angle of the three-dimensional dynamic icon 101 according to a roll angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting the yaw of the three-dimensional dynamic icon 101 according to the yaw angle of the aircraft 200 angle;
  • the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a three-dimensional dynamic icon according to the pitch angle and the roll angle of the aircraft 200 The pitch angle and roll angle of 101;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to the pitch angle and the yaw angle of the aircraft 200; The pitch angle and yaw angle of the dynamic icon 101;
  • Obtaining a roll angle and a yaw angle of the aircraft 200 according to the state information, and the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to a roll angle and a yaw angle of the aircraft 200; move The roll angle and yaw angle of the state icon 101;
  • the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude including: according to the pitch angle and the roll angle of the aircraft 200 And the yaw angle corresponds to adjusting the pitch angle, the roll angle, and the yaw angle of the three-dimensional dynamic icon 101.
  • the specific angles of the above seven cases may be equivalent adjustments, that is, how much the angle of the aircraft 200 changes, and the angle of the three-dimensional dynamic icon 101 changes, for example, the aircraft 200 is up to 60 degrees, the three-dimensional dynamic icon The 101 is also raised 60 degrees, the aircraft 200 is lowered 60 degrees, and the 3D dynamic icon 101 is also lowered 60 degrees.
  • the respective angles corresponding to the adjustment of the three-dimensional dynamic icon 101 may also be adjusted according to a preset ratio, for example, assuming that the predetermined ratio is 2:1, the aircraft 200 is up 60 degrees, the three-dimensional dynamic icon 101 is tilted 30 degrees, and the aircraft 200 The vehicle is tilted by 60 degrees, and the three-dimensional dynamic icon 101 is lowered by 30 degrees.
  • the respective angles of the three-dimensional dynamic icon 101 may be adjusted according to a preset mapping relationship.
  • the aircraft 200 is tilted 60 degrees, according to preset
  • the three-dimensional dynamic icon 101 is tilted by 30 degrees, and the aircraft 200 is tilted by 60 degrees.
  • the three-dimensional dynamic icon 101 is lowered by 30 degrees according to a preset mapping relationship.
  • the respective angles of the three-dimensional dynamic icon 101 may be adjusted correspondingly.
  • the angle is adjusted at a fixed angle. For example, if the elevation angle of the aircraft 200 is 0-30 degrees, the three-dimensional dynamic icon 101 is raised by 15 degrees, and the upward angle of the aircraft 200 is 30-60.
  • the angle of the three-dimensional dynamic icon 101 is 30 degrees, and if the angle of elevation of the aircraft 200 is 60-90 degrees, the three-dimensional dynamic icon 101 is raised by 60 degrees and the like.
  • adjusting the respective angles of the three-dimensional dynamic icon 101 is performed in an equivalent adjustment manner, so that the user can feel the posture change of the aircraft 200 in synchronization.
  • the corresponding adjustment may also be adjusted according to the user's autonomous input of respective corresponding angles, for example, the user inputs a pitch angle of 30 degrees, a roll angle of 50 degrees, and a yaw angle of 60 degrees; then, once the aircraft 200 is pitched, regardless of the pitch angle of the aircraft 200 How many, the three-dimensional dynamic icon 101 is uniformly tilted by 30 degrees; once the aircraft 200 rolls, regardless of the roll angle of the aircraft 200, the three-dimensional dynamic icon 101 rolls over 30 degrees; once the aircraft 200 yaws, regardless of the yaw of the aircraft 200 The angle of the three-dimensional dynamic icon 101 is yawed by 30 degrees.
  • the control device 110 includes a communication unit 111, a processor 112, and a display 113.
  • the communication unit 111 is used to implement S1, and the processor 112 is used to implement S2 and S4. , S5 and S6, the display 113 is used to implement S3. That is, the communication unit 111 is configured to receive status information of the aircraft 200.
  • the processor 112 is configured to acquire a flight trajectory of the aircraft 200 according to the state information, adjust a display trajectory of the three-dimensional dynamic icon 101 according to the flight trajectory, acquire a flight attitude according to the state information, and adjust the three-dimensional dynamic icon 101 according to the flight attitude. Show gestures.
  • the display 113 is for displaying a three-dimensional dynamic icon 101 corresponding to a flight trajectory.
  • the manner in which the processor 112 acquires the flight trajectory includes the above three methods, and the manner in which the display posture of the three-dimensional dynamic icon 101 is adjusted according to the flight attitude is the above seven types, and details are not described herein again.
  • 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 includes a mobile phone, a tablet computer, a remote controller (such as a remote control with a screen), a smart watch, smart glasses, a smart helmet, One or more of display terminals having display functions, such as other virtual reality wearable devices and other augmented reality wearable devices.
  • the display 113 in the electronic device 100 can display other related information of the aircraft 200 being monitored or operated, such as the model and parameters of the aircraft 200 itself, in addition to displaying the three-dimensional dynamic icon 101 corresponding to the flight path. Information, flight parameters of the aircraft 200, images or video footage taken by the aircraft 200, and interface information for manipulating the aircraft 200, and the like.
  • the following shows an example of displaying the three-dimensional dynamic icon 101, and adjusting the three-dimensional dynamic icon 101 corresponding to the flight trajectory according to the flight trajectory and the flight attitude:
  • the user clicks on any position of the display 113, and the display 113 displays the cursor 102 in the locking direction.
  • the communication unit 111 receives the status information of the aircraft 200, and the processor 112 acquires the flight trajectory of the aircraft 200 according to the status information, and the acquisition manner is any one of the above three manners; then, referring to FIG. 10, the display 113 will A three-dimensional dynamic icon 101 corresponding to the flight trajectory is displayed.
  • the flight trajectory of the aircraft 200 can be immediately known by observing the three-dimensional dynamic icon 101 displayed in the display 113.
  • the device 112 adjusts the display trajectory of the three-dimensional dynamic icon 101 according to the flight trajectory and adjusts the display posture of the three-dimensional dynamic icon 101 according to the flight attitude, as adjusted by the linear trajectory in FIG. 10 to the curved trajectory of FIG. 11, and a roll occurs.
  • the user can intuitively feel that the flight trajectory of the aircraft 200 also changes from a straight trajectory to a curved trajectory, and a roll occurs.
  • the three-dimensional dynamic icon 101 is in the shape of an arrow in which the highlight color is displayed, and is gradually narrowed as the display 113 displays the depth direction.
  • the three-dimensional dynamic icon 101 includes a plurality of sub-arrows arranged in sequence and spaced apart from each other.
  • the sub-arrows at the end of the three-dimensional dynamic icon 101 are displayed one by one in a swallowed manner with the flight direction of the aircraft 200.
  • the three-dimensional dynamic icon 101 may not be a high-bright color, and a relatively bright color may be set, for example, red, green, or yellow designed to give a visual impact.
  • the three-dimensional dynamic icon 101 can also be any other color or a simple combination or a gradual combination of a plurality of colors, as long as the user can be prompted.
  • the shape of the three-dimensional dynamic icon 101 is not limited to an arrow shape, and may be a triangle, a trapezoid, a column shape displayed in a scroll, or the like.
  • the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 113 to display the three-dimensional dynamic icon 101 embodying the flight trajectory of the aircraft 200 intelligently and with a sense of depth, so that when the user monitors or operates the aircraft 200, With a strong sense of depth, the user experience is enhanced. If it is displayed together with the images taken by the aircraft 200 and transmitted back, it will give the user an immersive feeling and greatly enhance the user experience.
  • the processor 112 can adjust the display trajectory and the display posture of the three-dimensional dynamic icon 101 according to the flight trajectory and the flight attitude of the aircraft 200, and the user can intuitively feel the flight trajectory of the aircraft 200 through the display trajectory and the display posture of the three-dimensional dynamic icon 101.
  • the flight attitude further enhances the user experience.
  • a control method is used by the control device 110 to control the electronic device 100, and the electronic device 100 can communicate with the aircraft 200.
  • the control method includes:
  • the flight path acquisition method includes the following three types:
  • the flight path of the aircraft 200 is planned in advance by the autonomous flight module in the aircraft 200 or by the autonomous flight module located in the electronic device 100.
  • the state information includes autonomous.
  • the flight module advances the planned planning trajectory.
  • the step of acquiring the flight trajectory of the aircraft 200 according to the state information is implemented by directly reading the planned trajectory in the state information.
  • the flight path of the aircraft 200 is predicted by the trajectory prediction module in the aircraft 200 according to the real-time trajectory during the flight.
  • the state information includes the trajectory in the aircraft 200.
  • the future trajectory predicted by the prediction module correspondingly, the step of acquiring the flight trajectory of the aircraft 200 according to the state information is realized by directly reading the future trajectory in the state information.
  • the aircraft 200 records the real-time trajectory during the flight.
  • the state information includes the real-time trajectory of the aircraft 200, and correspondingly, the flight of the aircraft 200 is acquired according to the state information.
  • the step of trajectory is implemented by predicting the future trajectory of the aircraft from the real-time trajectory after reading the real-time trajectory, at which time the trajectory prediction module is outside the aircraft 200.
  • steps S6 and S7 include the following seven methods:
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a pitch angle of the three-dimensional dynamic icon 101 according to a pitch angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting a roll angle of the three-dimensional dynamic icon 101 according to a roll angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting the yaw of the three-dimensional dynamic icon 101 according to the yaw angle of the aircraft 200 angle;
  • the step of displaying the posture of the three-dimensional dynamic icon includes: adjusting the pitch angle and the roll angle of the three-dimensional dynamic icon 101 according to the pitch angle and the roll angle of the aircraft 200;
  • step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to the pitch angle and the yaw angle of the aircraft 200; The pitch angle and yaw angle of the dynamic icon 101;
  • Obtaining a roll angle and a yaw angle of the aircraft 200 according to the state information, and the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude comprises: adjusting three-dimensional according to a roll angle and a yaw angle of the aircraft 200; The roll angle and yaw angle of the dynamic icon 101;
  • the step of adjusting the display posture of the three-dimensional dynamic icon according to the flight attitude including: according to the pitch angle and the roll angle of the aircraft 200 And the yaw angle corresponds to adjusting the pitch angle, the roll angle, and the yaw angle of the three-dimensional dynamic icon 101.
  • the specific angles of the above seven cases may be equivalent adjustments, that is, how much the angle of the aircraft 200 changes, and the angle of the three-dimensional dynamic icon 101 changes, for example, the aircraft 200 is up to 60 degrees, the three-dimensional dynamic icon The 101 is also raised 60 degrees, the aircraft 200 is lowered 60 degrees, and the 3D dynamic icon 101 is also lowered 60 degrees.
  • the respective angles corresponding to the adjustment of the three-dimensional dynamic icon 101 may also be adjusted according to a preset ratio, for example, assuming that the predetermined ratio is 2:1, the aircraft 200 is up 60 degrees, the three-dimensional dynamic icon 101 is tilted 30 degrees, and the aircraft 200 The vehicle is tilted by 60 degrees, and the three-dimensional dynamic icon 101 is lowered by 30 degrees.
  • the respective angles of the three-dimensional dynamic icon 101 may be adjusted according to a preset mapping relationship.
  • the aircraft 200 is tilted 60 degrees, according to preset
  • the three-dimensional dynamic icon 101 is tilted by 30 degrees, and the aircraft 200 is tilted by 60 degrees.
  • the three-dimensional dynamic icon 101 is lowered by 30 degrees according to a preset mapping relationship.
  • the respective angles of the three-dimensional dynamic icon 101 may be adjusted correspondingly.
  • the angle is adjusted at a fixed angle. For example, if the elevation angle of the aircraft 200 is 0-30 degrees, the three-dimensional dynamic icon 101 is raised by 15 degrees, and the upward angle of the aircraft 200 is 30-60.
  • the angle of the three-dimensional dynamic icon 101 is 30 degrees, and if the angle of elevation of the aircraft 200 is 60-90 degrees, the three-dimensional dynamic icon 101 is raised by 60 degrees and the like.
  • adjusting the respective angles of the three-dimensional dynamic icon 101 is performed in an equivalent adjustment manner, so that the user can feel the posture change of the aircraft 200 in synchronization.
  • the corresponding adjustment may also be adjusted according to the user's autonomous input of respective corresponding angles, for example, the user inputs a pitch angle of 30 degrees, a roll angle of 50 degrees, and a yaw angle of 60 degrees; then, once the aircraft 200 is pitched, regardless of the pitch angle of the aircraft 200 How many, the three-dimensional dynamic icon 101 is uniformly tilted by 30 degrees; once the aircraft 200 rolls, regardless of the roll angle of the aircraft 200, the three-dimensional dynamic icon 101 rolls over 30 degrees; once the aircraft 200 yaws, regardless of the yaw of the aircraft 200 The angle of the three-dimensional dynamic icon 101 is yawed by 30 degrees.
  • the control device 110 includes a communication unit 111, a processor 112, and a display 113.
  • the communication unit 111 is used to implement S1, and the processor 112 is used to implement S2 and S4. , S5 and S6, the display 113 is used to implement S3 and S7. That is, the communication unit 111 is configured to receive the shape of the aircraft 200. State information.
  • the processor 112 is configured to acquire a flight trajectory of the aircraft 200 according to the state information, adjust a display trajectory of the three-dimensional dynamic icon 101 according to the flight trajectory, acquire a flight attitude according to the state information, and adjust the three-dimensional dynamic icon 101 according to the flight attitude. Show gestures.
  • the display 113 is for displaying a three-dimensional dynamic icon 101 corresponding to a flight trajectory and for displaying text information 103 corresponding to the flight attitude of the aircraft 200.
  • the manner in which the processor 112 acquires the flight trajectory includes the above three methods, and the manner in which the display posture of the three-dimensional dynamic icon 101 is adjusted according to the flight attitude is the above seven types, and details are not described herein again.
  • 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 includes one of a display terminal having a display function, such as a mobile phone, a tablet computer, a remote controller (such as a screen remote controller), a smart watch, smart glasses, a smart helmet, other virtual reality wear devices, and other augmented reality wear devices. Or a variety.
  • the display 113 in the electronic device 100 can display other related information of the aircraft 200 being monitored or operated, such as the aircraft 200, in addition to displaying the three-dimensional dynamic icon 101 and the text information 103 corresponding to the flight path. Its own model and parameter information, flight parameters of the aircraft 200, images or video images taken by the aircraft 200, and interface information for manipulating the aircraft 200, and the like.
  • the following shows an example of displaying the three-dimensional dynamic icon 101, and adjusting the three-dimensional dynamic icon 101 corresponding to the flight trajectory according to the flight trajectory and the flight attitude, and displaying the corresponding text information 103:
  • the user clicks on any position of the display 113.
  • the display 113 displays the cursor 102 in the locking direction; then, the communication unit 111 receives the state information of the aircraft 200, and the processor 112 acquires the flight trajectory of the aircraft 200 according to the state information, and the acquisition mode is any one of the above three manners; Referring to Figure 10, the display 113 will display a three-dimensional dynamic icon 101 corresponding to the flight path.
  • the flight trajectory of the aircraft 200 can be immediately known by observing the three-dimensional dynamic icon 101 displayed in the display 113. If the flight path of the aircraft 200 changes at this time, as shown in FIG. 11, the user clicks on another position on the display 113, the flight path of the aircraft 200 changes, and the flight attitude also rolls, the processor 112
  • the display trajectory of the three-dimensional dynamic icon 101 is adjusted according to the flight trajectory and the display posture of the three-dimensional dynamic icon 101 is adjusted according to the flight attitude, as the linear trajectory in FIG. 10 is adjusted to the curved trajectory of FIG. 11, and a roll occurs.
  • the user can intuitively feel that the flight path of the aircraft 200 also changes from a straight track to a curved track, and a roll occurs.
  • the display 113 also displays the text information 103 corresponding to the scroll to remind the user that the text information 103 of "rolling 60 degrees" is displayed.
  • the user can intuitively feel that the trajectory of the aircraft 200 also changes from a linear trajectory to a curved trajectory, and a roll occurs, and the corresponding text information 103 can be quickly read from the display 113. If the text information "up” or “down” is displayed on the display 113, the user can quickly know that the aircraft 200 is "rising” or "falling".
  • the three-dimensional dynamic icon 101 is in the shape of an arrow in which the highlight color is displayed, and is gradually narrowed as the display 113 displays the depth direction.
  • the three-dimensional dynamic icon 101 includes a plurality of sub-arrows arranged in sequence and spaced apart from each other.
  • the sub-arrows at the end of the three-dimensional dynamic icon 101 are displayed one by one in a swallowed manner with the flight direction of the aircraft 200.
  • the three-dimensional dynamic icon 101 may not be a highlight color, and the setting may be relatively bright.
  • the color for example: is designed to give a visual impact of red, green, or yellow.
  • the three-dimensional dynamic icon 101 can also be any other color or a simple combination or a gradual combination of a plurality of colors, as long as the user can be prompted.
  • the shape of the three-dimensional dynamic icon 101 is not limited to an arrow shape, and may be a triangle, a trapezoid, a column shape displayed in a scroll, or the like.
  • the control method, the control device 110, and the electronic device 100 in the embodiment of the present invention control the display 113 to display the three-dimensional dynamic icon 101 embodying the flight trajectory of the aircraft 200 intelligently and with a sense of depth, so that when the user monitors or operates the aircraft 200, With a strong sense of depth, the user experience is enhanced. If it is displayed together with the images taken by the aircraft 200 and transmitted back, it will give the user an immersive feeling and greatly enhance the user experience.
  • the processor 112 can adjust the display trajectory and the display posture of the three-dimensional dynamic icon 101 according to the flight trajectory and the flight attitude of the aircraft 200, and the display 113 also displays the text information 103 corresponding to the flight attitude to remind the user that the user can pass the three-dimensional dynamic
  • the display trajectory and display posture of the icon 101 intuitively sense the flight trajectory and flight attitude of the aircraft 200, and can quickly read corresponding text information from the display 113, further enhancing 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.

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Abstract

一种控制方法、控制装置（110）及电子装置（100），其中，控制方法用于控制电子装置（100），电子装置（100）能够与飞行器（200）通信。控制方法包括：接收飞行器（200）的状态信息（S1）；根据状态信息获取飞行器（200）的飞行轨迹（S2）；及显示与飞行轨迹对应的三维动态图标（101）（S3）。

Description

控制方法、控制装置及电子装置 技术领域
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。
背景技术
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，当电子设备远程监控或操控飞行器时，无法有纵深感地显示被监控或***控的飞行器的飞行轨迹，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，所述电子装置能够与飞行器通信，所述控制方法包括以下步骤：
接收所述飞行器的状态信息；
根据所述状态信息获取所述飞行器的飞行轨迹；及
显示与所述飞行轨迹对应的三维动态图标。
在某些实施方式中，所述控制方法还包括：
根据所述飞行轨迹调整所述三维动态图标的显示轨迹。
在某些实施方式中，所述状态信息包括自主飞行模式下的规划轨迹，所述根据所述状态信息获取所述飞行器的飞行轨迹的步骤是通过在所述状态信息中读取所述规划轨迹来实现。
在某些实施方式中，所述状态信息包括手控飞行模式下所述飞行器预测的未来轨迹，所述根据所述状态信息获取所述飞行器的飞行轨迹的步骤是通过在所述状态信息中读取所述未来轨迹来实现。
在某些实施方式中，所述状态信息包括所述飞行器的实时轨迹，所述根据所述状态信息获取所述飞行器的飞行轨迹的步骤是通过在读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现。
在某些实施方式中，所述三维动态图标呈箭头状，并随着显示深度方向逐渐变窄。
在某些实施方式中，所述三维动态图标呈高亮色。
在某些实施方式中，所述三维动态图标包括依序排列且彼此间隔的多个子箭头，所述 三维动态图标末端的子箭头随着所述飞行器的飞行方向逐个以被吞没的方式显示。
在某些实施方式中，所述状态信息包括飞行姿态，所述控制方法还包括：
根据所述状态信息获取所述飞行姿态；及
根据所述飞行姿态调整所述三维动态图标的显示姿态。
在某些实施方式中，所述飞行姿态包括所述飞行器的俯仰角、和/或滚转角、和/或偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：
根据所述飞行器的俯仰角调整所述三维动态图标的俯仰角；和/或
根据所述飞行器的滚转角调整所述三维动态图标的滚转角；和/或
根据所述飞行器的偏航角调整所述三维动态图标的偏航角。
在某些实施方式中，所述控制方法还包括：
显示与所述飞行器的飞行姿态对应的文字信息。
本发明提供一种控制装置，用于控制电子装置，所述电子装置能够与飞行器通信，所述控制装置包括：
通信单元，用于接收所述飞行器的状态信息；
处理器，用于根据所述状态信息获取所述飞行器的飞行轨迹；及
显示器，用于显示与所述飞行轨迹对应的三维动态图标。
在某些实施方式中，所述处理器还用于根据所述飞行轨迹调整所述三维动态图标的显示轨迹。
在某些实施方式中，所述状态信息包括自主飞行模式下的规划轨迹，所述处理器是通过在所述状态信息中读取所述规划轨迹来实现获取所述飞行器的飞行轨迹。
在某些实施方式中，所述状态信息包括手控飞行模式下所述飞行器预测的未来轨迹，所述处理器是通过在所述状态信息中读取所述未来轨迹来实现获取所述飞行器的飞行轨迹。
在某些实施方式中，所述状态信息包括所述飞行器的实时轨迹，所述处理器是在所述通信单元接收所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现获取所述飞行器的飞行轨迹。
在某些实施方式中，所述三维动态图标呈箭头状，并随着显示深度方向逐渐变窄。
在某些实施方式中，所述三维动态图标呈高亮色。
在某些实施方式中，所述三维动态图标包括依序排列且彼此间隔的多个子箭头，所述三维动态图标末端的子箭头随着所述飞行器的飞行方向逐个以被吞没的方式显示。
在某些实施方式中，所述状态信息包括飞行姿态，所述处理器还用于：
根据所述状态信息获取所述飞行姿态；及
根据所述飞行姿态调整所述三维动态图标的显示姿态。
在某些实施方式中，所述飞行姿态包括所述飞行器的俯仰角、和/或滚转角、和/或偏航角：
所述处理器用于根据所述飞行器的俯仰角调整所述三维动态图标的俯仰角来实现调整所述三维动态图标的显示姿态；和/或
所述处理器用于根据所述飞行器的滚转角调整所述三维动态图标的滚转角来实现调整所述三维动态图标的显示姿态；和/或
所述处理器用于根据所述飞行器的偏航角调整所述三维动态图标的偏航角来实现调整所述三维动态图标的显示姿态。
在某些实施方式中，所述显示器还用于显示与所述飞行器的飞行姿态对应的文字信息。
本发明提供一种电子装置，所述电子装置包括如上任意一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中的一种或者多种。
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、有纵深感地显示体现飞行器的飞行轨迹的三维动态图标，使得用户在监控或操作飞行器时，有了强烈的纵深感，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。
附图说明
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控制方法的流程示意图。
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控制方法的流程示意图。
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的显示器显示界面的示意图。
图10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11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12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13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14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15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16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。
具体实施方式
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9-10，本发明一实施方式的控制方法，被控制装置110使用以控制电子装置100，电子装置100能够与飞行器200通信。所述控制方法包括：
S1，接收飞行器200的状态信息；
S2，根据状态信息获取飞行器200的飞行轨迹；及
S3，显示与飞行轨迹对应的三维动态图标101。
其中，飞行轨迹的获取方式包括以下三种：
第一、若飞行器200在自主飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的自主飞行模块或由位于电子装置100中的自主飞行模块提前规划好的，此时，状态信息包括自主飞行模块提前规划好的的规划轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述规划轨迹来实现的。
第二、若飞行器200在手控飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的轨迹预测模块根据飞行过程中的实时轨迹预测出来的，此时，状态信息包括飞行器200中的轨迹预测模块预测的未来轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述未来轨迹来实现。
第三、若飞行器200在手控飞行模式下飞行，飞行器200记录自己飞行过程中的实时轨迹，此时，状态信息包括飞行器200的实时轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现，此时，轨迹预测模块在飞行器200之外。
请参阅图2，在本发明一实施方式的控制装置110中，控制装置110包括通信单元111、处理器112、及显示器113，可分别用于实现S1、S2及S3。也就是说，通信单元111用于接收飞行器200的状态信息。处理器112用于根据状态信息获取飞行器200的飞行轨迹。显示器113用于显示与飞行轨迹对应的三维动态图标101。其中，处理器112获取飞行轨迹的方式包括上述控制方法中的三种方式，在此不再赘述。
本发明实施方式的控制装置110可应用于本发明一实施方式的电子装置100中。
电子装置100包括手机、平板电脑、遥控器(如带屏遥控器)、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。如图15-16所示，电子装置100中的显示器113除了显示与飞行轨迹对应的三维动态图标101，还能显示被监控或操作的飞行器200的其他相关信息，例如飞行器200自身的型号与参数信息、飞行器200的飞行参数、经飞行器200拍摄的图像或视频画面、以及用于操控飞行器200的界面信息等等。
下面举例来说明显示与飞行轨迹对应的三维动态图标101：首先，请参阅图9，用户点击显示器113上任意一位置，显示器113显示锁定方向的光标102；接着，通信单元111接收飞行器200的状态信息，处理器112根据状态信息获取飞行器200的飞行轨迹，获取方式为上述三种方式中的任意一种；然后，请参阅图10，显示器113就会显示与飞行轨迹对应的三维动态图标101。如此，可以通过观察显示器113中显示的三 维动态图标101来立即了解飞行器200的飞行轨迹。三维动态图标101呈高亮色显示的箭头状，并随着显示器113显示深度方向逐渐变窄。具体地，三维动态图标101包括依序排列且彼此间隔的多个子箭头，本实施方式中，三维动态图标101末端的子箭头随着飞行器200的飞行方向逐个以被吞没的方式显示。当然，三维动态图标101也可以不为高亮色，可以设置比较鲜艳的颜色，例如：设计成能给人以视觉冲击的红色、绿色、或黄色。当然，三维动态图标101还可以是任意其他颜色或者多种颜色的简单组合或渐变组合，只要能够给用户以提示即可。三维动态图标101的形状也不局限于箭头状，还可为三角形、梯形、滚动显示的柱状等等。
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113智能地、有纵深感地显示体现飞行器200的飞行轨迹的三维动态图标101，使得用户在监控或操作飞行器200时，有了强烈的纵深感，提升了用户体验。如果搭配经飞行器200拍摄并图传回的图像一起显示，就会让用户有身临其境的感觉，大大提升了用户体验。
请一并参阅图2、图4及图9-11，本发明一实施方式的控制方法，被控制装置110使用以控制电子装置100，电子装置100能够与飞行器200通信。所述控制方法包括：
S1，接收飞行器200的状态信息；
S2，根据状态信息获取飞行器200的飞行轨迹；
S3，显示与飞行轨迹对应的三维动态图标101；及
S4，根据飞行轨迹调整三维动态图标101的显示轨迹。
其中，飞行轨迹的获取方式包括以下三种：
第一、若飞行器200在自主飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的自主飞行模块或由位于电子装置100中的自主飞行模块提前规划好的，此时，状态信息包括自主飞行模块提前规划好的的规划轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述规划轨迹来实现的。
第二、若飞行器200在手控飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的轨迹预测模块根据飞行过程中的实时轨迹预测出来的，此时，状态信息包括飞行器200中的轨迹预测模块预测的未来轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述未来轨迹来实现。
第三、若飞行器200在手控飞行模式下飞行，飞行器200记录自己飞行过程中的实时轨迹，此时，状态信息包括飞行器200的实时轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现，此时，轨迹预测模块在飞行器200之外。
请结合图2，在本发明一实施方式的控制装置110中，控制装置110包括通信单元111、 处理器112、及显示器113，通信单元111用于实现S1，处理器112用于实现S2及S4，显示器113用于实现S3。也就是说，通信单元111用于接收飞行器200的状态信息。处理器112用于根据状态信息获取飞行器200的飞行轨迹、及用于根据飞行轨迹调整三维动态图标101的显示轨迹。显示器113用于显示与飞行轨迹对应的三维动态图标101。其中，处理器112获取飞行轨迹的方式包括上述控制方法中的三种方式，在此不再赘述。
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中。电子装置100包括手机、平板电脑、遥控器(如带屏遥控器)、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。如图15-16所示，电子装置100中的显示器113除了显示与飞行轨迹对应的三维动态图标101，还能显示被监控或操作的飞行器200的其他相关信息，例如飞行器200自身的型号与参数信息、飞行器200的飞行参数、经飞行器200拍摄的图像或视频画面、以及用于操控飞行器200的界面信息等等。
下面举例来说明显示三维动态图标101、及根据飞行轨迹调整与飞行轨迹对应的三维动态图标101：首先，请参阅图9，用户点击显示器113上任意一位置，显示器113显示锁定方向的光标102；接着，通信单元111接收飞行器200的状态信息，处理器112根据状态信息获取飞行器200的飞行轨迹，获取方式为上述三种方式中的任意一种；然后，请参阅图10，显示器113就会显示与飞行轨迹对应的三维动态图标101。如此，可以通过观察显示器113中显示的三维动态图标101来立即了解飞行器200的飞行轨迹。若此时飞行器200的飞行轨迹发生了变化，如图11所示，用户点击显示器113上的另一个位置，飞行器200的飞行轨迹就发生变化，处理器112就会根据飞行轨迹调整三维动态图标101的显示轨迹，如由图10中的直线轨迹调整为图11的曲线轨迹，此时，用户能够直观的感受到飞行器200的飞行轨迹也由直线轨迹转变为曲线轨迹。三维动态图标101呈高亮色显示的箭头状，并随着显示器113显示深度方向逐渐变窄。具体地，三维动态图标101包括依序排列且彼此间隔的多个子箭头，本实施方式中，三维动态图标101末端的子箭头随着飞行器200的飞行方向逐个以被吞没的方式显示。当然，三维动态图标101也可以不为高亮色，可以设置比较鲜艳的颜色，例如：设计成能给人以视觉冲击的红色、绿色、或黄色。当然，三维动态图标101还可以是任意其他颜色或者多种颜色的简单组合或渐变组合，只要能够给用户以提示即可。三维动态图标101的形状也不局限于箭头状，还可为三角形、梯形、滚动显示的柱状等等。
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113智能地、有纵深感地显示体现飞行器200的飞行轨迹的三维动态图标101，使得用户在监控或操作飞行器200时，有了强烈的纵深感，提升了用户体验。如果搭配经飞行器200拍摄并图传 回的图像一起显示，就会让用户有身临其境的感觉，大大提升了用户体验。而且，处理器112能够根据飞行器200的飞行轨迹调整三维动态图标101的显示轨迹，用户便能够通过三维动态图标101的显示轨迹直观感受飞行器200的飞行轨迹，进一步提升了用户体验。
请一并参阅图2、图5、图9-10及图12-14，本发明一实施方式的控制方法，被控制装置110使用以控制电子装置100，电子装置100能够与飞行器200通信。所述控制方法包括：
S1，接收飞行器200的状态信息；
S2，根据状态信息获取飞行器200的飞行轨迹；
S3，显示与飞行轨迹对应的三维动态图标101；
S5，根据状态信息获取飞行姿态；及
S6，根据飞行姿态调整三维动态图标101的显示姿态。
其中，飞行轨迹的获取方式包括以下三种：
第一、若飞行器200在自主飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的自主飞行模块或由位于电子装置100中的自主飞行模块提前规划好的，此时，状态信息包括自主飞行模块提前规划好的的规划轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述规划轨迹来实现的。
第二、若飞行器200在手控飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的轨迹预测模块根据飞行过程中的实时轨迹预测出来的，此时，状态信息包括飞行器200中的轨迹预测模块预测的未来轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述未来轨迹来实现。
第三、若飞行器200在手控飞行模式下飞行，飞行器200记录自己飞行过程中的实时轨迹，此时，状态信息包括飞行器200的实时轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现，此时，轨迹预测模块在飞行器200之外。
飞行器200的飞行姿态包括俯仰角、滚转角、及偏航角三种。因此，步骤S6及S7就包括以下七种方式：
(1)根据状态信息获取飞行器200的俯仰角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角对应调整三维动态图标101的俯仰角；
(2)根据状态信息获取飞行器200的滚转角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角对应调整三维动态图标101的滚转角；
(3)根据状态信息获取飞行器200的偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的偏航角对应调整三维动态图标101的偏航角；
(4)根据状态信息获取飞行器200的俯仰角及滚转角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及滚转角对应调整三维动态图标101的俯仰角及滚转角；
(5)根据状态信息获取飞行器200的俯仰角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及偏航角对应调整三维动态图标101的俯仰角及偏航角；
(6)根据状态信息获取飞行器200的滚转角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角及偏航角对应调整三维动态图标101的滚转角及偏航角；
(7)根据状态信息获取飞行器200的俯仰角、滚转角、及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角、滚转角、及偏航角对应调整三维动态图标101的俯仰角、滚转角、及偏航角。
以上7种情况的具体对应调整三维动态图标101的各个角度可以是等同调整，即飞行器200的角度变化多少，三维动态图标101的角度变化也多少，例如：飞行器200上仰60度，三维动态图标101也上仰60度，飞行器200下俯60度，三维动态图标101也下俯60度。或者，对应调整三维动态图标101的各个角度还可以是按预先设定的比例调整，例如：假设预定比例为2：1，飞行器200上仰60度，三维动态图标101上仰30度，飞行器200下俯60度，三维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是按预先设定的映射关系来调整，例如：飞行器200上仰60度，根据预先设定的映射关系三维动态图标101上仰30度，飞行器200下俯60度，根据预先设定的映射关系三维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是根据预先设定的飞行器的各个角度范围来以固定角度调整，例如，飞行器200上仰角度若在0-30度，则三维动态图标101上仰15度，飞行器200上仰角度若在30-60度，则三维动态图标101上仰30度，飞行器200上仰角度若在60-90度，则三维动态图标101上仰60度等等。优选地，调整三维动态图标101的各个角度是以等同调整方式进行的，如此能让用户同步感受飞行器200的姿态变化。对应调整还可以是按照由用户自主输入各个对应的角度来调整，例如用户输入俯仰角30度、滚转角50度、及偏航角60度；则一旦飞行器200发生俯仰，不管飞行器200的俯仰角度多少，三维动态图标101一律俯仰30度；一旦飞行器200发生滚转，不管飞行器200的滚转角度多少，三维动态图标101一律滚转30度；一旦飞行 器200发生偏航，不管飞行器200的偏航角度多少，三维动态图标101一律偏航30度。
请结合图2，在本发明一实施方式的控制装置110中，控制装置110包括通信单元111、处理器112、及显示器113，通信单元111用于实现S1，处理器112用于实现S2、S5及S6，显示器113用于实现S3。也就是说，通信单元111用于接收飞行器200的状态信息。处理器112用于根据状态信息获取飞行器200的飞行轨迹、用于根据状态信息获取飞行姿态、及用于根据飞行姿态调整三维动态图标101的显示姿态。显示器113用于显示与飞行轨迹对应的三维动态图标101。其中，处理器112获取飞行轨迹的方式包括上述控制方法中的三种方式，根据飞行姿态调整三维动态图标101的显示姿态的方式为以上七种，在此不再赘述。
本发明实施方式的控制装置110可应用于本发明一实施方式的电子装置100中。电子装置100包括手机、平板电脑、遥控器(如带屏遥控器)、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。如图15-16所示，电子装置100中的显示器113除了显示与飞行轨迹对应的三维动态图标101，还能显示被监控或操作的飞行器200的其他相关信息，例如飞行器200自身的型号与参数信息、飞行器200的飞行参数、经飞行器200拍摄的图像或视频画面、以及用于操控飞行器200的界面信息等等。
下面举例来说明显示三维动态图标101、及根据飞行姿态调整与飞行轨迹对应的三维动态图标101：首先，请参阅图9，用户点击显示器113任意一位置，显示器113显示锁定方向的光标102；接着，通信单元111接收飞行器200的状态信息，处理器112根据状态信息获取飞行器200的飞行轨迹，获取方式为上述三种方式中的任意一种；然后，请参阅图10，显示器113就会显示与飞行轨迹对应的三维动态图标101。如此，可以通过观察显示器113中显示的三维动态图标101来立即了解飞行器200的飞行轨迹。若此时飞行器200的飞行姿态发生了变化，处理器112就会根据飞行姿态调整三维动态图标101的显示姿态，例如，若飞行器200发生了偏航，飞行器200的机头朝向非飞行方向时，处理器112获取偏航角，对应地，三维动态图标101也会发生对应角度的偏航(如图12所示)。当飞行器200的偏航角达到180度，对应地，三维动态图标101也会发生对应180度的偏航(如图13所示)，而且此时三维动态图标101的显示轨迹可根据飞行器200的前进速度信息逐级消隐。更进一步地，若此时当用户操控遥控器油门往下时，三维动态图标101原有的显示轨迹透明度降低，往下箭头隐现(从图13到图14可以体现出此变化)；当用户操控遥控器油门往上时，三维动态图标101原有的显示轨迹透明度降低，往上箭头隐现。三维动态图标101呈高亮色显示的箭头状，并随着显示器113显示深度方向逐渐变窄。具体地，三维动态图标101包括依序排列且彼此间隔的多个子箭头，本实施方式中，三维动态图标101末端的子 箭头随着飞行器200的飞行方向逐个以被吞没的方式显示。当然，三维动态图标101也可以不为高亮色，可以设置比较鲜艳的颜色，例如：设计成能给人以视觉冲击的红色、绿色、或黄色。当然，三维动态图标101还可以是任意其他颜色或者多种颜色的简单组合或渐变组合，只要能够给用户以提示即可。三维动态图标101的形状也不局限于箭头状，还可为三角形、梯形、滚动显示的柱状等等。
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113智能地、有纵深感地显示体现飞行器200的飞行轨迹的三维动态图标101，使得用户在监控或操作飞行器200时，有了强烈的纵深感，提升了用户体验。如果搭配经飞行器200拍摄并图传回的图像一起显示，就会让用户有身临其境的感觉，大大提升了用户体验。而且，处理器112能够根据飞行器200的飞行姿态调整三维动态图标的显示姿态，用户便能够通过三维动态图标101的显示姿态直观感受飞行器200的飞行姿态，进一步提升了用户体验。
请一并参阅图2、图6、图9-10及图12-13，本发明一实施方式的控制方法，被控制装置110使用以控制电子装置100，电子装置100能够与飞行器200通信。所述控制方法包括：
S1，接收飞行器200的状态信息；
S2，根据状态信息获取飞行器200的飞行轨迹；
S3，显示与飞行轨迹对应的三维动态图标101；
S5，根据状态信息获取飞行姿态；
S6，根据飞行姿态调整三维动态图标101的显示姿态；及
S7，显示与飞行器200的飞行姿态对应的文字信息103。
其中，飞行轨迹的获取方式包括以下三种：
第一、若飞行器200在自主飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的自主飞行模块或由位于电子装置100中的自主飞行模块提前规划好的，此时，状态信息包括自主飞行模块提前规划好的的规划轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述规划轨迹来实现的。
第二、若飞行器200在手控飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的轨迹预测模块根据飞行过程中的实时轨迹预测出来的，此时，状态信息包括飞行器200中的轨迹预测模块预测的未来轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述未来轨迹来实现。
第三、若飞行器200在手控飞行模式下飞行，飞行器200记录自己飞行过程中的实时轨迹，此时，状态信息包括飞行器200的实时轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的 未来轨迹来实现，此时，轨迹预测模块在飞行器200之外。
飞行器200的飞行姿态包括俯仰角、滚转角、及偏航角三种。因此，步骤S6及S7就包括以下七种方式：
(1)根据状态信息获取飞行器200的俯仰角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角对应调整三维动态图标101的俯仰角；
(2)根据状态信息获取飞行器200的滚转角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角对应调整三维动态图标101的滚转角；
(3)根据状态信息获取飞行器200的偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的偏航角对应调整三维动态图标101的偏航角；
(4)根据状态信息获取飞行器200的俯仰角及滚转角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及滚转角对应调整三维动态图标101的俯仰角及滚转角；
(5)根据状态信息获取飞行器200的俯仰角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及偏航角对应调整三维动态图标101的俯仰角及偏航角；
(6)根据状态信息获取飞行器200的滚转角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角及偏航角对应调整三维动态图标101的滚转角及偏航角；
(7)根据状态信息获取飞行器200的俯仰角、滚转角、及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角、滚转角、及偏航角对应调整三维动态图标101的俯仰角、滚转角、及偏航角。
以上7种情况的具体对应调整三维动态图标101的各个角度可以是等同调整，即飞行器200的角度变化多少，三维动态图标101的角度变化也多少，例如：飞行器200上仰60度，三维动态图标101也上仰60度，飞行器200下俯60度，三维动态图标101也下俯60度。或者，对应调整三维动态图标101的各个角度还可以是按预先设定的比例调整，例如：假设预定比例为2：1，飞行器200上仰60度，三维动态图标101上仰30度，飞行器200下俯60度，三维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是按预先设定的映射关系来调整，例如：飞行器200上仰60度，根据预先设定的映射关系三维动态图标101上仰30度，飞行器200下俯60度，根据预先设定的映射关系三 维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是根据预先设定的飞行器的各个角度范围来以固定角度调整，例如，飞行器200上仰角度若在0-30度，则三维动态图标101上仰15度，飞行器200上仰角度若在30-60度，则三维动态图标101上仰30度，飞行器200上仰角度若在60-90度，则三维动态图标101上仰60度等等。优选地，调整三维动态图标101的各个角度是以等同调整方式进行的，如此能让用户同步感受飞行器200的姿态变化。对应调整还可以是按照由用户自主输入各个对应的角度来调整，例如用户输入俯仰角30度、滚转角50度、及偏航角60度；则一旦飞行器200发生俯仰，不管飞行器200的俯仰角度多少，三维动态图标101一律俯仰30度；一旦飞行器200发生滚转，不管飞行器200的滚转角度多少，三维动态图标101一律滚转30度；一旦飞行器200发生偏航，不管飞行器200的偏航角度多少，三维动态图标101一律偏航30度。
请结合图2，在本发明一实施方式的控制装置110中，控制装置110包括通信单元111、处理器112、及显示器113，通信单元111用于实现S1，处理器112用于实现S2、S5及S6，显示器113用于实现S3及S7。也就是说，通信单元111用于接收飞行器200的状态信息。处理器112用于根据状态信息获取飞行器200的飞行轨迹、用于根据状态信息获取飞行姿态、及用于根据飞行姿态调整三维动态图标101的显示姿态。显示器113用于显示与飞行轨迹对应的三维动态图标101及用于显示与飞行器200的飞行姿态对应的文字信息103。其中，处理器112获取飞行轨迹的方式包括上述控制方法中的三种方式，根据飞行姿态调整三维动态图标101的显示姿态的方式为以上七种，在此不再赘述。
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中。电子装置100包括手机、平板电脑、遥控器(如带屏遥控器)、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。如图15-16所示，电子装置100中的显示器113除了显示与飞行轨迹对应的三维动态图标101及文字信息103外，还能显示被监控或操作的飞行器200的其他相关信息，例如飞行器200自身的型号与参数信息、飞行器200的飞行参数、经飞行器200拍摄的图像或视频画面、以及用于操控飞行器200的界面信息等等。
下面举例来说明显示三维动态图标101、根据飞行姿态调整与飞行轨迹对应的三维动态图标101及显示对应的文字信息103：首先，请结合图9，用户点击显示器113任意一位置，显示器113显示锁定方向的光标102；接着，通信单元111接收飞行器200的状态信息，处理器112根据状态信息获取飞行器200的飞行轨迹，获取方式为上述三种方式中的任意一种；然后，请参阅图10，显示器113就会显示与飞行轨迹对应的三维动态图标101。如此，可以通过观察显示器113中显示的三维动态图标101来立即了解飞行器200的飞行轨迹。若此时飞行器200的飞行姿态发生了变化，处理器112就会根据飞行姿态调整三维动 态图标101的显示姿态，例如，若飞行器200发生了偏航，飞行器200的机头朝向非飞行方向时，处理器112获取偏航角，对应地，三维动态图标101也会发生对应角度的偏航(如图12所示)。当飞行器200的偏航角达到180度，对应地，三维动态图标101也会发生对应180度的偏航(如图13所示)，而且此时三维动态图标101的显示轨迹可根据飞行器200的前进速度信息逐级消隐。显示器113还显示与偏航对应的文字信息103以提醒用户，如：由图10中的三维动态图标101变为图15中发生了偏航的三维动态图标101，且显示“偏航180度”的文字信息103。此时，用户能够直观的感受到飞行器200发生了偏航并能够快速地从显示器113中读到对应的文字信息103。若显示器113中显示“上升”或“下降”的文字信息，用户就能够迅速地了解飞行器200正在“上升”或正在“下降”。三维动态图标101呈高亮色显示的箭头状，并随着显示器113显示深度方向逐渐变窄。具体地，三维动态图标101包括依序排列且彼此间隔的多个子箭头，本实施方式中，三维动态图标101末端的子箭头随着飞行器200的飞行方向逐个以被吞没的方式显示。当然，三维动态图标101也可以不为高亮色，可以设置比较鲜艳的颜色，例如：设计成能给人以视觉冲击的红色、绿色、或黄色。当然，三维动态图标101还可以是任意其他颜色或者多种颜色的简单组合或渐变组合，只要能够给用户以提示即可。三维动态图标101的形状也不局限于箭头状，还可为三角形、梯形、滚动显示的柱状等等。
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113智能地、有纵深感地显示体现飞行器200的飞行轨迹的三维动态图标101，使得用户在监控或操作飞行器200时，有了强烈的纵深感，提升了用户体验。如果搭配经飞行器200拍摄并图传回的图像一起显示，就会让用户有身临其境的感觉，大大提升了用户体验。而且，处理器112能够根据飞行器200的飞行姿态调整三维动态图标的显示姿态，显示器113还显示与飞行姿态对应的文字信息103以提醒用户，用户便能够通过三维动态图标101的显示姿态直观感受飞行器200的飞行姿态及能够快速地从显示器113上读到对应的文字信息103，进一步提升了用户体验。
请一并参阅图2、图7及图9-11，本发明一实施方式的控制方法，被控制装置110使用以控制电子装置100，电子装置100能够与飞行器200通信。所述控制方法包括：
S1，接收飞行器200的状态信息；
S2，根据状态信息获取飞行器200的飞行轨迹；
S3，显示与飞行轨迹对应的三维动态图标101；
S4，根据飞行轨迹调整三维动态图标101的显示轨迹；
S5，根据状态信息获取飞行姿态；及
S6，根据飞行姿态调整三维动态图标101的显示姿态。
其中，飞行轨迹的获取方式包括以下三种：
第一、若飞行器200在自主飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的自主飞行模块或由位于电子装置100中的自主飞行模块提前规划好的，此时，状态信息包括自主飞行模块提前规划好的的规划轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述规划轨迹来实现的。
第二、若飞行器200在手控飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的轨迹预测模块根据飞行过程中的实时轨迹预测出来的，此时，状态信息包括飞行器200中的轨迹预测模块预测的未来轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述未来轨迹来实现。
第三、若飞行器200在手控飞行模式下飞行，飞行器200记录自己飞行过程中的实时轨迹，此时，状态信息包括飞行器200的实时轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现，此时，轨迹预测模块在飞行器200之外。
飞行器200的飞行姿态包括俯仰角、滚转角、及偏航角三种。因此，步骤S6及S7就包括以下七种方式：
(1)根据状态信息获取飞行器200的俯仰角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角对应调整三维动态图标101的俯仰角；
(2)根据状态信息获取飞行器200的滚转角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角对应调整三维动态图标101的滚转角；
(3)根据状态信息获取飞行器200的偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的偏航角对应调整三维动态图标101的偏航角；
(4)根据状态信息获取飞行器200的俯仰角及滚转角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及滚转角对应调整三维动态图标101的俯仰角及滚转角；
(5)根据状态信息获取飞行器200的俯仰角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及偏航角对应调整三维动态图标101的俯仰角及偏航角；
(6)根据状态信息获取飞行器200的滚转角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角及偏航角对应调整三维动 态图标101的滚转角及偏航角；
(7)根据状态信息获取飞行器200的俯仰角、滚转角、及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角、滚转角、及偏航角对应调整三维动态图标101的俯仰角、滚转角、及偏航角。
以上7种情况的具体对应调整三维动态图标101的各个角度可以是等同调整，即飞行器200的角度变化多少，三维动态图标101的角度变化也多少，例如：飞行器200上仰60度，三维动态图标101也上仰60度，飞行器200下俯60度，三维动态图标101也下俯60度。或者，对应调整三维动态图标101的各个角度还可以是按预先设定的比例调整，例如：假设预定比例为2：1，飞行器200上仰60度，三维动态图标101上仰30度，飞行器200下俯60度，三维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是按预先设定的映射关系来调整，例如：飞行器200上仰60度，根据预先设定的映射关系三维动态图标101上仰30度，飞行器200下俯60度，根据预先设定的映射关系三维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是根据预先设定的飞行器的各个角度范围来以固定角度调整，例如，飞行器200上仰角度若在0-30度，则三维动态图标101上仰15度，飞行器200上仰角度若在30-60度，则三维动态图标101上仰30度，飞行器200上仰角度若在60-90度，则三维动态图标101上仰60度等等。优选地，调整三维动态图标101的各个角度是以等同调整方式进行的，如此能让用户同步感受飞行器200的姿态变化。对应调整还可以是按照由用户自主输入各个对应的角度来调整，例如用户输入俯仰角30度、滚转角50度、及偏航角60度；则一旦飞行器200发生俯仰，不管飞行器200的俯仰角度多少，三维动态图标101一律俯仰30度；一旦飞行器200发生滚转，不管飞行器200的滚转角度多少，三维动态图标101一律滚转30度；一旦飞行器200发生偏航，不管飞行器200的偏航角度多少，三维动态图标101一律偏航30度。
请结合图2，在本发明一实施方式的控制装置110中，控制装置110包括通信单元111、处理器112、及显示器113，通信单元111用于实现S1，处理器112用于实现S2、S4、S5及S6，显示器113用于实现S3。也就是说，通信单元111用于接收飞行器200的状态信息。处理器112用于根据状态信息获取飞行器200的飞行轨迹、用于根据飞行轨迹调整三维动态图标101的显示轨迹、用于根据状态信息获取飞行姿态、及用于根据飞行姿态调整三维动态图标101的显示姿态。显示器113用于显示与飞行轨迹对应的三维动态图标101。其中，处理器112获取飞行轨迹的方式包括上述控制方法中的三种方式，根据飞行姿态调整三维动态图标101的显示姿态的方式为以上七种，在此不再赘述。
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中。电子装置100包括手机、平板电脑、遥控器(如带屏遥控器)、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。如图15-16所示，电子装置100中的显示器113除了显示与飞行轨迹对应的三维动态图标101，还能显示被监控或操作的飞行器200的其他相关信息，例如飞行器200自身的型号与参数信息、飞行器200的飞行参数、经飞行器200拍摄的图像或视频画面、以及用于操控飞行器200的界面信息等等。
下面举例来说明显示三维动态图标101、根据飞行轨迹及飞行姿态调整与飞行轨迹对应的三维动态图标101：首先，请参阅图9，用户点击显示器113任意一位置，显示器113显示锁定方向的光标102；接着，通信单元111接收飞行器200的状态信息，处理器112根据状态信息获取飞行器200的飞行轨迹，获取方式为上述三种方式中的任意一种；然后，请参阅图10，显示器113就会显示与飞行轨迹对应的三维动态图标101。如此，可以通过观察显示器113中显示的三维动态图标101来立即了解飞行器200的飞行轨迹。若此时飞行器200的飞行轨迹及飞行姿态发生了变化，如图11所示，用户点击显示器113上的另一个位置，飞行器200的飞行轨迹就发生变化，且飞行姿态也发生了横滚，处理器112就会根据飞行轨迹调整三维动态图标101的显示轨迹及根据飞行姿态调整三维动态图标101的显示姿态，如由图10中的直线轨迹调整为图11的曲线轨迹，且发生了横滚，此时，用户能够直观的感受到飞行器200的飞行轨迹也由直线轨迹转变为曲线轨迹，且发生了横滚。三维动态图标101呈高亮色显示的箭头状，并随着显示器113显示深度方向逐渐变窄。具体地，三维动态图标101包括依序排列且彼此间隔的多个子箭头，本实施方式中，三维动态图标101末端的子箭头随着飞行器200的飞行方向逐个以被吞没的方式显示。当然，三维动态图标101也可以不为高亮色，可以设置比较鲜艳的颜色，例如：设计成能给人以视觉冲击的红色、绿色、或黄色。当然，三维动态图标101还可以是任意其他颜色或者多种颜色的简单组合或渐变组合，只要能够给用户以提示即可。三维动态图标101的形状也不局限于箭头状，还可为三角形、梯形、滚动显示的柱状等等。
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113智能地、有纵深感地显示体现飞行器200的飞行轨迹的三维动态图标101，使得用户在监控或操作飞行器200时，有了强烈的纵深感，提升了用户体验。如果搭配经飞行器200拍摄并图传回的图像一起显示，就会让用户有身临其境的感觉，大大提升了用户体验。而且，处理器112能够根据飞行器200的飞行轨迹及飞行姿态分别调整三维动态图标101的显示轨迹及显示姿态，用户便能够通过三维动态图标101的显示轨迹及显示姿态直观感受飞行器200的飞行轨迹及飞行姿态，进一步提升了用户体验。
请一并参阅图2及图8-11，本发明一实施方式的控制方法，被控制装置110使用以控制电子装置100，电子装置100能够与飞行器200通信。所述控制方法包括：
S1，接收飞行器200的状态信息；
S2，根据状态信息获取飞行器200的飞行轨迹；
S3，显示与飞行轨迹对应的三维动态图标101；
S4，根据飞行轨迹调整三维动态图标101的显示轨迹；
S5，根据状态信息获取飞行姿态；及
S6，根据飞行姿态调整三维动态图标101的显示姿态；及
S7，显示与飞行器200的飞行姿态对应的文字信息103。
其中，飞行轨迹的获取方式包括以下三种：
第一、若飞行器200在自主飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的自主飞行模块或由位于电子装置100中的自主飞行模块提前规划好的，此时，状态信息包括自主飞行模块提前规划好的的规划轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述规划轨迹来实现的。
第二、若飞行器200在手控飞行模式下飞行，飞行器200的飞行轨迹是由飞行器200中的轨迹预测模块根据飞行过程中的实时轨迹预测出来的，此时，状态信息包括飞行器200中的轨迹预测模块预测的未来轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过在状态信息中直接读取所述未来轨迹来实现。
第三、若飞行器200在手控飞行模式下飞行，飞行器200记录自己飞行过程中的实时轨迹，此时，状态信息包括飞行器200的实时轨迹，对应地，所述根据状态信息获取飞行器200的飞行轨迹的步骤是通过读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现，此时，轨迹预测模块在飞行器200之外。
飞行器200的飞行姿态包括俯仰角、滚转角、及偏航角三种。因此，步骤S6及S7就包括以下七种方式：
(1)根据状态信息获取飞行器200的俯仰角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角对应调整三维动态图标101的俯仰角；
(2)根据状态信息获取飞行器200的滚转角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角对应调整三维动态图标101的滚转角；
(3)根据状态信息获取飞行器200的偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的偏航角对应调整三维动态图标101的偏航角；
(4)根据状态信息获取飞行器200的俯仰角及滚转角，所述根据所述飞行姿态调整所述 三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及滚转角对应调整三维动态图标101的俯仰角及滚转角；
(5)根据状态信息获取飞行器200的俯仰角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角及偏航角对应调整三维动态图标101的俯仰角及偏航角；
(6)根据状态信息获取飞行器200的滚转角及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的滚转角及偏航角对应调整三维动态图标101的滚转角及偏航角；
(7)根据状态信息获取飞行器200的俯仰角、滚转角、及偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：根据飞行器200的俯仰角、滚转角、及偏航角对应调整三维动态图标101的俯仰角、滚转角、及偏航角。
以上7种情况的具体对应调整三维动态图标101的各个角度可以是等同调整，即飞行器200的角度变化多少，三维动态图标101的角度变化也多少，例如：飞行器200上仰60度，三维动态图标101也上仰60度，飞行器200下俯60度，三维动态图标101也下俯60度。或者，对应调整三维动态图标101的各个角度还可以是按预先设定的比例调整，例如：假设预定比例为2：1，飞行器200上仰60度，三维动态图标101上仰30度，飞行器200下俯60度，三维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是按预先设定的映射关系来调整，例如：飞行器200上仰60度，根据预先设定的映射关系三维动态图标101上仰30度，飞行器200下俯60度，根据预先设定的映射关系三维动态图标101下俯30度；或者，对应调整三维动态图标101的各个角度还可以是根据预先设定的飞行器的各个角度范围来以固定角度调整，例如，飞行器200上仰角度若在0-30度，则三维动态图标101上仰15度，飞行器200上仰角度若在30-60度，则三维动态图标101上仰30度，飞行器200上仰角度若在60-90度，则三维动态图标101上仰60度等等。优选地，调整三维动态图标101的各个角度是以等同调整方式进行的，如此能让用户同步感受飞行器200的姿态变化。对应调整还可以是按照由用户自主输入各个对应的角度来调整，例如用户输入俯仰角30度、滚转角50度、及偏航角60度；则一旦飞行器200发生俯仰，不管飞行器200的俯仰角度多少，三维动态图标101一律俯仰30度；一旦飞行器200发生滚转，不管飞行器200的滚转角度多少，三维动态图标101一律滚转30度；一旦飞行器200发生偏航，不管飞行器200的偏航角度多少，三维动态图标101一律偏航30度。
请结合图2，在本发明一实施方式的控制装置110中，控制装置110包括通信单元111、处理器112、及显示器113，通信单元111用于实现S1，处理器112用于实现S2、S4、S5及S6，显示器113用于实现S3及S7。也就是说，通信单元111用于接收飞行器200的状 态信息。处理器112用于根据状态信息获取飞行器200的飞行轨迹、用于根据飞行轨迹调整三维动态图标101的显示轨迹、用于根据状态信息获取飞行姿态、及用于根据飞行姿态调整三维动态图标101的显示姿态。显示器113用于显示与飞行轨迹对应的三维动态图标101及用于显示与飞行器200的飞行姿态对应的文字信息103。其中，处理器112获取飞行轨迹的方式包括上述控制方法中的三种方式，根据飞行姿态调整三维动态图标101的显示姿态的方式为以上七种，在此不再赘述。
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中。电子装置100包括手机、平板电脑、遥控器(如带屏遥控器)、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。如图15-16所示，电子装置100中的显示器113除了显示与飞行轨迹对应的三维动态图标101及文字信息103外，还能显示被监控或操作的飞行器200的其他相关信息，例如飞行器200自身的型号与参数信息、飞行器200的飞行参数、经飞行器200拍摄的图像或视频画面、以及用于操控飞行器200的界面信息等等。
下面举例来说明显示三维动态图标101、及根据飞行轨迹及飞行姿态调整与飞行轨迹对应的三维动态图标101并显示对应的文字信息103：首先，请参阅图9，用户点击显示器113任意一位置，显示器113显示锁定方向的光标102；接着，通信单元111接收飞行器200的状态信息，处理器112根据状态信息获取飞行器200的飞行轨迹，获取方式为上述三种方式中的任意一种；然后，请参阅图10，显示器113就会显示与飞行轨迹对应的三维动态图标101。如此，可以通过观察显示器113中显示的三维动态图标101来立即了解飞行器200的飞行轨迹。若此时飞行器200的飞行轨迹发生了变化，如图11所示，用户点击显示器113上的另一个位置，飞行器200的飞行轨迹就会发生改变，且飞行姿态也发生了横滚，处理器112就会根据飞行轨迹调整三维动态图标101的显示轨迹及根据飞行姿态调整三维动态图标101的显示姿态，如由图10中的直线轨迹调整为图11的曲线轨迹，且发生了横滚，此时，用户能够直观的感受到飞行器200的飞行轨迹也由直线轨迹转变为曲线轨迹，且发生了横滚。同时，显示器113还显示与横滚对应的文字信息103以提醒用户，即显示“横滚60度”的文字信息103。此时，用户能够直观的感受到飞行器200的轨迹也由直线轨迹转变为曲线轨迹，且发生了横滚，并能够快速地从显示器113中读到对应的文字信息103。若显示器113中显示“上升”或“下降”的文字信息，用户就能够迅速地了解飞行器200正在“上升”或正在“下降”。三维动态图标101呈高亮色显示的箭头状，并随着显示器113显示深度方向逐渐变窄。具体地，三维动态图标101包括依序排列且彼此间隔的多个子箭头，本实施方式中，三维动态图标101末端的子箭头随着飞行器200的飞行方向逐个以被吞没的方式显示。当然，三维动态图标101也可以不为高亮色，可以设置比较鲜艳 的颜色，例如：设计成能给人以视觉冲击的红色、绿色、或黄色。当然，三维动态图标101还可以是任意其他颜色或者多种颜色的简单组合或渐变组合，只要能够给用户以提示即可。三维动态图标101的形状也不局限于箭头状，还可为三角形、梯形、滚动显示的柱状等等。
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113智能地、有纵深感地显示体现飞行器200的飞行轨迹的三维动态图标101，使得用户在监控或操作飞行器200时，有了强烈的纵深感，提升了用户体验。如果搭配经飞行器200拍摄并图传回的图像一起显示，就会让用户有身临其境的感觉，大大提升了用户体验。而且，处理器112能够根据飞行器200的飞行轨迹及飞行姿态分别调整三维动态图标101的显示轨迹及显示姿态，显示器113还显示与飞行姿态对应的文字信息103以提醒用户，用户便能够通过三维动态图标101的显示轨迹及显示姿态直观感受飞行器200的飞行轨迹及飞行姿态，并能够快速地从显示器113上读到对应的文字信息，进一步提升了用户体验。
在本说明书的描述中，参考术语“某些实施方式”、“一实施方式”、“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 (24)

  1. 一种控制方法，用于控制电子装置，所述电子装置能够与飞行器通信，其特征在于，所述控制方法包括以下步骤：
    接收所述飞行器的状态信息；
    根据所述状态信息获取所述飞行器的飞行轨迹；及
    显示与所述飞行轨迹对应的三维动态图标。
  2. 如权利要求1所述的控制方法，其特征在于，所述控制方法还包括：
    根据所述飞行轨迹调整所述三维动态图标的显示轨迹。
  3. 如权利要求2所述的控制方法，其特征在于，所述状态信息包括自主飞行模式下的规划轨迹，所述根据所述状态信息获取所述飞行器的飞行轨迹的步骤是通过在所述状态信息中读取所述规划轨迹来实现。
  4. 如权利要求2所述的控制方法，其特征在于，所述状态信息包括手控飞行模式下所述飞行器预测的未来轨迹，所述根据所述状态信息获取所述飞行器的飞行轨迹的步骤是通过在所述状态信息中读取所述未来轨迹来实现。
  5. 如权利要求2所述的控制方法，其特征在于，所述状态信息包括所述飞行器的实时轨迹，所述根据所述状态信息获取所述飞行器的飞行轨迹的步骤是通过在读取所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现。
  6. 如权利要求1所述的控制方法，其特征在于，所述三维动态图标呈箭头状，并随着显示深度方向逐渐变窄。
  7. 如权利要求1所述的控制方法，其特征在于，所述三维动态图标呈高亮色。
  8. 如权利要求1所述的控制方法，其特征在于，所述三维动态图标包括依序排列且彼此间隔的多个子箭头，所述三维动态图标末端的子箭头随着所述飞行器的飞行方向逐个以被吞没的方式显示。
  9. 如权利要求1-8任意一项所述的控制方法，其特征在于，所述状态信息包括飞行姿 态，所述控制方法还包括：
    根据所述状态信息获取所述飞行姿态；及
    根据所述飞行姿态调整所述三维动态图标的显示姿态。
  10. 如权利要求9所述的控制方法，其特征在于，所述飞行姿态包括所述飞行器的俯仰角、和/或滚转角、和/或偏航角，所述根据所述飞行姿态调整所述三维动态图标的显示姿态的步骤包括：
    根据所述飞行器的俯仰角调整所述三维动态图标的俯仰角；和/或
    根据所述飞行器的滚转角调整所述三维动态图标的滚转角；和/或
    根据所述飞行器的偏航角调整所述三维动态图标的偏航角。
  11. 如权利要求9所述的控制方法，其特征在于，所述控制方法还包括：
    显示与所述飞行器的飞行姿态对应的文字信息。
  12. 一种控制装置，用于控制电子装置，所述电子装置能够与飞行器通信，其特征在于，所述控制装置包括：
    通信单元，用于接收所述飞行器的状态信息；
    处理器，用于根据所述状态信息获取所述飞行器的飞行轨迹；及
    显示器，用于显示与所述飞行轨迹对应的三维动态图标。
  13. 如权利要求12所述的控制装置，其特征在于，所述处理器还用于根据所述飞行轨迹调整所述三维动态图标的显示轨迹。
  14. 如权利要求13所述的控制装置，其特征在于，所述状态信息包括自主飞行模式下的规划轨迹，所述处理器是通过在所述状态信息中读取所述规划轨迹来实现获取所述飞行器的飞行轨迹。
  15. 如权利要求13所述的控制装置，其特征在于，所述状态信息包括手控飞行模式下所述飞行器预测的未来轨迹，所述处理器是通过在所述状态信息中读取所述未来轨迹来实现获取所述飞行器的飞行轨迹。
  16. 如权利要求13所述的控制装置，其特征在于，所述状态信息包括所述飞行器的实 时轨迹，所述处理器是在所述通信单元接收所述实时轨迹后根据所述实时轨迹预测所述飞行器的未来轨迹来实现获取所述飞行器的飞行轨迹。
  17. 如权利要求12所述的控制装置，其特征在于，所述三维动态图标呈箭头状，并随着显示深度方向逐渐变窄。
  18. 如权利要求12所述的控制装置，其特征在于，所述三维动态图标呈高亮色。
  19. 如权利要求12所述的控制装置，其特征在于，所述三维动态图标包括依序排列且彼此间隔的多个子箭头，所述三维动态图标末端的子箭头随着所述飞行器的飞行方向逐个以被吞没的方式显示。
  20. 如权利要求12-19任意一项所述的控制装置，其特征在于，所述状态信息包括飞行姿态，所述处理器还用于：
    根据所述状态信息获取所述飞行姿态；及
    根据所述飞行姿态调整所述三维动态图标的显示姿态。
  21. 如权利要求20所述的控制装置，其特征在于，所述飞行姿态包括所述飞行器的俯仰角、和/或滚转角、和/或偏航角：
    所述处理器用于根据所述飞行器的俯仰角调整所述三维动态图标的俯仰角来实现调整所述三维动态图标的显示姿态；和/或
    所述处理器用于根据所述飞行器的滚转角调整所述三维动态图标的滚转角来实现调整所述三维动态图标的显示姿态；和/或
    所述处理器用于根据所述飞行器的偏航角调整所述三维动态图标的偏航角来实现调整所述三维动态图标的显示姿态。
  22. 如权利要求20所述的控制装置，其特征在于，所述显示器还用于显示与所述飞行器的飞行姿态对应的文字信息。
  23. 一种电子装置，其特征在于，所述电子装置包括如权利要求12-22任意一项所述的控制装置。
  24. 如权利要求23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中的一种或者多种。
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CN107077150B (zh) 2018-12-18
US20190265730A1 (en) 2019-08-29

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