CN104317640B - The analogue system and method for a kind of Aerial Electronic Equipment - Google Patents
The analogue system and method for a kind of Aerial Electronic Equipment Download PDFInfo
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Abstract
This application discloses a kind of analogue system of Aerial Electronic Equipment and emulation mode, including：DD models, POP models and the data Internet, being predefined in DD models has the first data-interface, being predefined in POP models has data-interface, and DD models are connected by the first data-interface with data interaction network, and POP models are connected by the second data-interface with data interaction network.So, logical data is published to data interaction network by DD models, POP models read logical data from data interaction network, DD models and POP models are no longer directly docked, no longer it is the entirety of close coupling, data-interface only needs to change data-interface program when changing, when being modified to DD models and POP models, also data-interface will not be impacted, the versatility and durability of DD models and POP models can be strengthened, strengthen autgmentability and the flexibility of associative simulation, and concurrent development, improve development efficiency.
Description
Technical field
The application is related to Aerial Electronic Equipment simulation technical field, the analogue system of more particularly to a kind of Aerial Electronic Equipment and side
Method.
Background technology
As V model is in the popularization in avionics system Top-layer Design Method field, increasing designing unit will verify and confirm
Process introduce design cycle.For avionics Top-layer Design Method, a most important checking and confirmation means are by POP and DD
Associative simulation, do requirement validation with final user of service pilot.DD (Detail Design) is the letter of detailed design
Claim, refer mainly to the function logic detailed design of each equipment of avionics system；POP (Pilot Operation Procedures) is
The abbreviation of pilot operator specification, refers mainly to the detailed design of the operation interface and application method of pilot in aircraft cockpit.
In general, POP design can use some virtual instrument developing instruments, such as VAPS XT commonly used in the trade,
Altia, iDATA, QT etc., the POP models built using these instruments, are generally configured with interface and simple display control is patrolled
Volume；The design of DD models can use some logics or algorithm modeling tool, Simulink, Rhapsody such as commonly used in the trade
Deng, DD models can build with actual airborne equipment function identical logic, drive the operation at POP interfaces.User is in modeling tool
DD models are put up on (such as Simulink), after real time workshop and cross compile, DD models and POP models can be passed through
Between data-interface (including EBI and non-bus signaling interface etc.) DD models be sent to POP models be patterned
Interface operation, thereby using the mode of emulation come with pilot do demand link up and confirm.
POP general at present and DD combined simulation system, majority are building DD models by the way of intra process communication
During with POP models, some global variables are defined by dynamic base, DD models and POP models is accessed these variables, then will
DD models and POP models carry out code building, cross compile and downloading-running as an entirety, and one is compiled into emulation
Executable program, the data between DD models and POP models are completed by the intra process communication of global variable or shared drive
Interaction.
But, at least there are the following problems in the prior art：DD models and POP models are entered into line code as an entirety
Generation, cross compile and downloading-running, DD models and POP models can only be carried out simultaneously as an entirety in function call
Docking, with very strong coupled relation, every time when model change or interface variation need to modify, update or expand,
Being modified to global procedures, re-starting the work such as code building and cross compile repeatedly is needed, causes the general of model
Property and durability it is poor, development efficiency is low, and DD models and POP models can not individually manage with concurrent development debugging, limit DD
The autgmentability and flexibility of model and POP model associative simulations.
The content of the invention
In view of this, the application provides a kind of analogue system and method for Aerial Electronic Equipment, to solve prior art in emulation
When DD models and POP models close coupling relation limitation Simulation System Extension and the problem of flexibility, make the imitative of Aerial Electronic Equipment
True mode more generalization and multiplexingization, and program development efficiency can be improved by concurrent development.
To achieve these goals, the technical scheme that the embodiment of the present application is provided is as follows：
A kind of analogue system of Aerial Electronic Equipment, detailed design DD models and pilot operator rule for realizing Aerial Electronic Equipment
The associative simulation of model POP models, including：
Being predefined in DD models, POP models and the data Internet, the DD models has the first data-interface, the POP
Being predefined in model has the second data-interface, and the DD models pass through first data-interface and the data interaction network phase
Connection, the POP models are connected by second data-interface with the data interaction network, wherein：
The DD models receive the functional parameter of the Aerial Electronic Equipment of user's input, and being calculated according to the functional parameter is used for
Drive the POP models to carry out the logical data of interface display, and be published to logical data by first data-interface
In the data interaction network；
The POP models read logical data, and root by second data-interface from the data interaction network
Interface display is carried out according to the logical data of reading.
Preferably, the data interaction network is built in advance based on data distribution middleware, the data interaction net
The logical data memory block based on distribution subscription mechanism is provided with network, the data interaction network issues the DD models
Logical data is stored in the logical data memory block, the logical number of the POP models from the data interaction network
According to reading logical data in memory block.
Preferably, the data publication function based on Code automatic build technology, institute are provided with first data-interface
State and the data subscription function based on Code automatic build technology is provided with the second data-interface；
When logical data is published in the data interaction network by the DD models by first data-interface,
First data-interface extracts the Data Identification of the logical data of the DD models issue, and according to the data publication letter
The logical data is packaged into the logical data bag corresponding with the Data Identification by number, and the logical data bag is published to
In the data interaction network；
When the POP models read logical data by second data-interface from the data interaction network,
Second data-interface determines the Data Identification of the POP models logical data to be read, from the data interaction net
The logical data bag corresponding with the Data Identification of the POP models logical data to be read is extracted in network and according to described
Data subscription Function Solution is bundled into logical data.
The application also provides a kind of emulation mode of Aerial Electronic Equipment, applied in the analogue system of Aerial Electronic Equipment, realizes boat
The detailed design DD models of electric equipment and the associative simulation of pilot operator specification POP models, the analogue system include：DD moulds
Predefine to have in the first data-interface, the POP models in type, POP models and the data Internet, the DD models and predefine
There is the second data-interface, the DD models are connected by first data-interface with the data interaction network, the POP
Model is connected by second data-interface with the data interaction network；
The emulation mode includes：
Receive and store the logical data that the DD models are issued by first data-interface；The logical data is
What the functional parameter for the Aerial Electronic Equipment that the DD models are inputted according to user was calculated, for driving the POP models to carry out boundary
Face is shown；
Receive the logical data read requests that the POP models are sent by second data-interface, extract with it is described
The corresponding logical data of logical data read requests is simultaneously sent to the POP models by second data-interface, so that
The POP models carry out interface display according to the logical data of reading.
Preferably, the data interaction network is built in advance based on data distribution middleware, the data interaction net
The logical data memory block based on distribution subscription mechanism is provided with network；
Then,
It is described to receive and store the logical data that the DD models are issued by first data-interface, be specially：Connect
The logical data that the DD models are issued by first data-interface is received, and the logical data of reception is stored in described patrol
Collect in data storage area；
It is described to receive the logical data read requests that the POP models are sent by second data-interface, extract and
The corresponding logical data of the logical data read requests is simultaneously sent to the POP models by second data-interface,
So that the POP models carry out interface display according to the logical data of reading, it is specially：Receive the POP models pass through it is described
The logical data read requests that second data-interface is sent, extract from the logical data memory block and are read with the logical data
Take and ask corresponding logical data and the POP models are sent to by second data-interface, so that the POP models
Interface display is carried out according to the logical data of reading.
Preferably, the data publication function based on Code automatic build technology, institute are provided with first data-interface
State and the data subscription function based on Code automatic build technology is provided with the second data-interface；
Then,
It is described to receive and store the logical data that the DD models are issued by first data-interface, be specially：Connect
The logical data that the DD models are issued by first data-interface is received, and the DD is extracted in first data-interface
Model issue logical data Data Identification, according to the data publication function by the logical data be packaged into it is described
After the corresponding logical data bag of Data Identification, the logical data bag is stored；
It is described to receive the logical data read requests that the POP models are sent by second data-interface, extract and
The corresponding logical data of the logical data read requests is simultaneously sent to the POP models by second data-interface,
So that the POP models carry out interface display according to the logical data of reading, it is specially：Receive the POP models pass through it is described
The logical data read requests that second data-interface is sent, and determine that the POP models will be read in second data-interface
After the Data Identification of the logical data taken, the Data Identification for extracting the POP models logical data to be read is corresponding
Logical data bag, so that described in second data-interface is bundled into after logical data according to the data subscription Function Solution and is sent to
POP models.
The analogue system and emulation mode for the Aerial Electronic Equipment that above the application is provided, for realizing setting in detail for Aerial Electronic Equipment
The associative simulation of DD models and pilot operator specification POP models is counted, including：DD models, POP models and the data Internet,
Predefine to have to predefine in the first data-interface, the POP models in the DD models and have the second data-interface, the DD models
It is connected by first data-interface with the data interaction network, the POP models pass through second data-interface
It is connected with the data interaction network, wherein：The DD models receive the functional parameter of the Aerial Electronic Equipment of user's input, according to
The functional parameter is calculated for driving the POP models to carry out the logical data of interface display, and is counted by described first
Logical data is published in the data interaction network according to interface；The POP models are by second data-interface from institute
State and logical data is read in data interaction network, and interface display is carried out according to the logical data of reading.So, make DD models and
Logical data is published to data interaction by POP models by predefined data-interface and data interaction network connection, DD models
Network, POP models read logical data from data interaction network, and DD models and POP models are no longer directly docked, but are passed through
Data interaction real-time performance emulates the interaction of data so that DD models and POP models are no longer the entirety of close coupling, data-interface
Only need to change predefined data-interface program during change, the part not changed can be directly multiplexed, it is not necessary to be given birth to again
Into code and compiling, in the case where data-interface is constant, when DD models and POP models are modified, upgrade or replaced, no
Data interface routine and configuration information can be impacted, the versatility and durability of DD models and POP models can be strengthened, it is many
In the case of individual DD models and multiple POP models associative simulations, can also easily be carried out by data interaction network it is integrated and
Integrate, each model both faces towards data interaction network and debugged, and can strengthen the extension of DD models and POP model associative simulations
Property and flexibility, and DD models and POP models can individually manage with concurrent development debugging, program development can be effectively improved
Efficiency.
Brief description of the drawings
, below will be to embodiment or existing in order to illustrate more clearly of the embodiment of the present application or technical scheme of the prior art
There is the accompanying drawing used required in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments described in application, for those of ordinary skill in the art, on the premise of not paying creative work,
Other accompanying drawings can also be obtained according to these accompanying drawings.
The structural representation of the analogue system for the Aerial Electronic Equipment that Fig. 1 provides for the embodiment of the present application；
The flow chart of the emulation mode for the Aerial Electronic Equipment that Fig. 2 provides for the embodiment of the present application.
Embodiment
In order that those skilled in the art more fully understand the technical scheme in the application, it is right below in conjunction with accompanying drawing
The technical scheme of the application is clearly and completely described, it is clear that described embodiment is only the application part implementation
Example, rather than whole embodiments.Based on the embodiment in the application, those of ordinary skill in the art are not making creativeness
The every other embodiment obtained under the premise of work, should all belong to the scope of the application protection.
In order that those skilled in the art more fully understand application scheme, the application is made into one below in conjunction with the accompanying drawings
The detailed description of step：
The structural representation of the analogue system for the Aerial Electronic Equipment that Fig. 1 provides for the embodiment of the present application.
Shown in reference picture 1, the analogue system for the Aerial Electronic Equipment that the embodiment of the present application is provided, for realizing the detailed of Aerial Electronic Equipment
The associative simulation of thin design DD models and pilot operator specification POP models, including：
Being predefined in DD models 1, POP models 2 and the data Internet 3, the DD models 1 has the first data-interface 11,
Being predefined in the POP models 2 has the second data-interface 21, the DD models 1 by first data-interface 11 with it is described
Data interaction network 3 is connected, and the POP models 2 are connected by second data-interface 21 with the data interaction network 3
Connect, wherein：
The DD models 1 receive the functional parameter of the Aerial Electronic Equipment of user's input, and use is calculated according to the functional parameter
The logical data of interface display is carried out in the driving POP models 2, and is sent out logical data by first data-interface 11
Cloth is into the data interaction network 3；
The POP models 2 read logical data by second data-interface 21 from the data interaction network 3,
And interface display is carried out according to the logical data of reading.
In the embodiment of the present application, the data interaction network 3 is built in advance based on data distribution middleware, described
Logical data memory block 4 based on distribution subscription mechanism, the data interaction network 3 can also be set in data interaction network 3
The logical data that the DD models 1 are issued is stored in the logical data memory block 4, and the POP models 2 are from the data
Logical data is read in the logical data memory block 4 of the Internet 3.
In the embodiment of the present application, the first data-interface 11 and the second data-interface 21 are respectively in DD models 1 and POP moulds
Predefined in type 2, the core of the embodiment of the present application is to define a kind of general data interaction network 3, the He of DD models 1
POP models 2 are connected by predefined data-interface with data interaction network 3, without directly interacting, and support parallel
Exploitation and the debugging respective data process methods of DD and POP, then realize associative simulation by data interaction network 3.First number
Clear according to the definition of the data-interface 21 of interface 11 and second, extension and modification are convenient, can reduce the difficulty of program development, improve
Exploitation and debugging efficiency.
Further, the data publication based on Code automatic build technology can be provided with first data-interface 11
The data subscription function based on Code automatic build technology can be provided with function, second data-interface 21；
Logical data is published to by the data interaction network 3 by first data-interface 11 in the DD models 1
When middle, first data-interface 11 extracts the Data Identification for the logical data that the DD models 1 are issued, and according to the number
The logical data is packaged into the logical data bag corresponding with the Data Identification according to issue function, by the logical data
Bag is published in the data interaction network 3；
Logical data from the data interaction network 3 is read by second data-interface 21 in the POP models 2
When, second data-interface 21 determines the Data Identification of the logical data to be read of POP models 2, from the data
The logical data bag corresponding with the Data Identification of the logical data to be read of POP models 2 is extracted in the Internet 3 simultaneously
Logical data is bundled into according to the data subscription Function Solution.
In the embodiment of the present application, first have to developing DD models 1 and predefining in DD and POP the during POP models 2 respectively
One data-interface 11 and the second data-interface 21, then by real time workshop technology, defined in the first data-interface 11
Data publication function, the data subscription function defined in the second data-interface 21, and all logical data are in data interaction
Distinguished, be packaged into logical data according to Data Identification by unique Data Identification on network 3 by data publication function
The logical data bag of preset format, preset format is bundled into by data subscription function according to Data Identification by logical data bag solution
Logical data, you can the issue and subscription of the logical data at DD and POP two ends are realized by data interaction network 3.
For the technical scheme of clearer elaboration the embodiment of the present application, scheme is refined below by example
It is bright：
In this example, when developing DD models 1 and POP models 2, data interaction is built based on data distribution agreement middleware
Network 3, it is logical data memory block 4 to define data area, defines the data publication function and the second number of the first data-interface 11
According to the data subscription function of interface 21, the parameter of data publication function and data subscription function is the Data Identification of logical data
And data content, the packing and unpacking of preset format can be carried out to logical data according to Data Identification.
When setting up POP models 2, roll angle, the angle of pitch, course angle that POP models 2 are used to show aircraft, modeling are defined
Instrument uses VAPS XT；
When setting up DD models 1, the functional parameter that DD models 1 are used to receive the Aerial Electronic Equipment of user's input, emulation are defined
The function of inertial navigation computer, resolves the flight attitude of aircraft, obtains logical data, and logical data here is used to drive
Interface display in POP models 2, modeling tool uses Rhapsody；
By three logical datas of aspect it is that roll angle, the angle of pitch, course angle are resolved respectively in DD models 1
Afterwards, it is that each logical data specifies Data Identification, the Data Identification of each data is globally unique identifier；
Using Code automatic build technology, above three is issued into data interaction network 3 in the first data-interface 11 and is flown
Function is issued during the logical data of machine posture by API data to pack for logical data；
The logical data of the aspect of reception is saved in logical data memory block 4 by data interaction network 3；
POP models 2 are developed, display interface is built, determines the animation path of display data, and needing POP models 2 to carry out
During emulation, POP models 2 send logical data into logical data memory block 4 by the second data-interface 21 and extract request, should ask
The Data Identification for the logical data to be extracted is included in asking；
Second data-interface 21 extracts corresponding logical data bag according to the Data Identification from logical data memory block 4,
And Code automatic build technology is utilized, function is subscribed to by aircraft appearance of the logical data bag unpacking for preset format by API data
The logical data of state, POP models 2 are sent to by the logical data of unpacking, so that POP models 2 pass through three different data marks
Know to recognize Different Logic data, obtain three attitude angles, and associated with animation path foundation, so as to be carried out to three attitude angles
Interface display, so that program debugging personnel are according to interface display debugging model function, checks displaying whether correctly for logical data,
Whether the mode for linking up interface display with end user meets requirement.
It is understood that the technical scheme of the embodiment of the present application, imitative in multiple DD models 1 and multiple POP models 2 joint
In the case of genuine, it can also easily be carried out integrated and integrated by data interaction network 3, each model both faces towards data interaction
Network 3 is debugged, and can strengthen autgmentability and the flexibility of DD models 1 and the associative simulation of POP models 2,
Above the application provide Aerial Electronic Equipment analogue system, for realize Aerial Electronic Equipment detailed design DD models and
The associative simulation of pilot operator specification POP models, including：DD models, POP models and the data Internet, the DD models
In predefine to have to predefine in the first data-interface, the POP models and have the second data-interface, the DD models pass through described the
One data-interface is connected with the data interaction network, and the POP models pass through second data-interface and the data
The Internet is connected, wherein：The DD models receive the functional parameter of the Aerial Electronic Equipment of user's input, are joined according to the function
Number is calculated for driving the POP models to carry out the logical data of interface display, and will be patrolled by first data-interface
Data publication is collected into the data interaction network；The POP models are by second data-interface from the data interaction
Logical data is read in network, and interface display is carried out according to the logical data of reading.So, make DD models and POP models logical
Predefined data-interface and data interaction network connection are crossed, logical data is published to data interaction network, POP moulds by DD models
Type reads logical data from data interaction network, and DD models and POP models are no longer directly docked, but pass through data interaction net
Network realizes the interaction of emulation data so that DD models and POP models are no longer the entirety of close coupling, and data-interface is only needed when changing
Predefined data-interface program is changed, the part not changed can be directly multiplexed, it is not necessary to regenerate code and volume
Translate, in the case where data-interface is constant, when DD models and POP models are modified, upgrade or replaced, data will not be connect
Mouthful program and configuration information are impacted, and can strengthen the versatility and durability of DD models and POP models, multiple DD models and
In the case of multiple POP models associative simulations, it can also easily be carried out integrated and integrated, each mould by data interaction network
Type both faces towards data interaction network and debugged, and can strengthen autgmentability and the flexibility of DD models and POP model associative simulations,
And DD models and POP models can be managed individually to be debugged with concurrent development, can effectively improve program development efficiency.
The flow chart of the emulation mode for the Aerial Electronic Equipment that Fig. 2 provides for the embodiment of the present application.
Shown in reference picture 2, the emulation mode for the Aerial Electronic Equipment that the embodiment of the present application is provided, the emulation applied to Aerial Electronic Equipment
In system, the detailed design DD models of Aerial Electronic Equipment and the associative simulation of pilot operator specification POP models are realized, its feature exists
In the analogue system includes：Being predefined in DD models, POP models and the data Internet, the DD models has the first data
Being predefined in interface, the POP models has the second data-interface, and the DD models pass through first data-interface and the number
It is connected according to the Internet, the POP models are connected by second data-interface with the data interaction network；
The emulation mode includes：
Step S11：Receive and store the logical data that the DD models are issued by first data-interface；It is described to patrol
Collect the functional parameter that data are the Aerial Electronic Equipments that the DD models are inputted according to user to calculate, for driving the POP moulds
Type carries out interface display；
Step S12：The logical data read requests that the POP models are sent by second data-interface are received, are carried
Take the logical data corresponding with the logical data read requests and the POP moulds are sent to by second data-interface
Type, so that the POP models carry out interface display according to the logical data of reading.
In the embodiment of the present application, the data interaction network is built in advance based on data distribution middleware, described
The logical data memory block based on distribution subscription mechanism is provided with data interaction network；
Then, in step S11 the reception simultaneously stores the logic that the DD models are issued by first data-interface
Data, are specifically as follows：Receive the logical data that the DD models are issued by first data-interface, and patrolling reception
Data storage is collected in the logical data memory block；
The logical data that the reception POP models in step S12 are sent by second data-interface is read
Request, extracts the logical data corresponding with the logical data read requests and is sent to institute by second data-interface
POP models are stated, so that the POP models carry out interface display according to the logical data of reading, are specially：Receive the POP moulds
The logical data read requests that type is sent by second data-interface, from the logical data memory block extract with it is described
The corresponding logical data of logical data read requests is simultaneously sent to the POP models by second data-interface, so that
The POP models carry out interface display according to the logical data of reading.
In the embodiment of the present application, the data hair based on Code automatic build technology is provided with first data-interface
The data subscription function based on Code automatic build technology is provided with cloth function, second data-interface；
Then, in step S11 the reception simultaneously stores the logic that the DD models are issued by first data-interface
Data, be specially：The logical data that the DD models are issued by first data-interface is received, and in first data
Interface extracts the Data Identification of the logical data of DD models issue, according to the data publication function by the logical number
According to being packaged into after the logical data bag corresponding with the Data Identification, the logical data bag is stored.
The logical data that the reception POP models in step S12 are sent by second data-interface is read
Request, extracts the logical data corresponding with the logical data read requests and is sent to institute by second data-interface
POP models are stated, so that the POP models carry out interface display according to the logical data of reading, are specially：Receive the POP moulds
The logical data read requests that type is sent by second data-interface, and determine the POP in second data-interface
After the Data Identification of the model logical data to be read, the data mark of the POP models logical data to be read is extracted
Sensible corresponding logical data bag, so that second data-interface is bundled into after logical data according to the data subscription Function Solution
It is sent to the POP models.
The emulation mode for the Aerial Electronic Equipment that the embodiment of the present application is provided, the avionics that can apply in said system embodiment
The analogue system of equipment, therefore realization principle is consistent with above-described embodiment, here is omitted.
The analogue system and emulation mode for the Aerial Electronic Equipment that above the application is provided, for realizing setting in detail for Aerial Electronic Equipment
The associative simulation of DD models and pilot operator specification POP models is counted, including：DD models, POP models and the data Internet,
Predefine to have to predefine in the first data-interface, the POP models in the DD models and have the second data-interface, the DD models
It is connected by first data-interface with the data interaction network, the POP models pass through second data-interface
It is connected with the data interaction network, wherein：The DD models receive the functional parameter of the Aerial Electronic Equipment of user's input, according to
The functional parameter is calculated for driving the POP models to carry out the logical data of interface display, and is counted by described first
Logical data is published in the data interaction network according to interface；The POP models are by second data-interface from institute
State and logical data is read in data interaction network, and interface display is carried out according to the logical data of reading.So, make DD models and
Logical data is published to data interaction by POP models by predefined data-interface and data interaction network connection, DD models
Network, POP models read logical data from data interaction network, and DD models and POP models are no longer directly docked, but are passed through
Data interaction real-time performance emulates the interaction of data so that DD models and POP models are no longer the entirety of close coupling, data-interface
Only need to change predefined data-interface program during change, the part not changed can be directly multiplexed, it is not necessary to be given birth to again
Into code and compiling, in the case where data-interface is constant, when DD models and POP models are modified, upgrade or replaced, no
Data interface routine and configuration information can be impacted, the versatility and durability of DD models and POP models can be strengthened, it is many
In the case of individual DD models and multiple POP models associative simulations, can also easily be carried out by data interaction network it is integrated and
Integrate, each model both faces towards data interaction network and debugged, and can strengthen the extension of DD models and POP model associative simulations
Property and flexibility, and DD models and POP models can individually manage with concurrent development debugging, program development can be effectively improved
Efficiency.
For convenience of description, it is divided into various units during description apparatus above with function to describe respectively.Certainly, this is being implemented
The function of each unit can be realized in same or multiple softwares and/or hardware during application.
Each embodiment in this specification is described by the way of progressive, identical similar portion between each embodiment
Divide mutually referring to what each embodiment was stressed is the difference with other embodiment.Especially for device or
For system embodiment, because it is substantially similar to embodiment of the method, so describing fairly simple, related part is referring to method
The part explanation of embodiment.Apparatus and system embodiment described above is only schematical, wherein the conduct
The unit that separating component illustrates can be or may not be it is physically separate, the part shown as unit can be or
Person may not be physical location, you can with positioned at a place, or can also be distributed on multiple NEs.Can root
Some or all of module therein is factually selected to realize the purpose of this embodiment scheme the need for border.Ordinary skill
Personnel are without creative efforts, you can to understand and implement.
Professional further appreciates that, with reference to the unit of each example of the embodiments described herein description
And algorithm steps, can be realized with electronic hardware, computer software or the combination of the two, in order to clearly demonstrate hardware and
The interchangeability of software, generally describes the composition and step of each example according to function in the above description.These
Function is performed with hardware or software mode actually, depending on the application-specific and design constraint of technical scheme.Specialty
Technical staff can realize described function to each specific application using distinct methods, but this realization should not
Think beyond the scope of this invention.
Directly it can be held with reference to the step of the method or algorithm that the embodiments described herein is described with hardware, processor
Capable software module, or the two combination are implemented.Software module can be placed in random access memory (RAM), internal memory, read-only deposit
Reservoir (ROM), electrically programmable ROM, electrically erasable ROM, register, hard disk, moveable magnetic disc, CD-ROM or technology
In any other form of storage medium well known in field.
The foregoing description of the disclosed embodiments, enables professional and technical personnel in the field to realize or using the present invention.
A variety of modifications to these embodiments will be apparent for 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, it is of the invention
The embodiments shown herein is not intended to be limited to, and is to fit to and principles disclosed herein and features of novelty phase one
The most wide scope caused.
Claims (6)
1. a kind of analogue system of Aerial Electronic Equipment, detailed design DD models and pilot operator specification for realizing Aerial Electronic Equipment
The associative simulation of POP models, it is characterised in that including：
Being predefined in DD models, POP models and the data Internet, the DD models has the first data-interface, the POP models
In predefine have the second data-interface, the DD models are connected by first data-interface with the data interaction network
Connect, the POP models are connected by second data-interface with the data interaction network, wherein：
The DD models receive the functional parameter of the Aerial Electronic Equipment of user's input, are calculated according to the functional parameter for driving
The POP models carry out the logical data of interface display, and by first data-interface are published to logical data described
In data interaction network；
The POP models read logical data by second data-interface from the data interaction network, and according to reading
The logical data taken carries out interface display.
2. analogue system according to claim 1, it is characterised in that the data interaction network is based in data distribution
Between part build in advance, be provided with the logical data memory block based on distribution subscription mechanism in the data interaction network, it is described
The logical data that the DD models are issued is stored in the logical data memory block by data interaction network, the POP models
Logical data is read from the logical data memory block of the data interaction network.
3. analogue system according to claim 1, it is characterised in that be provided with first data-interface based on code
The data based on Code automatic build technology are provided with the data publication function of Auto, second data-interface
Subscribe to function；
It is described when logical data is published in the data interaction network by the DD models by first data-interface
First data-interface extracts the Data Identification of the logical data of the DD models issue, and will according to the data publication function
The logical data is packaged into the logical data bag corresponding with the Data Identification, the logical data bag is published to described
In data interaction network；
It is described when the POP models read logical data by second data-interface from the data interaction network
Second data-interface determines the Data Identification of the POP models logical data to be read, from the data interaction network
Extract the logical data bag corresponding with the Data Identification of the POP models logical data to be read and according to the data
Subscribe to Function Solution and be bundled into logical data.
4. a kind of emulation mode of Aerial Electronic Equipment, applied in the analogue system of Aerial Electronic Equipment, realizing setting in detail for Aerial Electronic Equipment
Count the associative simulation of DD models and pilot operator specification POP models, it is characterised in that the analogue system includes：DD models,
Predefining to have to predefine in the first data-interface, the POP models in POP models and the data Internet, the DD models has
Second data-interface, the DD models are connected by first data-interface with the data interaction network, the POP moulds
Type is connected by second data-interface with the data interaction network；
The emulation mode includes：
Receive and store the logical data that the DD models are issued by first data-interface；The logical data is described
What the functional parameter for the Aerial Electronic Equipment that DD models are inputted according to user was calculated, show for driving the POP models to carry out interface
Show；
The logical data read requests that the POP models are sent by second data-interface are received, are extracted and the logic
The corresponding logical data of data read request is simultaneously sent to the POP models by second data-interface, so that described
POP models carry out interface display according to the logical data of reading.
5. emulation mode according to claim 4, it is characterised in that the data interaction network is based in data distribution
Between part build in advance, be provided with the logical data memory block based on distribution subscription mechanism in the data interaction network；
Then,
It is described to receive and store the logical data that the DD models are issued by first data-interface, be specially：Receive institute
The logical data that DD models are issued by first data-interface is stated, and the logical data of reception is stored in the logical number
According in memory block；
It is described to receive the logical data read requests that the POP models are sent by second data-interface, extraction with it is described
The corresponding logical data of logical data read requests is simultaneously sent to the POP models by second data-interface, so that
The POP models carry out interface display according to the logical data of reading, are specially：The POP models are received by described second
The logical data read requests that data-interface is sent, extract to read with the logical data from the logical data memory block and ask
Seek corresponding logical data and the POP models be sent to by second data-interface so that the POP models according to
The logical data of reading carries out interface display.
6. emulation mode according to claim 4, it is characterised in that be provided with first data-interface based on code
The data based on Code automatic build technology are provided with the data publication function of Auto, second data-interface
Subscribe to function；
Then,
It is described to receive and store the logical data that the DD models are issued by first data-interface, be specially：Receive institute
The logical data that DD models are issued by first data-interface is stated, and the DD models are extracted in first data-interface
The logical data, is packaged into and the data by the Data Identification for the logical data issued according to the data publication function
After the corresponding logical data bag of mark, the logical data bag is stored；
It is described to receive the logical data read requests that the POP models are sent by second data-interface, extraction with it is described
The corresponding logical data of logical data read requests is simultaneously sent to the POP models by second data-interface, so that
The POP models carry out interface display according to the logical data of reading, are specially：The POP models are received by described second
The logical data read requests that data-interface is sent, and determine what the POP models to be read in second data-interface
After the Data Identification of logical data, the corresponding logic of the Data Identification of the POP models logical data to be read is extracted
Packet, so that second data-interface is bundled into after logical data according to the data subscription Function Solution is sent to the POP
Model.
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| CN104636188B (en) * | 2015-02-25 | 2017-10-24 | 北京润科通用技术有限公司 | A kind of emulation mode and system |
| CN104915245B (en) * | 2015-07-01 | 2017-12-12 | 四川航天系统工程研究所 | Realize analogue system and the integrated system and method for the operation of actual functional capability systematic unity |
| CN106452918B (en) * | 2016-11-23 | 2019-04-26 | 北京润科通用技术有限公司 | A kind of communication means and system of avionics network system |
| CN107563075B (en) * | 2017-09-08 | 2020-09-18 | 中国航空工业集团公司沈阳飞机设计研究所 | Method for realizing CosiMate network and DDS network interconnection |
| CN109656147A (en) * | 2018-11-23 | 2019-04-19 | 中国航空工业集团公司沈阳飞机设计研究所 | Air-combat simulation system |
| CN109739767A (en) * | 2018-12-29 | 2019-05-10 | 北京润科通用技术有限公司 | A kind of human-computer interaction interface logic function test method and device |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101763443A (en) * | 2008-12-23 | 2010-06-30 | 江西洪都航空工业集团有限责任公司 | Avionics system digitalized design verification system and method |
| CN102609248A (en) * | 2011-12-28 | 2012-07-25 | 方伟 | Integrated avionics system modeling and simulation platform based on MDA (model driven architecture) |
Family Cites Families (1)
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-
2014
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Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101763443A (en) * | 2008-12-23 | 2010-06-30 | 江西洪都航空工业集团有限责任公司 | Avionics system digitalized design verification system and method |
| CN102609248A (en) * | 2011-12-28 | 2012-07-25 | 方伟 | Integrated avionics system modeling and simulation platform based on MDA (model driven architecture) |
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