CN102289208A - Simulation test system for ARINC (Aeronautical Radio Incorporated) 429 data bus - Google Patents
Simulation test system for ARINC (Aeronautical Radio Incorporated) 429 data bus Download PDFInfo
- Publication number
- CN102289208A CN102289208A CN2011101119743A CN201110111974A CN102289208A CN 102289208 A CN102289208 A CN 102289208A CN 2011101119743 A CN2011101119743 A CN 2011101119743A CN 201110111974 A CN201110111974 A CN 201110111974A CN 102289208 A CN102289208 A CN 102289208A
- Authority
- CN
- China
- Prior art keywords
- data
- definition
- button
- port com
- transmission
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Abstract
The invention discloses a simulation test system for an ARINC (Aeronautical Radio Incorporated) 429 data bus, which belongs to the technical field of simulation test. The simulation test system is characterized in that a simulation controller [1], a data transmission and control bus [2], an ARINC429 communication interface [3] and an ARINC429 interface adapter [4] form an ARINC429 data bus simulation and test environment; the simulation controller [1] is used for controlling the ARINC429 communication interface [3] to transmit and receive data information through the data transmission and control bus [2], simulate the generating and transmitting process of an airborne flight control system, an aircraft electronic system and other airborne equipment information streams, receive and display the other airborne equipment information streams. The simulation test system has the advantages of complete system functions, reasonable layout, compact structure, reliability in work, convenience in use and favorable expansibility and cutting property.
Description
Affiliated technical field
The present invention relates to a kind of ARINC429 data bus emulation test system, particularly relate to the generation, transmission, processing, the procedure for displaying that are used to simulate airborne equipment information flows such as avionics system, flight-control computer, belong to the l-G simulation test technical field of measurement and test.
Background technology
Flight control system, airborne equipments such as avionics system are more and more important in the present generation aircraft design process, along with the fax flight control technology, the application of the active control technology and the information processing technology, flight control system, avionics system has reached overall with aircraft, pneumatic, the stage of structure and intensity Synchronization Design, simultaneously, flight control system, the security of avionics system and reliability are more important for the safety of aircraft, in order to guarantee flight control system, the security of avionics system and reliability, on the basis of design, another important channel is carried out ground simulation test exactly, in ground simulation test how to flight control system, avionics system carries out comprehensively, detailed checking becomes flight control system, the difficult problem that the avionics system ground experiment faces.In traditional demonstration test, need development to be specifically designed to the environment backup facility of test, required environmental baseline when as far as possible can the simulated flight control system working aboard: as design each building block that special test-bed is used to support and install flight control system, and for the work of each building block provides necessary hydraulic energy source and power supply, configuration necessary control and testing apparatus.
In the demonstration test of flight control system, avionics system, most of checking project is relevant with the transmission of the information flow of airborne equipment, in the checking of test, the mobile system that needs use to install is finished operation control and the state adjustment to flight control system, avionics system.Adopt installation equipment to have following shortcoming:
(1) installation equipment is after Design of Flight Control is finished, and could produce provides, and can not satisfy the needs of test of design development or sample preparation part step-by-step test just;
(2) installation equipment is to special flight control system development and production, does not have versatility, after flight control system, other unit status of avionics system change, need carry out the suitability change, or even process again, produces.
(3) installation equipment relies on manually-operated to finish, and the validation test process efficiency is low, and the cycle is long;
(4) air environment is of a great variety, avionics system is all very complicated big system of a 26S Proteasome Structure and Function, with the real system investment greatly, suitable risk is arranged again, and emulation technology can exchange the reduction significantly on the risk with less investment for, obtains very high efficiency-cost ratio;
(5) research of real system is not only time-consuming expensive, the cost height, have a big risk, the cycle is long, and is difficult to accomplish, then can abbreviate with computer simulation technique, use manpower and material resources sparingly greatly.
At present, be a certain stage mostly to flight control system, the simulation study of avionics system data information transfer both at home and abroad at flight control system, avionics system structured data flow transmission or processing, only in a certain respect mutual at system information, to the performance of flight control system, avionics system carry out system, comprehensively evaluation analysis has certain limitation.
In the development and design of aircraft, adopt digital simulation technique in large quantities, Digital Simulation has been proved to be to develop the aircraft efficient ways, and it provides faster, has developed the advantage of aircraft more efficiently.In order to guarantee the cycle of aircraft development, accelerate flight control system, avionics system test progress, be necessary in the test of flight control system, avionics system, to adopt more digital simulation technique; On the other hand, flight control system, avionics system checking project are many, and a large amount of tests need, and the design phase finishes in the early stage, so just need a test platform, satisfy while designing the workflow of test, so that make flight control system, avionics system reach more high maturity to the ground experiment stage.For carry out test earlier as far as possible, this also requires to use digital simulation technique progressively to replace a large amount of actual loading test technology that depend on as the digitizing experimental technique of core, shortens the aircraft development cycle, accelerates Development Schedule.
Summary of the invention
The object of the present invention is to provide a kind of ARINC 429 data bus simulation detection system and emulation modes thereof, the generation and the transmission course of airborne equipment information flows such as simulated flight control system, avionics system have been reacted mutual cooperation and information interaction between each subsystem.
Technical scheme of the present invention is: a kind of ARINC 429 data bus simulation detection systems, comprise emulation controller, data transmission and control bus, ARINC 429 communication interfaces, ARINC 429 interface adapters, realize the transmission and the reception of data message by data transmission and control bus control ARINC 429 communication interfaces by emulation controller, simulate airborne flight control system, the generation and the process of transmitting of airborne equipment information flows such as avionics system, and receive other airborne equipment information flow and show, data transmission and control bus are configured in the cabinet of test emulation controller, realize the data information transmission and the exchange of emulation controller and ARINC 429 communication interfaces, and clock, trigger, the transmission of control signal such as synchronously, ARINC 429 communication interfaces will send to the ARINC429 data bus from the data message of emulation controller, or from ARINC 429 data bus receiving data informations and be transferred to emulation controller, ARINC 429 interface adapters are finished the physical connection of ARINC 429 communication interfaces and ARINC 429 data buss, guarantee the unimpeded of data information transfer passage.
The generation of airborne equipment information flows such as simulated flight control system of the present invention, avionics system sends, receives transmission course, and finish the preservation of receiving data information, these functions are to realize by the application software that operates in emulation controller, application software adopts the modular construction of layering, is made up of operation interface layer, user application layer, Communication Control layer and layers of physical devices.
Realized man-machine interface operation control function at the operation interface layer, select the user application layer operation by menu-drive, finish the transmission and the reception of data message, and the work of simulation airborne equipment, the transmission or the reception of data message finished by PORT COM;
Or select the Communication Control layer operation, finish ARINC 429 interface managements and parameter configuration;
Or select the layers of physical devices operation, finish ARINC 429 interface controls, self check, diagnosis etc.
User application layer has been realized variety of way data information transmission and receiving function, and the transmission and the receiving function of the information flow of simulation airborne equipment, data information transmission and receiving function aspect have realized data format definition editting function, Data Receiving memory function, have received data-driven tabulation Presentation Function, have received the graphical display function of data-driven, simple data sending function, function type data sending function, discrete data sending function;
The data definition editting function has realized definition increase, deletion, modification to data etc., editor, the modification that data are defined is provided to the user, and the edit-modify result preserved with document form, form communication interface control document, for to the parsing of data, filter in use;
The Data Receiving memory function has realized the selection PORT COM, has selected communication speed, has selected data definition and identity code, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information at reception data buffer, finish once receiving operation;
Receiving data-driven tabulation Presentation Function has realized the selection PORT COM, has selected communication speed, has selected data definition and identity code, after beginning to receive data, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, receiving data rows list area demonstration filtered data information, finish continuous Data Receiving operation, up to stopping the Data Receiving operation;
The graphical display function that receives data-driven has realized the selection PORT COM, has selected communication speed, has selected data definition and identity code, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information with the graph curve form, finish continuous Data Receiving operation, up to stopping the Data Receiving operation;
Function type data sending function has been realized the selection PORT COM, has selected communication speed, has been selected transmission turnover rate, selection data definition and identity code, selection to send the data definition function, when being in transmit status, according to selected function calculation functional value, and with the combination of the data definition identity code of current selection, form ARINC 429 formatted datas, send data message from current selected PORT COM, according to selecting to send the cycle that the turnover rate specified data sends, up to stopping the data transmit operation;
The discrete data sending function has been realized the selection PORT COM, has selected communication speed, has been selected transmission turnover rate, selection data definition and identity code, selection to send the data definition file, when being in transmit status, according to selected data file, reading numerical values, and with the combination of the data definition identity code of current selection, form ARINC 429 formatted datas, send data message from current selected PORT COM, according to selecting to send the cycle that the turnover rate specified data sends, up to stopping the data transmit operation.
The Communication Control layer has been realized ARINC 429 data message sending functions, ARINC 429 data message receiving functions and ARINC 429 interface managements and parameter configuration function.
Layers of physical devices is finished the physical connection of ARINC 429 communication control interfaces and ARINC 429 data buss, realizes ARINC 429 communications and data information transfer function.
The present invention has the following advantages:
(1) the present invention is a kind of ARINC429 data bus emulation test system, has simulated the production process and the receiving course of airborne information flow, the correctness of data information transfer is verified telotism.
(2) compactness rational in infrastructure, reliable operation adopt high reliability communication interface and emulator controller, through optimal design, modularization, standardization and seriation, can adapt at harsh electromagnetism and mechanical environment and use.
(3) good extendability, cutting out property and reusability, each emulator and communication interface adopt the design of assembly mould blocking, and the component software technology based on framework is adopted in software development, and the optional component module realizes the unitization combination of system as required.
(4) reduce cost,, on function, be equivalent to the function of original a plurality of specialized equipments, greatly reduce equipment cost owing to realized General design.
(4) concerning the user, because on-board data Transmission System Simulation device has improved experimental test efficient greatly, shortened the test period, significantly reduced expense.
Along with the development in technology and market, ARINC429 data bus simulation detection system certainly will become most economical, the most practical emulation test system.
Below in conjunction with drawings and Examples the present invention is described in detail.
Description of drawings
Fig. 1 is a kind of ARINC429 data bus emulation test system structural representation of the present invention.
Fig. 2 is the composition structural drawing of one embodiment of the present of invention.
Fig. 3 is that application software component module of the present invention is formed structural drawing.
Fig. 4 is a data definition editing operation of the present invention interface synoptic diagram.
Fig. 5 is a Data Receiving operation interface synoptic diagram of the present invention.
Fig. 6 is that data sequence of the present invention receives the operation interface synoptic diagram.
Fig. 7 is a data transmit operation of the present invention interface synoptic diagram.
Fig. 8 is a discrete and function type data transmit operation interface synoptic diagram of the present invention.
Embodiment
The structural representation of a kind of ARINC429 data bus emulation test system as shown in Figure 1, comprise emulation controller [1], data transmission and control bus [2], ARINC 429 communication interfaces [3], ARINC 429 interface adapters [4], realize the transmission and the reception of data message by data transmission and control bus [2] control ARINC 429 communication interfaces [3] by emulation controller [1], simulate airborne flight control system, the generation and the process of transmitting of airborne equipment information flows such as avionics system, and receive other airborne equipment information flow and show, data transmission and control bus [2] are configured in the cabinet of test emulation controller, realize the data information transmission and the exchange of emulation controller [1] and ARINC 429 communication interfaces [3], and clock, trigger, the transmission of control signal such as synchronously, ARINC 429 communication interfaces [3] will send to ARINC 429 data buss from the data message of emulation controller, or from ARINC 429 data bus receiving data informations and be transferred to emulation controller [1], ARINC 429 interface adapters [4] are finished the physical connection of ARINC 429 communication interfaces [3] and ARINC 429 data buss, guarantee the unimpeded of data information transfer passage.
Fig. 2 is the composition structural drawing of one embodiment of the present of invention.
Among a kind of ARINC429 data bus emulation test system embodiment, emulation controller [1] adopts the PXI bus system, configuration has the PXI-1045 of the NI company cabinet of 18 slots, and apolegamy PXI-8102 embedded controller, data transmission and control bus [2] adopt cpci bus, ARINC 429 communication interfaces [3] adopt the GE BAR-CPCI-1608 of company communication interface card, this interface card provides 8 transmit ports and 8 receiving ports, the data of finishing multiport send and receive, the adapter that ARINC 429 interface adapters [4] are selected and the BAR-CPCI-1608 communication interface card matches.
Above-mentioned feature of the present invention can be done following variation, but they all do not depart from essence of the present invention.
In full reportedly defeated and control bus place selects can also select CPCI, PCI, VXI test bus or computer bus etc. outside the PXI test bus;
Emulation controller [1] adopts outside the NI PXI-1045 of the company cabinet, can also select other model cabinet, as PXI-1036, PXI-1044, or other company such as Ling Hua cPCIS-1100A, cPCIS-1202, PXIS-2503, PXIS-2630, PXIS-2700, PXIS-2719 etc., or the test of other model of other company control cabinet;
Outside the embedded controller apolegamy PXI-8102, can also match NI PXI-8145RT, NI PXI-8184RT, NI PXI-8196RT, the NI PXI-8195RT of NI company, or the PXI-3910 of Ling Hua company, PXI-3920, PXI-3950, or the embedded controller of other model of other company;
ARINC 429 communication interface cards can also be selected the communication interface card of other model of other company except that adopting the BAR-CPCI-1608 communication interface card.
Fig. 3 is that application software component module of the present invention is formed structural drawing.
Application software of the present invention adopts the modular construction of layering, formed by operation interface layer, user application layer, Communication Control layer and layers of physical devices, the man-machine interface operation Control Component module [301] of operation interface layer has realized man-machine interface operation control function, selection user application layer operation by menu-drive, finish the transmission and the reception of data message, and the work of simulation airborne equipment, finish the transmission or the reception of data message by PORT COM; Or select the Communication Control layer operation, finish ARINC429 interface management and parameter configuration; Or select the layers of physical devices operation, finish ARINC 429 interface controls, self check, diagnosis etc.
User application layer has been realized variety of way data information transmission and receiving function, and the transmission and the receiving function of information flow of simulation airborne equipment, by data format definition editing component module [302], Data Receiving memory module module [303], receive data-driven tabulation display module module [304], the graphic presentation assembly module [305], function type data sending assembly module [306], the discrete data sending assembly module [307] that receive data-driven realized data information transmission and receiving function;
Data definition editing component module [302] has realized definition increase, deletion, modification to data etc., editor, the modification that data are defined is provided for the user, and the edit-modify result preserved with document form, form communication interface control document for to the parsing of data, filter in use;
Data Receiving memory module module [303] has realized the selection PORT COM, has selected communication speed, has selected data definition and identity code, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information at reception data buffer, finish once receiving operation;
Receiving data-driven tabulation display module module [304] has realized the selection PORT COM, has selected communication speed, has selected data definition and identity code, after beginning to receive data, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, receiving data rows list area demonstration filtered data information, finish continuous Data Receiving operation, up to stopping the Data Receiving operation;
The graphic presentation assembly module [305] that receives data-driven has been realized the selection PORT COM, has selected communication speed, has been selected data definition and identity code, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information with the graph curve form, finish continuous Data Receiving operation, up to stopping the Data Receiving operation;
Function type data sending assembly module [306] has realized the selection PORT COM, has selected communication speed, has selected transmission turnover rate, selection data definition and identity code, selection to send the data definition function, when being in transmit status, according to selected function calculation functional value, and with the combination of the data definition identity code of current selection, form ARINC 429 formatted datas, send data message from current selected PORT COM, according to selecting to send the cycle that the turnover rate specified data sends, up to stopping the data transmit operation;
Discrete data sending assembly module [307] has realized the selection PORT COM, has selected communication speed, has selected transmission turnover rate, selection data definition and identity code, selection to send the data definition file, when being in transmit status, according to selected data file, reading numerical values, and with the combination of the data definition identity code of current selection, form ARINC 429 formatted datas, send data message from current selected PORT COM, according to selecting to send the cycle that the turnover rate specified data sends, up to stopping the data transmit operation.
The Communication Control layer comprises ARINC 429 data message sending assembly modules [308], ARINC 429 data message receiving unit modules [309] and ARINC 429 interface managements and parameter configuration assembly module [310].
Layers of physical devices comprises ARINC 429 Communication Control assembly modules [311], realizes and the physical connection of ARINC 429 data buss, realizes ARINC 429 communications and data information transfer.
Fig. 4 is a data definition editing operation of the present invention interface synoptic diagram.
Definition increase, deletion, modification to data etc. realized at data definition editing operation interface, editor, the modification that data are defined is provided for the user, and the edit-modify result preserved with document form, form communication interface control document for using to the parsing of data, in filtering, the definition of the data of institute's edit-modify is corresponding one by one with the signal that is transmitted formation.
Data definition editing operation interface comprises editor's panel [401], editor's panel [401] is provided with each the section editor to data, the function of modification, and these data segments comprise the unit [407] of the abbreviation [405] of the identity code [403] of sequence number [402], transmission data or the respective signal of transmitting data or respective signal definition, the title [404] of transmitting data or respective signal, transmission data or respective signal, engineer's scale/definition [406] of transmitting data or respective signal, transmission data or respective signal;
On data definition editing operation interface editing panel [401], also be provided with the feature operation virtual push button, it is respectively " increase " button [408], " deletion " button [409], the Edit button [410], " affirmation " button [411], " cancellation " button [412], use " increase " button [408] to increase the definition of transmission data or respective signal form, use the definition of " deletion " button [409] deletion transmission data or respective signal form, use the Edit button [410] editor, revise the definition of transmission data or respective signal form, finish increase to the definition of transmission data or respective signal form, deletion, after editor waits operation, use " affirmation " button to preserve current result, and return upper level and operate, if abandon current operation, then use " cancellation " button to return the upper level operation interface.
Fig. 5 is a Data Receiving operation interface synoptic diagram of the present invention.
The Data Receiving operation interface has the PORT COM of selection, selects communication speed, selects data definition and identity code function, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information at reception data buffer, finish once receiving operation.
The Data Receiving operation interface comprises guidance panel [501], guidance panel [501] is provided with PORT COM selective listing frame [502], communication speed selective listing frame [503], data definition and identity code selective listing frame [504], Data Receiving buffer zone display window [505], on Data Receiving operation interface guidance panel [501], also be provided with the feature operation virtual push button, it is respectively " reception " button [506], " stop " button [507], the Back button [508], use " reception " button, PORT COM receiving data information from current appointment, and show at Data Receiving buffer zone display window [505], use " stopping " button, stop PORT COM receiving data information from current appointment, use the Back button, just turn back to the upper level operation interface.
Fig. 6 is that data sequence of the present invention receives the operation interface synoptic diagram.
Data sequence receives operation interface to be had the PORT COM of selection, selection communication speed, selects data definition and identity code function, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, filtered data information is write storing data files, finish receiving operation.
Data sequence receives operation interface and comprises guidance panel [601], guidance panel [601] is provided with PORT COM selective listing frame [602], communication speed selective listing frame [603], data definition and identity code selective listing frame [604], data storage file name window [605], receive datagraphic curve display window [606], receive data list display window [607], on data sequence reception operation interface guidance panel [601], also be provided with the feature operation virtual push button, it is respectively " reception " button [608], " stop " button [609], the Back button [610], use " reception " button, PORT COM receiving data information from current appointment, filter receiving data, show at reception datagraphic curve display window [606] and reception data list display window [607], and be written in the defined file of data storage file name window [605], use " stopping " button, stop PORT COM receiving data information from current appointment, use the Back button, just turn back to the upper level operation interface.
Fig. 7 is a data transmit operation of the present invention interface synoptic diagram.
Data transmit operation interface has the PORT COM of selection, selects communication speed, selects data definition and identity code function, when being in transmit status, the data of data buffer and the data definition identity code combination of current selection will be sent, be assembled into the data layout that is fit to ARINC-429 communication transmission, send data from selected PORT COM, finish a transmit operation.
Data transmit operation interface comprises guidance panel [701], guidance panel [701] is provided with PORT COM selective listing frame [702], communication speed selective listing frame [703], data definition and identity code selective listing frame [704], data send buffer zone display window [705], on data transmit operation interface operation panel [701], also be provided with the feature operation virtual push button, it is respectively " transmission " button [706], " stop " button [707], the Back button [708], use " transmission " button, data are sent the PORT COM transmission of buffer zone display window data from current appointment, use " stopping " button, stop to send data message from the PORT COM of current appointment, use the Back button, just turn back to the upper level operation interface.
Fig. 8 is a discrete and function type data transmit operation interface synoptic diagram of the present invention.
Discrete and function type data transmit operation interface has the selection PORT COM, select communication speed, select to send turnover rate, select data definition and identity code, select the discrete data file, select the data definition function performance, when being in transmit status, from discrete data file reading of data, perhaps produce data according to the defined function of data definition function, data definition identity code combination with current selection, be assembled into the data layout that is fit to ARINC-429 communication transmission, send data from selected PORT COM, data transmitting period is upgraded according to sending turnover rate, up to finishing transmit operation or having stopped the data transmit operation.
Discrete and function type data transmit operation interface comprises guidance panel [801], guidance panel [801] is provided with PORT COM selective listing frame [802], communication speed selective listing frame [803], send turnover rate definition list box [804], data definition and identity code selective listing frame [805], send discrete data file display window [806], data definition function selective listing frame [807], on discrete and function type data transmit operation interface operation panel [801], also be provided with the feature operation virtual push button, it is respectively " transmission " button [809], " stop " button [810], the Back button [811], use " transmission " button, from sending the discrete data file reading of data of discrete data file display window [806] appointment, perhaps produce data according to the defined function of data definition function selective listing frame [807], the data definition identity code of selecting with data definition and identity code selective listing frame [805] makes up, send from the PORT COM of current appointment, use " stopping " button, stop to send data message from the PORT COM of current appointment, use the Back button, just turn back to the upper level operation interface.
Claims (9)
1. ARINC429 data bus emulation test system, it is characterized in that, this emulation test system comprises emulation controller [1], data transmission and control bus [2], ARINC 429 communication interfaces [3], ARINC 429 interface adapters [4], realize the transmission and the reception of data message by data transmission and control bus [2] control ARINC 429 communication interfaces [3] by emulation controller [1], simulate airborne flight control system, the generation and the process of transmitting of airborne equipment information flows such as avionics system, and receive other airborne equipment information flow and show, data transmission and control bus [2] are configured in the cabinet of test emulation controller, realize the data information transmission and the exchange of emulation controller [1] and ARINC429 communication interface [3], and clock, trigger, the transmission of control signal such as synchronously, ARINC 429 communication interfaces [3] will send to ARINC 429 data buss from the data message of emulation controller, or from ARINC 429 data bus receiving data informations and be transferred to emulation controller [1], ARINC 429 interface adapters [4] are finished the physical connection of ARINC 429 communication interfaces [3] and ARINC 429 data buss, guarantee the unimpeded of data information transfer passage.
2. a kind of ARINC429 data bus emulation test system according to claim 1, it is characterized in that emulation controller [1] adopts the PXI bus system, configuration has the PXI-1045 cabinet of 18 slots, and apolegamy PXI-8102 embedded controller, data transmission and control bus [2] adopt cpci bus, ARINC 429 communication interfaces [3] adopt the BAR-CPCI-1608 communication interface card, this interface card provides 8 transmit ports and 8 receiving ports, the data of finishing multiport send and receive, the adapter that ARINC 429 interface adapters [4] are selected and the BAR-CPCI-1608 communication interface card matches.
3. a kind of ARINC429 data bus emulation test system according to claim 1, it is characterized in that application software adopts the modular construction of layering, formed by operation interface layer, user application layer, Communication Control layer and layers of physical devices, the man-machine interface operation Control Component module [301] of operation interface layer has realized man-machine interface operation control function, select the user application layer operation by menu-drive, finish the transmission and the reception of data message, and the work of simulation airborne equipment, finish the transmission or the reception of data message by PORT COM;
Or, finish ARINC 429 interface managements and parameter configuration by menu-drive selection Communication Control layer operation;
Or, finish ARINC 429 interface controls, self check, diagnosis etc. by the operation of menu-drive selection layers of physical devices.
4. according to claim 1 or the described a kind of ARINC429 data bus emulation test system of claim 3, it is characterized in that user application layer realized variety of way data information transmission and receiving function, and the transmission and the receiving function of the information flow of simulation airborne equipment, by data format definition editing component module [302], Data Receiving memory module module [303], receive data-driven tabulation display module module [304], receive the graphic presentation assembly module [305] of data-driven, function type data sending assembly module [306], discrete data sending assembly module [307] has realized data information transmission and receiving function;
Data definition editing component module [302] has realized definition increase, deletion, modification to data etc., editor, the modification that data are defined is provided for the user, and the edit-modify result preserved with document form, form communication interface control document for to the parsing of data, filter in use;
Data Receiving memory module module [303] has realized the selection PORT COM, has selected communication speed, has selected data definition and identity code, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information at reception data buffer, finish once receiving operation;
Receiving data-driven tabulation display module module [304] has realized the selection PORT COM, has selected communication speed, has selected data definition and identity code, after beginning to receive data, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, receiving data rows list area demonstration filtered data information, finish continuous Data Receiving operation, up to stopping the Data Receiving operation;
The graphic presentation assembly module [305] that receives data-driven has been realized the selection PORT COM, has selected communication speed, has been selected data definition and identity code, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information with the graph curve form, finish continuous Data Receiving operation, up to stopping the Data Receiving operation;
Function type data sending assembly module [306] has realized the selection PORT COM, has selected communication speed, has selected transmission turnover rate, selection data definition and identity code, selection to send the data definition function, when being in transmit status, according to selected function calculation functional value, and with the combination of the data definition identity code of current selection, form ARINC 429 formatted datas, send data message from current selected PORT COM, according to selecting to send the cycle that the turnover rate specified data sends, up to stopping the data transmit operation;
Discrete data sending assembly module [307] has realized the selection PORT COM, has selected communication speed, has selected transmission turnover rate, selection data definition and identity code, selection to send the data definition file, when being in transmit status, according to selected data file, reading numerical values, and with the combination of the data definition identity code of current selection, form ARINC 429 formatted datas, send data message from current selected PORT COM, according to selecting to send the cycle that the turnover rate specified data sends, up to stopping the data transmit operation.
5. a kind of ARINC429 data bus emulation test system according to claim 1, it is characterized in that data definition editing operation interface realized definition increase, deletion, modification to data etc., editor, the modification that data are defined is provided for the user, and the edit-modify result preserved with document form, form communication interface control document for using the data definition of institute's edit-modify and the signal that is transmitted formation one-to-one relationship to the parsing of data, in filtering;
Data definition editing operation interface comprises editor's panel [401], editor's panel [401] is provided with each the section editor to data, the function of modification, and these data segments comprise the unit [407] of the abbreviation [405] of the identity code [403] of sequence number [402], transmission data or the respective signal of transmitting data or respective signal definition, the title [404] of transmitting data or respective signal, transmission data or respective signal, engineer's scale/definition [406] of transmitting data or respective signal, transmission data or respective signal;
On data definition editing operation interface editing panel [401], also be provided with the feature operation virtual push button, it is respectively " increase " button [408], " deletion " button [409], the Edit button [410], " affirmation " button [411], " cancellation " button [412], use " increase " button [408] to increase the definition of transmission data or respective signal form, use the definition of " deletion " button [409] deletion transmission data or respective signal form, use the Edit button [410] editor, revise the definition of transmission data or respective signal form, finish increase to the definition of transmission data or respective signal form, deletion, after editor waits operation, use " affirmation " button to preserve current result, and return upper level and operate, if abandon current operation, then use " cancellation " button to return the upper level operation interface.
6. a kind of ARINC429 data bus emulation test system according to claim 1, it is characterized in that the Data Receiving operation interface has the PORT COM of selection, selects communication speed, selects data definition and identity code function, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, show filtered data information, finish once receiving operation at reception data buffer;
The Data Receiving operation interface comprises guidance panel [501], guidance panel [501] is provided with PORT COM selective listing frame [502], communication speed selective listing frame [503], data definition and identity code selective listing frame [504], Data Receiving buffer zone display window [505], on Data Receiving operation interface guidance panel [501], also be provided with the feature operation virtual push button, it is respectively " reception " button [506], " stop " button [507], the Back button [508], use " reception " button, PORT COM receiving data information from current appointment, and show at Data Receiving buffer zone display window [505], use " stopping " button, stop PORT COM receiving data information from current appointment, use the Back button, just turn back to the upper level operation interface.
7. a kind of ARINC429 data bus emulation test system according to claim 1, it is characterized in that data sequence receives operation interface and has the PORT COM of selection, selection communication speed, selects data definition and identity code function, when being in accepting state, from current selected PORT COM receiving data information, and with the data definition identity code of current selection relatively, carry out the filtration of data message, filtered data information is write storing data files, finish receiving operation;
Data sequence receives operation interface and comprises guidance panel [601], guidance panel [601] is provided with PORT COM selective listing frame [602], communication speed selective listing frame [603], data definition and identity code selective listing frame [604], data storage file name window [605], receive datagraphic curve display window [606], receive data list display window [607], on data sequence reception operation interface guidance panel [601], also be provided with the feature operation virtual push button, it is respectively " reception " button [608], " stop " button [609], the Back button [610], use " reception " button, PORT COM receiving data information from current appointment, filter receiving data, show at reception datagraphic curve display window [606] and reception data list display window [607], and be written in the defined file of data storage file name window [605], use " stopping " button, stop PORT COM receiving data information from current appointment, use the Back button, just turn back to the upper level operation interface.
8. a kind of ARINC429 data bus emulation test system according to claim 1, it is characterized in that data transmit operation interface has the PORT COM of selection, selects communication speed, selects data definition and identity code function, when being in transmit status, the data of data buffer and the data definition identity code combination of current selection will be sent, be assembled into the data layout that is fit to ARINC-429 communication transmission, send data from selected PORT COM, finish a transmit operation.
Data transmit operation interface comprises guidance panel [701], guidance panel [701] is provided with PORT COM selective listing frame [702], communication speed selective listing frame [703], data definition and identity code selective listing frame [704], data send buffer zone display window [705], on data transmit operation interface operation panel [701], also be provided with the feature operation virtual push button, it is respectively " transmission " button [706], " stop " button [707], the Back button [708], use " transmission " button, data are sent the PORT COM transmission of buffer zone display window data from current appointment, use " stopping " button, stop to send data message from the PORT COM of current appointment, use the Back button, just turn back to the upper level operation interface.
9. a kind of ARINC429 data bus emulation test system according to claim 1, it is characterized in that discrete and function type data transmit operation interface has the selection PORT COM, select communication speed, select to send turnover rate, select data definition and identity code, select the discrete data file, select the data definition function performance, when being in transmit status, from discrete data file reading of data, perhaps produce data according to the defined function of data definition function, data definition identity code combination with current selection, be assembled into the data layout that is fit to ARINC-429 communication transmission, send data from selected PORT COM, data transmitting period is upgraded according to sending turnover rate, up to finishing transmit operation or having stopped the data transmit operation;
Discrete and function type data transmit operation interface comprises guidance panel [801], guidance panel [801] is provided with PORT COM selective listing frame [802], communication speed selective listing frame [803], send turnover rate definition list box [804], data definition and identity code selective listing frame [805], send discrete data file display window [806], data definition function selective listing frame [807], on discrete and function type data transmit operation interface operation panel [801], also be provided with the feature operation virtual push button, it is respectively " transmission " button [809], " stop " button [810], the Back button [811], use " transmission " button, from sending the discrete data file reading of data of discrete data file display window [806] appointment, perhaps produce data according to the defined function of data definition function selective listing frame [807], the data definition identity code of selecting with data definition and identity code selective listing frame [805] makes up, send from the PORT COM of current appointment, use " stopping " button, stop to send data message from the PORT COM of current appointment, use the Back button, just turn back to the upper level operation interface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101119743A CN102289208A (en) | 2011-04-22 | 2011-04-22 | Simulation test system for ARINC (Aeronautical Radio Incorporated) 429 data bus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101119743A CN102289208A (en) | 2011-04-22 | 2011-04-22 | Simulation test system for ARINC (Aeronautical Radio Incorporated) 429 data bus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102289208A true CN102289208A (en) | 2011-12-21 |
Family
ID=45335698
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011101119743A Pending CN102289208A (en) | 2011-04-22 | 2011-04-22 | Simulation test system for ARINC (Aeronautical Radio Incorporated) 429 data bus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102289208A (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106354027A (en) * | 2015-07-17 | 2017-01-25 | 陕西千山航空电子有限责任公司 | ICD (interface control document)-oriented RS422 bus signal simulation testing method |
| CN107689895A (en) * | 2017-07-04 | 2018-02-13 | 西安飞机工业（集团）有限责任公司 | A kind of detection method and detection means of aviation ARINC429 signals |
| CN109032860A (en) * | 2018-06-27 | 2018-12-18 | 中国直升机设计研究所 | A kind of ARINC429 bus general purpose simulation system and emulation mode |
| CN109426507A (en) * | 2017-08-25 | 2019-03-05 | 中车株洲电力机车研究所有限公司 | A kind of cabinet equipment document distribution method and system |
| CN109855651A (en) * | 2018-11-12 | 2019-06-07 | 中航通飞研究院有限公司 | The ground testing system and test method of modern aircraft radio communication navigation system |
| CN110488630A (en) * | 2019-07-15 | 2019-11-22 | 中国人民解放军第五七二一工厂 | A kind of control increases steady flight control computer test macro and test method |
| CN110704353A (en) * | 2019-09-30 | 2020-01-17 | 北京航空航天大学 | CPCI-ARINC429 hot plug system |
| CN110838961A (en) * | 2019-10-12 | 2020-02-25 | 沈阳航空航天大学 | General aviation bus message scheduling system |
| CN111277452A (en) * | 2019-08-29 | 2020-06-12 | 上海飞机制造有限公司 | Bus data testing method, device, equipment and storage medium |
| CN112162495A (en) * | 2020-09-25 | 2021-01-01 | 中国直升机设计研究所 | Inertial navigation simulation system and method based on ARINC429 bus |
| CN112498736A (en) * | 2019-09-16 | 2021-03-16 | 上海飞机制造有限公司 | Universal bus test system suitable for AFDX bus |
| CN113514716A (en) * | 2021-04-20 | 2021-10-19 | 北京航空航天大学 | Digital bus electromagnetic environment effect simulation device and method |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070164166A1 (en) * | 2006-01-17 | 2007-07-19 | Jukka Matti Hirvonen | Apparatus and method for backup control in a distributed flight control system |
| US20080100474A1 (en) * | 2006-10-12 | 2008-05-01 | Avion Engineering Services Inc. Dba Avion Partners | Flight information module |
| CN101226402A (en) * | 2007-12-13 | 2008-07-23 | 陕西飞机工业（集团）有限公司 | Method and apparatus for detecting airplane digital type fuel oil measurement control system |
| CN101482753A (en) * | 2009-02-11 | 2009-07-15 | 北京华力创通科技股份有限公司 | Real-time simulation apparatus and system of redundancy flight control computer |
-
2011
- 2011-04-22 CN CN2011101119743A patent/CN102289208A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070164166A1 (en) * | 2006-01-17 | 2007-07-19 | Jukka Matti Hirvonen | Apparatus and method for backup control in a distributed flight control system |
| US20080100474A1 (en) * | 2006-10-12 | 2008-05-01 | Avion Engineering Services Inc. Dba Avion Partners | Flight information module |
| CN101226402A (en) * | 2007-12-13 | 2008-07-23 | 陕西飞机工业（集团）有限公司 | Method and apparatus for detecting airplane digital type fuel oil measurement control system |
| CN101482753A (en) * | 2009-02-11 | 2009-07-15 | 北京华力创通科技股份有限公司 | Real-time simulation apparatus and system of redundancy flight control computer |
Non-Patent Citations (2)
| Title |
|---|
| 万凤琴: "智能化飞机燃油管理系统中ARINC429通讯技术的研究", 《航空精密制造技术》, vol. 45, no. 02, 15 April 2009 (2009-04-15) * |
| 杨勇等: "一种飞控系统信号源仿真设备的设计与实现", 《测控技术》, vol. 27, no. 03, 31 December 2008 (2008-12-31), pages 24 - 26 * |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106354027A (en) * | 2015-07-17 | 2017-01-25 | 陕西千山航空电子有限责任公司 | ICD (interface control document)-oriented RS422 bus signal simulation testing method |
| CN107689895A (en) * | 2017-07-04 | 2018-02-13 | 西安飞机工业（集团）有限责任公司 | A kind of detection method and detection means of aviation ARINC429 signals |
| CN109426507A (en) * | 2017-08-25 | 2019-03-05 | 中车株洲电力机车研究所有限公司 | A kind of cabinet equipment document distribution method and system |
| CN109032860A (en) * | 2018-06-27 | 2018-12-18 | 中国直升机设计研究所 | A kind of ARINC429 bus general purpose simulation system and emulation mode |
| CN109855651A (en) * | 2018-11-12 | 2019-06-07 | 中航通飞研究院有限公司 | The ground testing system and test method of modern aircraft radio communication navigation system |
| CN109855651B (en) * | 2018-11-12 | 2023-10-27 | 中航通飞华南飞机工业有限公司 | Ground test system and test method for modern aircraft radio communication navigation system |
| CN110488630A (en) * | 2019-07-15 | 2019-11-22 | 中国人民解放军第五七二一工厂 | A kind of control increases steady flight control computer test macro and test method |
| CN110488630B (en) * | 2019-07-15 | 2022-11-18 | 中国人民解放军第五七二一工厂 | Test system and test method for controlling stability-increasing flight control computer |
| CN111277452A (en) * | 2019-08-29 | 2020-06-12 | 上海飞机制造有限公司 | Bus data testing method, device, equipment and storage medium |
| CN112498736A (en) * | 2019-09-16 | 2021-03-16 | 上海飞机制造有限公司 | Universal bus test system suitable for AFDX bus |
| CN110704353A (en) * | 2019-09-30 | 2020-01-17 | 北京航空航天大学 | CPCI-ARINC429 hot plug system |
| CN110838961A (en) * | 2019-10-12 | 2020-02-25 | 沈阳航空航天大学 | General aviation bus message scheduling system |
| CN112162495A (en) * | 2020-09-25 | 2021-01-01 | 中国直升机设计研究所 | Inertial navigation simulation system and method based on ARINC429 bus |
| CN113514716A (en) * | 2021-04-20 | 2021-10-19 | 北京航空航天大学 | Digital bus electromagnetic environment effect simulation device and method |
| CN113514716B (en) * | 2021-04-20 | 2023-03-03 | 北京航空航天大学 | Digital bus electromagnetic environment effect simulation device and method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102289208A (en) | Simulation test system for ARINC (Aeronautical Radio Incorporated) 429 data bus | |
| CN102938713A (en) | 1553B data bus testing simulation system | |
| CN109855651B (en) | Ground test system and test method for modern aircraft radio communication navigation system | |
| CN103516551B (en) | Utilize passive pair of RFID tag to optical fiber physical port intelligent management system | |
| CN103116287B (en) | Avionics equipment running environment dynamic simulating device and method | |
| CN109116315B (en) | General radar avionics simulation system | |
| CN111124927B (en) | Testing method for multi-partition airborne software | |
| CN109270918A (en) | A kind of aircraft avionics floor synthetic debugging system based on performance test | |
| CN102999425A (en) | Housekeeping software simulation test system based on technology of virtual instrument | |
| CN110275833B (en) | Universal test equipment and use method | |
| EP3001367A1 (en) | Method and system for preparing aircraft maintenance application data for portable devices | |
| CN103970024A (en) | Real-time simulation system of large aircraft hydraulic system | |
| CN107480327A (en) | A kind of emulation verification method, device and electronic equipment | |
| CN112162495A (en) | Inertial navigation simulation system and method based on ARINC429 bus | |
| CN102945001A (en) | Servo actuator system simulator and simulation method thereof | |
| CN106776321A (en) | A kind of winged guard system software emulation contrast conversion method based on dynamic link library | |
| CN201413462Y (en) | Novel data collector | |
| CN201766599U (en) | Airborne radio installation automatic test system | |
| CN109557898A (en) | A kind of general-purpose system comprehensive verification equipment for various UAV ground control station | |
| US20110246975A1 (en) | Control architecture and process for porting application software for equipment on board an aircraft to a consumer standard computer hardware unit | |
| CN103514074A (en) | MVB network card development method and platform | |
| CN109842534A (en) | A kind of equipment test verification method based on switch type FC artificial card | |
| CN112416715B (en) | Computer interlocking performance test system based on operation scene | |
| zu Hörste et al. | Modelling functionality of train control systems using petri nets | |
| CN103576667A (en) | Main control panel test method, device and system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20111221 |