CN108595175A - Digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method - Google Patents
Digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method Download PDFInfo
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- CN108595175A CN108595175A CN201810284824.4A CN201810284824A CN108595175A CN 108595175 A CN108595175 A CN 108595175A CN 201810284824 A CN201810284824 A CN 201810284824A CN 108595175 A CN108595175 A CN 108595175A
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- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F8/00—Arrangements for software engineering
- G06F8/30—Creation or generation of source code
- G06F8/38—Creation or generation of source code for implementing user interfaces
Abstract
The invention discloses a kind of digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method, the two-dimentional interface information that can be designed according to user is automatic to write the source program of two-dimentional display interface, and generates corresponding interface.Two-dimentional interface source program writing process shows the interface information storage file of widget library and unified format description dependent on established two dimension.Artificial intelligence program person writes the data transmission code of control correlative code, control and digital aircraft real-time status amount data source included in the correlative code of interface integrity attribute, interface according to storage file successively, the correlative code that data are shown in control.Compile deployment after the completion of writing automatically to source program.Using artificial intelligence Writing method, it is automatically performed two dimension and shows that source program is write, avoid repetitive operation, improve development efficiency.By the above-mentioned means, the present invention can effectively realize that the Real-time Two-dimensional of digital aircraft correlated condition amount is shown.
Description
Technical field
The present invention relates to two-dimentional display technologies, more particularly to a kind of digital aircraft Real-time Two-dimensional display interface source program
Artificial intelligence Writing method.
Background technology
Digital aircraft is constituted according to the building block of actual aircraft, and parameter keeps one with actual aircraft
It causes, by carrying out dynamic analog to aircraft subsystems and its component, can show the working condition of aerocraft system, take off
Show the operation principle of each system and mutual cooperation relation.For each component, principle model, telecommunication interface mould are established
Type, error model, failure model go out the state of flight of actual aircraft in ground simulation, have reflected the operation principle of component,
The reliability of telecommunication interface and component when use.
Digital aircraft is an individual human window when running, and the dynamic of quantity of state becomes in the aerial vehicle simulation period
Change cannot be clear and intuitive reflect, user cannot monitor the operating status of digital aircraft in real time, it is therefore desirable to rely on number
The mating auxiliary show tools of word aircraft, two dimension display is one such means.The interface of traditional two-dimentional display interface
Style and shown state information are fixed, and for different aircraft, such as satellite, guided missile, opportunity of combat, and user is closed
The quantity of state of the heart is different, therefore different mating displays circle is just needed for the dynamic analog process of different aircraft
Face.The present invention can voluntarily select quantity of state of concern, reduce repetition work according to user demand designed, designed display interface
Make, improves working efficiency.
Invention content
In view of this, the present invention provides a kind of writings of digital aircraft Real-time Two-dimensional display interface source program artificial intelligence
Method, in the design process of digital aircraft two dimension display interface, people need to only make the decision process of quantity of state to be shown, keep away
The overlapping development work for having exempted from people, improves program development efficiency.
To achieve the goals above, the present invention adopts the following technical scheme that：
A kind of digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method, implementation method is specifically such as
Under：
It establishes two dimension and shows widget library；
Show that widget library completes the design of two-dimentional display interface in designing module in conjunction with the two dimension；
The interface result is carried out to the description of unified format；
Two-dimentional display interface source code is write according to design result；
Digital aircraft quantity of state real-time display.
Preferably, two dimension shows that the specific control of widget library includes：
Chart, text box, slider bar, indicator light, progress bar, label, container, list, horizontal line, a variety of controls including vertical line
Part.User can build the frame of display interface by pulling the above control, and the clear control work(in interface is arranged by control property
Energy.Control property includes the data attribute that itself attribute is mutually bound with control, and user can voluntarily change as needed.
Preferably, show that widget library completes the specific step that two-dimentional display interface designs in designing module in conjunction with the two dimension
Suddenly include：
Appropriate control is selected from widget library, determines the positions and dimensions information of each control；
Quantity of state to be shown can be being selected in dispaly state amount list；
Binding relationship is established between selection quantity of state and control, determines which quantity of state each control shows；
Determine the attribute informations such as display interface background, font.
Preferably, the interface result is subjected to specifically including for unified format description：
Two-dimentional display interface design result is saved as to the file of unified format description.
The design result description of two-dimentional display interface is including but not limited to interface title, interface number, operational mode, interface
Background color, interface background picture, interface dimensions information (height, width), interface layout (line information) and control information；
Form of presentation is including but not limited to standardized data library format, standardized XML.
Preferably, writing two-dimentional display interface source code steps according to design result includes：
Write interface integrity attribute code；
Write in interface includes control correlative code；
Write the data transmission code of control and digital aircraft real-time status amount data source；
Write the code of quantity of state display function；
Preferably, the specific steps of digital aircraft quantity of state real-time display include：
The state numerical quantity and quantity of state ID that simulated program transmits are got by communication interface；
It is matched with the control bundle state information in two-dimentional display interface design result；
It determines the corresponding display control of data, realizes that data are shown.
Preferably, simulated program and two dimension show that program communication modes use TCP/IP communication modes.
Interface module and widget library have provided the interface platform of unified standard to the user, and user can be according to certainly
Body needs, and builds the display interface with oneself style, the problem of avoiding by unified format constraint so that the scope of application of interface
Wider, application is more flexible.And the unified format descriptor of interface final design result is preserved with set by unified standard preservation
The interface of meter, the interface involved by different user can be mutually general, facilitates the unified scale development at interface.Digital aircraft with
Unified communication modes equally ensure that the versatility between the aircraft of different model and interface between interface.
Therefore, digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method can be widely used in a variety of
The related data of type aircraft is shown, in the design process of digital aircraft two dimension display interface, people need to only make and wait showing
Show the decision process of quantity of state, for example, control dragging and dispaly state amount decision, remaining process is independently complete by computer
At high efficiency and time conservation.
Description of the drawings
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technology description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 attached drawings are digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method flow chart；
Fig. 2 attached drawings are digital aircraft Real-time Two-dimensional display design module；
Fig. 3 attached drawings are digital aircraft Real-time Two-dimensional display interface.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Step flow chart shown in FIG. 1 for the present invention, below in conjunction with the accompanying drawings and by specific embodiment to the present invention
It is described in further detail.
The invention particularly discloses a kind of digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method,
Writing method includes the following steps：
Step 1：It establishes two dimension and shows widget library；
Step 2：Show that widget library completes the design of two-dimentional display interface in designing module in conjunction with the two dimension；
Step 3：The interface result is carried out to the description of unified format；
Step 4：Two-dimentional display interface source code is write according to design result
Step 5：Digital aircraft quantity of state real-time display
In the following, will one by one be described to above-mentioned key step.
1, widget library is established
Include chart, text box, slider bar, indicator light, progress bar, label, container, list, horizontal line, vertical line in widget library
Many controls inside.
Chart mainly realizes the relational graph drawn between quantity of state, wherein including two class relational graphs；The first is default type
Relational graph mainly draws a certain digital aircraft quantity of state and changes with time image, and the dynamic for reacting the state information is special
Property, play the role of the monitoring of quantity of state；Second class is X-Y type plan views, and main draw appoints arbitrary two kinds of digital aircraft states
The relation curve of amount reacts the relevance between two states amount.The graph color of dispaly state amount, class of a curve can be arranged in user
Type, the data attributes such as vertex type and maximum realistic number；And it can be arranged comprising figure ground, the controls category such as graphics transparency
Property.
Text box is the carrier of display data, can be by way of dragging by the flight state amount in the database of load
Information is bound with text box, realizes the real-time display of pulled quantity of state；User can be arranged comprising font, transparency, background face
Color, frame control property.
Slider bar auxiliary user adjusts the concrete numerical value of certain quantity of states.Definition status amount adjustable extent, i.e. maximum value
And minimum value, realize the adjusting control of quantity of state.Slider bar data attribute includes maximum value, minimum value；Control property includes the back of the body
Scape, transparency, frame etc..
Indicator light auxiliary user knows the certain state status of aircraft, and state includes only yes/no, i.e., lamp is bright when 0 and 1,1,
Lamp goes out when 0.Control property includes indicator light transparency, panel background, transparency, frame, font size color etc..
Progress bar plays the function of dispaly state amount emulation progress, maximum value and the minimum of user setting simulation state amount
Value, by comparing the emulation progress of current state numerical quantity and the relationship real-time display simulation state amount of max min.Into
It includes the control properties such as background transparent degree and frame, the data attributes such as data maximums minimum value to spend item.
Label plays the role of display text.Control property includes the background of label, transparency, the color size of font
Deng.
Container shows the surplus information of certain quantity of states, such as electricity, fuel quantity etc..Container data attribute includes state
Max min is measured, control property includes background, transparency, frame etc..
Button plays the role of controlling background program.Button is bound with certain background programs, can be by clicking button triggering
The program bound therewith, or play the role of controlling simulation velocity.The data attribute of button includes optional binding subprogram, can
Choosing binding sentence etc., control property includes button background, font size, color, button binding function etc..
List is to show the relevant information of quantity of state in the form of a list.Table data attribute includes the time, quantity of state
Number, title, affiliated board title, quantity of state type, data length, reduction length, maximum value, minimum value, selectable value, engineering
Data etc.；Control property includes the background of list, frame, transparency etc..
Horizontal line, vertical line play the combing effect of the relationship between control, show the relationship between each control.Control property packet
Color containing lines, frame, thickness etc..
2, the design of two-dimentional display interface is completed in designing module
It is required from the two-dimentional display interface of widget library selection in generated two-dimentional display interface programming module
Control, using ship to air missile as embodiment, drawing the control selected when ship to air missile has：Label, text box and indicator light.User is logical
It crosses the form pulled control is added in display frame, wherein label is used to store the necessary word in interface, and text box is used
Store correlated condition amount to be shown, indicator light is used for showing guided missile state, including transmitting, hit, explosion etc..
In generated two-dimentional display interface programming module quantity of state to be shown, this reality are selected from quantity of state list
Applying the quantity of state chosen in example is：Three axis component of naval vessel position and speed, three axis component of carrier aircraft position and speed, missile position and
Three axis component of speed and guided missile state etc..The binding information of control and quantity of state is stored in unified format descriptor, with red
For square guided missile position Input shows guided missile x-axis location components, by Input and quantity of state MissileOrbits-
3-1 is bound together, therefore should be stored the control in the unified format descriptor for preserving Input information and be shown number
According to relevant information, information include band display data number, band display data title.The interface of completion is designed in designing module
Blank is as shown in Figure 2.
The attributes such as design interface size, background, color in interface property setting, and it is stored in unified format descriptor
In.
3, design result unifies format description
The design result description of two-dimentional display interface is including but not limited to interface title, interface number, operational mode, interface
Background color, interface background picture, interface dimensions information (height, width), interface layout (line information) and control information.
Form of presentation is including but not limited to standardized data library format, standardized XML.
XML descriptions are selected in two-dimentional display interface design result description here.
4, two-dimentional display interface source code is write according to design result
Artificial intelligence program person's writing process divides following four part：
Write interface integrity attribute code；
Write in interface includes control correlative code；
Write the data transmission code of control and digital aircraft real-time status amount data source；
Write the code of quantity of state display function；
Each process is hereafter described in detail successively.
Interface integrity attribute includes mainly interface size, layout, background, binding data library etc..Artificial intelligence program person reads
It goes bail for and deposits the xml document of design result and get above-mentioned attribute.Interface layout (n rows m row) points out that interface can be divided by n x
The rectangle of m grid composition, interface size (long, wide) record the size of the rectangle.Square of the artificial intelligence program person in the n x m
Rectangular coordinate system is established in shape interface, origin is located at the position of 0 row 0 row, and X-axis is line number, and Y-axis is columns, so far appoints in interface
Some positions can be uniquely determined by ranks.Background information is the absolute address of a certain background picture, is obtained artificial behind change of address
The picture is inserted into background by intelligent program person.With each digital aircraft quantity of state number of database purchase of two-dimentional interface binding
Value, artificial intelligence program person obtains database address, convenient for accessing at any time.
On the basis of completing above-mentioned interface integrity attribute program writing, each control corresponding source in two-dimentional interface is write
Code.Each relevant source code writing step of control is consistent, is followed successively by：Control property setting, control and quantity of state binding, control
It draws.
Wherein control property needs artificial intelligence program person to be obtained from the xml document for preserving design result, and attribute is main
Including the information such as control size, position, color, frame, write setting source code successively.Each control can be bound with quantity of state,
Pass through the shape of structure list to quantity of state ID according to quantity of state name acquiring by the database root of access storage configuration amount
Control ID, bound quantity of state title and the unified preservations of current quantity of state ID are established binding relationship by formula.Artificial intelligence program
After member gets the location information (row, column) of control, the control can be set in interface coordinate system described above at interface
In position, write display source code of the control in interface.With red missile position X-axis information text frame in the present embodiment
For control, line information is 3 row, 11 row, and dimension information is 1 width 3 of height, and program is sought in coordinate system established above
The position that coordinate is (3,11) is found, the Input that size is (1,3) is placed.
The data transmission code of control and digital aircraft is fixed code, which is stored in code library.Number
Word aircraft and type in the transmission channel a total of three of two-dimentional display interface, are kinetic parameter filing, device parameter respectively
Filing, telemetry filing.The transport channel type that artificial intelligence program person includes according to Contemporary Digital aircraft, from code library
In select corresponding fixed code, and complete to write.
Quantity of state display function code steps are followed successively by：Identification channel type receives data, control match cognization, state
Amount display.
Wherein, channel type identification rely on keyword, keyword be and the associated digital aircraft of two-dimentional display interface
It is ' Archive ' that build-in attribute, wherein dynamics, which file channel and the keyword in equipment filing channel, and telemetry files channel
Keyword is ' Telemetry ', writes matched related source code accordingly.Digital aircraft can be sent to two-dimentional display interface works as
The ID and numerical value of preceding quantity of state, according to the information got, artificial intelligence program person can write the matching of current quantity of state control
Source program related to display, principle are as follows：The structure list of quantity of state and control information must be preserved by accessing backstage, it is known that when
Preceding quantity of state ID can be matched to the structure for preserving the ID from structure list, and then obtain the control ID bound therewith,
So that it is determined that control, writing makes the correlated source code commands that the quantity of state is shown in the control bound with it.
5, data real-time display
The definition that kinetic parameter filing, device parameter filing and telemetry archive information mentioned above are transmitted is such as
Under：
It is digital aircraft that kinetic parameter, which files starting point, and digital aircraft sends data to dynamics profiling module,
The ID of data and numerical value are sent to two-dimentional display interface by profiling module.
It is digital aircraft that device parameter, which files starting point, and digital aircraft sends data to equipment profiling module, is filed
The ID of data and numerical value are sent to two-dimentional display interface by module.
It is digital aircraft that telemetry parameter, which files starting point, and telemetry group packet is sent to telemetering decoder module by aircraft,
Telemetry profiling module is sent data to after the completion of decoding, telemetry profiling module sends out the ID of telemetry and numerical value
It send to two-dimentional display interface.
By taking the red missile position X-axis information display process in the present embodiment as an example, digital missile simulated program is led
Position data, is sent to mating filing procedure by the real time data that sticking position is set, and filing procedure is according to by position numerical value and its ID
(69) it is sent to two-dimentional display interface program, two-dimentional display interface program can one by one be matched according to ID in control, be matched to text
This frame control TextBox1 shows the missile position data received in text box TextBox1, and so on complete it is all
The display of control bundle quantity of state.The two-dimentional interface final effect figure intelligently generated is as shown in Figure 3.
Each embodiment is described by the way of progressive in this specification, the highlights of each of the examples are with other
The difference of embodiment, just to refer each other for identical similar portion between each embodiment.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest range caused.
Claims (7)
1. digital aircraft Real-time Two-dimensional display interface source program artificial intelligence Writing method, which is characterized in that the writing side
Method includes the following steps：
Step 1：It establishes two dimension and shows widget library；
Step 2：Show that widget library completes the design of two-dimentional display interface in designing module in conjunction with the two dimension；
Step 3：The interface result is carried out to the description of unified format；
Step 4：Two-dimentional display interface source code is write according to design result；
Step 5：Digital aircraft quantity of state real-time display.
2. requiring the digital aircraft Real-time Two-dimensional display interface source program artificial intelligence writing side described in 1 according to right descriptions
Method, which is characterized in that the widget library in the step 1 refers to：It is made of the different function control in two-dimentional display interface
Set；
The control that is particularly shown in the step 1 includes but not limited to chart, text box, slider bar, indicator light, progress bar, mark
Label, container, list, horizontal line, vertical line.
3. requiring the digital aircraft Real-time Two-dimensional display interface source program artificial intelligence writing side described in 1 according to right descriptions
Method, which is characterized in that the step 2 specifically includes:
The control needed for user is selected from widget library, determines the positions and dimensions information of each control；
Quantity of state to be shown can be being selected in dispaly state amount list；
Binding relationship is established between selection quantity of state and control, determines which quantity of state each control shows；
Determine display interface background, font generic attribute information.
4. requiring the digital aircraft Real-time Two-dimensional display interface source program artificial intelligence writing side described in 1 according to right descriptions
Method, which is characterized in that the step 3 specifically includes:
Two-dimentional display interface design result is saved as to the file of unified format description；
The design result description of two-dimentional display interface is including but not limited to interface title, interface number, operational mode, interface background
Color, interface background picture, interface dimensions information height, width, interface layout line information and control information；
Form of presentation is including but not limited to standardized data library format, standardized XML.
5. requiring the digital aircraft Real-time Two-dimensional display interface source program artificial intelligence writing side described in 1 according to right descriptions
Method, which is characterized in that the step 4 includes：
Write interface integrity attribute code；
Write in interface includes control correlative code；
Write the data transmission code of control and digital aircraft real-time status amount data source；
Write the code of quantity of state display function.
6. requiring the digital aircraft Real-time Two-dimensional display interface source program artificial intelligence writing side described in 1 according to right descriptions
Method, which is characterized in that the specific steps of the step 5 include：
The state numerical quantity and quantity of state ID that simulated program transmits are got by communication interface；
It is matched with the control bundle state information in two-dimentional display interface design result；
It determines the corresponding display control of data, realizes that data are shown.
7. requiring the digital aircraft Real-time Two-dimensional display interface source program artificial intelligence writing side described in 1 according to right descriptions
Method, which is characterized in that the simulated program and two dimension show that program communication modes use TCP/IP communication modes.
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