CN106775215A - A kind of unmanned plane task window changing method - Google Patents
A kind of unmanned plane task window changing method Download PDFInfo
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- CN106775215A CN106775215A CN201611082334.3A CN201611082334A CN106775215A CN 106775215 A CN106775215 A CN 106775215A CN 201611082334 A CN201611082334 A CN 201611082334A CN 106775215 A CN106775215 A CN 106775215A
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- display
- information
- viewing area
- unmanned plane
- changing method
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
- G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
- G06F3/048—Interaction techniques based on graphical user interfaces [GUI]
- G06F3/0481—Interaction techniques based on graphical user interfaces [GUI] based on specific properties of the displayed interaction object or a metaphor-based environment, e.g. interaction with desktop elements like windows or icons, or assisted by a cursor's changing behaviour or appearance
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
- G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
- G06F3/048—Interaction techniques based on graphical user interfaces [GUI]
- G06F3/0481—Interaction techniques based on graphical user interfaces [GUI] based on specific properties of the displayed interaction object or a metaphor-based environment, e.g. interaction with desktop elements like windows or icons, or assisted by a cursor's changing behaviour or appearance
- G06F3/0483—Interaction with page-structured environments, e.g. book metaphor
-
- 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
- G06F3/0486—Drag-and-drop
Abstract
A kind of unmanned plane task window changing method of the present invention, belongs to aviation display control technology field.The present invention is comprised the following steps：Step one, determine windows display content；Step 2, design windows display system；Step 3, display content is associated with display window；Step 4, display window catch handover information, carry out windows exchange.The present invention is solved and is shown bulk information and the limited contradiction of display space simultaneously using display zoning scheme, improves the operating efficiency of operating personnel, reduces system design complexity.Realize rational deployment and the display of unmanned aerial vehicle station task system bulk information, operator both can simultaneously check the information of multiple windows in auxiliary viewing area, the information content of concern can be amplified to main viewing area again, check details, improve the operating efficiency of operator, the complexity of system design is reduced, display content is rationally solved more and the limited contradiction in viewing area.
Description
Technical field
The invention belongs to aviation display control technology field, and in particular to a kind of unmanned plane task window changing method.
Background technology
Display is that operator obtains attitude of flight vehicle navigation information, mission bit stream, the key equipment of situation of battlefield, with
The integration degree more and more higher such as cabin, display is developed to compact and integration direction, causes display picture
Information content is excessive, will have a strong impact on the judgement of operator；
The information of unmanned aerial vehicle station task system operating personnel's needs concern is more and more, and text importing mode is not straight enough
See, patterned display mode intuitively can efficiently show the back information of each equipment of task system, but cannot overcome figure
Change the screen space that display takes excessive with the limited contradiction in earth station's task system viewing area.
The content of the invention
The purpose of the present invention：In order to solve the above problems, the present invention proposes a kind of unmanned plane task window changing method,
Using display zoning scheme, solve and show bulk information and the limited contradiction of display space simultaneously, improve operator
The operating efficiency of member, reduces system design complexity.
Technical scheme：A kind of unmanned plane task window changing method, comprises the following steps:
Step one, determine windows display content；
Step 2, design windows display system；
Step 3, display content is associated with display window；
Step 4, display window catch handover information, carry out windows exchange.
Preferably, the display content in the step one includes：State of flight information, radar information, light thunder information, equipment
Status information, situation information.
Preferably, the display system in the step 2 is made up of a main viewing area and three auxiliary viewing areas.Described three
Individual auxiliary viewing area is respectively the first auxiliary viewing area, the second auxiliary viewing area, the 3rd auxiliary viewing area.
Preferably, the main viewing area association situation information, three auxiliary viewing areas are respectively associated state of flight information, radar
Information and equipment state information.
Preferably, in the step 4, display system cycle detection windows exchange mark catches handover information.
Preferably, the windows exchange is clicked the auxiliary viewing area of correspondence and is completed by left mouse button.
Technology beneficial effect of the invention：Realize the rational deployment of unmanned aerial vehicle station task system bulk information and show
Show, operator both can simultaneously check the information of multiple windows in auxiliary viewing area, can be amplified to the information content of concern again
Main viewing area, checks details, improves the operating efficiency of operator, reduces the complexity of system design, rationally solves
Display content is more and viewing area limited contradiction.
Brief description of the drawings
Fig. 1 is that a kind of display system interface of a preferred embodiment of unmanned plane task window changing method of the invention is illustrated
Figure.
Fig. 2 is a kind of windows exchange action capture of a preferred embodiment of unmanned plane task window changing method of the invention
Schematic diagram.
Fig. 3 is a kind of design flow diagram of a preferred embodiment of unmanned plane task window changing method of the invention.
Specific embodiment
To make the purpose, technical scheme and advantage of present invention implementation clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from start to finish or class
As label represent same or similar element or the element with same or like function.Described embodiment is the present invention
A part of embodiment, rather than whole embodiments.Embodiment below with reference to Description of Drawings is exemplary, it is intended to used
It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.Under
Face is described in detail with reference to accompanying drawing to embodiments of the invention.
In the description of the invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outward " are based on accompanying drawing institute
The orientation or position relationship for showing, are for only for ease of the description present invention and simplify description, rather than the dress for indicating or implying meaning
Put or element with specific orientation, with specific azimuth configuration and operation, therefore it is not intended that must be protected to the present invention
The limitation of scope.
Embodiments of the invention are described in detail below in conjunction with the accompanying drawings, refer to Fig. 1 to Fig. 3；
A kind of unmanned plane task window changing method, comprises the following steps:
A) windows display content, such as flight status information, radar information, light thunder information, equipment state information, state are determined
Gesture information etc.；
B) windows display system is designed, the size and number of main viewing area and auxiliary viewing area are determined；Show in the present embodiment
Show that system is made up of a main viewing area and three auxiliary viewing areas, three auxiliary viewing areas are respectively the first viewing area, second
Viewing area, the 3rd viewing area；
C) display content is associated with display window；First viewing area associates state of flight information, the second viewing area
Correlation rader information, the 3rd viewing area association equipment state information；
D) display window catches handover information, carries out windows exchange；
Auxiliary display window captures left mouse button and clicks on message, then it represents that operating personnel currently to the information of the window more
, then be set to windows exchange mark very by concern；Display system each cycle all checks windows exchange mark, if true, then will be by
The window of click amplifies and moves to main viewing area, the display window of current main viewing area is reduced and replaced the window being clicked
Display location.
The first auxiliary viewing area captures left mouse button and clicks on message in display system design, then it is assumed that the current task stage,
Earth station operating personnel more pay close attention to the state of flight information of the first auxiliary viewing area association, then cut the window of the first auxiliary viewing area
Dehorn will is set to very, and display system detects windows exchange and is masked as very, then state of flight information and other information are shown into interior
Appearance is exchanged.
The present invention realizes rational deployment and the display of unmanned aerial vehicle station task system bulk information, and operator both can be with
The information of multiple windows is checked simultaneously in auxiliary viewing area, the information content of concern main viewing area can be amplified to again, is checked in detail
Thin information, improves the operating efficiency of operator, reduces the complexity of system design, rationally solves display content many and aobvious
Show the limited contradiction in region.
It is last it is to be noted that：The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations.To the greatest extent
Pipe has been described in detail to the present invention with reference to the foregoing embodiments, it will be understood by those within the art that：It is still
Technical scheme described in foregoing embodiments can be modified, or which part technical characteristic is equally replaced
Change；And these modifications or replacement, do not make the essence of the essence disengaging various embodiments of the present invention technical scheme of appropriate technical solution
God and scope.
Claims (6)
1. a kind of unmanned plane task window changing method, it is characterised in that comprise the following steps:
Step one, determine windows display content；
Step 2, design windows display system；
Step 3, display content is associated with display window；
Step 4, display window catch handover information, carry out windows exchange.
2. unmanned plane task window changing method according to claim 1, it is characterised in that：Display in the step one
Content includes：State of flight information, radar information, light thunder information, equipment state information, situation information.
3. unmanned plane task window changing method according to claim 1, it is characterised in that：Display in the step 2
System is made up of a main viewing area and three auxiliary viewing areas, and three auxiliary viewing areas are respectively the first auxiliary viewing area, second
Auxiliary viewing area, the 3rd auxiliary viewing area.
4. unmanned plane task window changing method according to claim 1, it is characterised in that：The main viewing area association state
Gesture information, three auxiliary viewing areas are respectively associated state of flight information, radar information and equipment state information.
5. unmanned plane task window changing method according to claim 1, it is characterised in that：In the step 4, display
System cycle detection windows exchange mark, catches handover information.
6. unmanned plane task window changing method according to claim 5, it is characterised in that：The windows exchange passes through mouse
Mark left button is clicked the auxiliary viewing area of correspondence and is completed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201611082334.3A CN106775215A (en) | 2016-11-30 | 2016-11-30 | A kind of unmanned plane task window changing method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201611082334.3A CN106775215A (en) | 2016-11-30 | 2016-11-30 | A kind of unmanned plane task window changing method |
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| CN201611082334.3A Pending CN106775215A (en) | 2016-11-30 | 2016-11-30 | A kind of unmanned plane task window changing method |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108153459A (en) * | 2017-12-14 | 2018-06-12 | 中国航空工业集团公司成都飞机设计研究所 | A kind of display interface with function control status bar |
| CN108279826A (en) * | 2018-03-07 | 2018-07-13 | 北京布卡互动科技有限公司 | A kind of more videos and Multiple Document Interface alignment placement method |
| CN108513647A (en) * | 2017-06-16 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Control method, aerocraft system and display terminal |
| CN113741498A (en) * | 2021-08-25 | 2021-12-03 | 深圳市道通智能航空技术股份有限公司 | Zoom control method and device for pan-tilt camera and terminal |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003186593A (en) * | 2001-12-14 | 2003-07-04 | Sumitomo Electric Ind Ltd | Multiwindow display method and system thereof |
| CN101291398A (en) * | 2008-06-02 | 2008-10-22 | 深圳华为通信技术有限公司 | Method and apparatus of multi-image setting |
| CN104284236A (en) * | 2014-10-22 | 2015-01-14 | 百度在线网络技术（北京）有限公司 | Method and device for controlling and playing multi-video resources on terminal |
| CN105912288A (en) * | 2016-04-12 | 2016-08-31 | 上海易天无人飞行器科技有限公司 | Method and system for comprehensive processing display capable of monitoring flight state of unmanned aerial vehicle |
-
2016
- 2016-11-30 CN CN201611082334.3A patent/CN106775215A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003186593A (en) * | 2001-12-14 | 2003-07-04 | Sumitomo Electric Ind Ltd | Multiwindow display method and system thereof |
| CN101291398A (en) * | 2008-06-02 | 2008-10-22 | 深圳华为通信技术有限公司 | Method and apparatus of multi-image setting |
| CN104284236A (en) * | 2014-10-22 | 2015-01-14 | 百度在线网络技术（北京）有限公司 | Method and device for controlling and playing multi-video resources on terminal |
| CN105912288A (en) * | 2016-04-12 | 2016-08-31 | 上海易天无人飞行器科技有限公司 | Method and system for comprehensive processing display capable of monitoring flight state of unmanned aerial vehicle |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108513647A (en) * | 2017-06-16 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Control method, aerocraft system and display terminal |
| WO2018227623A1 (en) * | 2017-06-16 | 2018-12-20 | 深圳市大疆创新科技有限公司 | Control method, aircraft system, and display terminal |
| CN108153459A (en) * | 2017-12-14 | 2018-06-12 | 中国航空工业集团公司成都飞机设计研究所 | A kind of display interface with function control status bar |
| CN108279826A (en) * | 2018-03-07 | 2018-07-13 | 北京布卡互动科技有限公司 | A kind of more videos and Multiple Document Interface alignment placement method |
| CN113741498A (en) * | 2021-08-25 | 2021-12-03 | 深圳市道通智能航空技术股份有限公司 | Zoom control method and device for pan-tilt camera and terminal |
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