CN108287959A - Artificial intelligence program person writes digital aircraft source code specifications decision and executes method - Google Patents
Artificial intelligence program person writes digital aircraft source code specifications decision and executes method Download PDFInfo
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Abstract
The present invention proposes artificial intelligence program person and writes digital aircraft source code specifications decision execution method, includes the following steps：Digital aircraft source code is decomposed at many levels；It establishes digital aircraft source code and writes decision tree；The artificial intelligence program person for executing specification writing operation is established according to decision tree branches situation；The configuration information that scene is generated needed for reading generates digital aircraft emulation source program.Artificial intelligence program person proposed by the present invention writes digital aircraft source code specifications decision and executes method, greatly alleviates the workload of people, shortens the lead time of digital aircraft, preferably provides safeguard for the Life cycle of aircraft.It ensure that the objectivity and versatility of simulated program, the requirement for later Complex Battlefield Environments and combat duty to aircraft and the requirement to operator provide research, study, training platform.
Description
Technical field
The present invention relates to a kind of source code intelligent writing decision-making technic field, more particularly to a kind of artificial intelligence
Programmer writes digital aircraft source code specifications decision and executes method.
Background technology
Digital Simulation is because its cost advantage is widely used in fields such as satellite, guided missile, unmanned planes, not with computer technology
Disconnected development, application percentage is constantly promoted in the whole life cycles such as various Flight Vehicle Designs, test, operation.Digital Simulation
Main problem is the difference of same real system, thus how to ensure function between the two, composition, structure, pattern, program,
The completely the same of operation is critical issue.The artificial standby digital aircraft with real system consistency of writting tool emulates source program work
Work amount is huge, the period is longer, and in face of the increase of aircraft type, model, and this limitation is more obvious.
Face the future complex environment and mission requirements, and the cooperation between aircraft is gradually promoted with confrontation, every field
The difference of modeling specification causes the integrated difficulty of digital aircraft larger, and manually writes emulation and inevitably inadvertently bring into
The subjective factor of people, the above problem propose challenge to the objectivity and versatility of digital Modeling of Vehicle.
Therefore, how a kind of artificial intelligence for overcoming Digital Simulation limitation and emulating the integration problem that difference is brought is provided
Programmer writes digital aircraft source code specifications decision and executes the problem of method is those skilled in the art's urgent need to resolve.
Invention content
In view of this, the present invention provides a kind of artificial intelligence program person's writing digital aircraft source code specifications decision execution
Method, this method are brought for the artificial limitation for writing digital aircraft emulation source code and each field Digital Simulation difference
Integration problem, propose using artificial intelligence technology structure intelligent program person realize digital aircraft emulation source code quick intelligence
It can structure.
To achieve the goals above, the present invention adopts the following technical scheme that：
A kind of artificial intelligence program person's writing digital aircraft source code specifications decision execution method, which is characterized in that packet
Include following steps：
Step 1 decomposes digital aircraft source code using a variety of dimension decomposition methods at many levels, obtains minimum point
Solve result；
Step 2 clusters the minimal decomposition result, and establishes digital aircraft source code and write decision tree；
Step 3 establishes the artificial intelligence program person for executing specification writing operation according to decision tree branches situation；
Step 4 reads the required configuration information for generating scene using the artificial intelligence program person and generates digital aircraft
Emulate source program.
Preferably, a variety of dimension decomposition methods include at least in the step 1：Code level, type of aircraft, system dimension,
Emulate the combined crosswise between granularity and a variety of dimension decomposition methods.
According to code hierachical decomposition, including system layer and application layer；
Include guided missile, satellite, unmanned plane, rocket by type of aircraft decomposition；
It includes subsystem, component, element to each type of aircraft decompose by system dimension；It is tieed up to source code by system
It includes engineering, file, variable, function decompose.
By emulation granularity decompose, from comprising subsystem angle decomposition be Subsystem emulation, multiple subsystem emulation, full subsystem
System emulation emulates granularity from low fidelity ideal subsystem model to sophisticated subsystems mould for the subsystem according to subsystem
Type resolves into a variety of granularities, from partial model emulation granularity be decomposed into ideal components model, be added global error partial model,
Partial model, the part component level high fidelity partial model of failure is added.
Preferably, the step 2 specifically includes：
(1) the minimal decomposition result is clustered, provides the applicable object and applicable elements of branch after cluster；
(2) after clustering the minimal decomposition result, decision tree is established.
Preferably, the cluster is according to including versatility, work-based logic mode：
The application layer code in code level is clustered according to versatility, including all aircraft are general, same class
Type aircraft is general, the different special three parts of aircraft model；
Aircraft motion control portion is clustered according to aircraft work-based logic mode, including flight state determines
Module, the status monitoring of flight course and meets specific condition switch logic module, aircraft motion-control module.
Preferably, in the step 3：
Execution method is write to source code and is selected according to the scope of application, change frequency, variation pattern factor, establishes intelligence
It can programmer；
It includes saving as file, saving as database, be fixed on writing logic manually to write working specification and execute method
In intelligent program person.
Preferably, the step 4 specifically includes：
(1) it includes aircraft configuration information that intelligent program person, which reads the required scene that generates,；
(2) the aircraft configuration information is successively judged according to decision tree branches applicable elements, obtains source code
Operation execution method is write, writing operation is executed and automatically generates source code.
It can be seen via above technical scheme that advantage is the present invention compared with prior art：People is replaced using computer generation
Work intelligent program person completes the digital aircraft source code intelligent writing for having clear specification, reduces the master of people in simulated program
Sight factor, while greatly alleviating the workload of people, shortening the lead time of digital aircraft, it is the full life of aircraft
Period preferably provides safeguard.Requirement for later Complex Battlefield Environments and combat duty to aircraft and operator is wanted
Offer research, study, training platform are provided.
Description of the drawings
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technology description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 attached drawings are that artificial intelligence program person provided by the invention writes the digital aircraft source code specifications decision side of execution
Method flow chart；
Fig. 2 attached drawings are the digital aircraft source code decision tree decomposition diagram that the embodiment of the present invention is established.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
The whole of digital aircraft source code specifications decision execution method is write referring to Fig. 1, Fig. 1 is artificial intelligence program person
Body flow diagram.
Step S101：Digital aircraft source code is decomposed at many levels using a variety of dimension decomposition methods.
Decomposition method includes mainly code level, type of aircraft, system dimension, emulation granularity and a variety of decomposition methods
Between combined crosswise.
Include mainly system layer and application layer two parts according to code hierachical decomposition.System layer predominantly realizes specific function
Modularization source code, it is unrelated with aircraft, in conjunction with attached drawing 2, including Fundamentals of Mathematics module, mechanical foundation module, negotiation communication
Module, data processing module, file operation module etc..Application layer is mainly the source code of aircraft section.
Include guided missile, satellite, unmanned plane, rocket etc. by type of aircraft decomposition.
It includes subsystem, component, element etc. to each type of aircraft decompose according to system dimension.It is tieed up to source by system
It includes engineering, file, variable, function that code, which decompose,.
In conjunction with attached drawing 2, by taking satellite as an example, subsystem includes structure subsystem, attitude and orbit control subsystem, power subsystem, survey
Control subsystem, promote subsystem, thermal control subsystem, number tube system, payload etc..Guided missile subsystem includes subsystem of structure
System, guidance control system, propulsion system, energy resource system, Fuse-warhead system etc..
Each subsystem carries out component decomposition, includes sensor, executing agency and controller again by taking Satellite attitude and orbit control as an example,
Sensor is decomposed into gyro, sun sensor, earth sensor, star sensor, magnetometer etc., executing agency include thruster,
Momenttum wheel, control-moment gyro, magnetic torquer etc., controller are mainly the spaceborne computer of master backup.It is deposited according between component
It includes gyro, accelerometer, 3 combinations of momenttum wheel, 3+1S combinations etc., 8 combinations, 12 of thruster to be decomposed in combined situation
Situations such as cold standby existing for a combination, 14 combinations etc. and other component and Hot Spare.
Each component source code of attitude and orbit control subsystem can be analyzed to variable-definition, component sends information, component receives information,
Partial model algorithm, unit status promote, parts data is filed.Digital aircraft source code can be analyzed to posture and determines mould again
Block, gesture stability module, mode monitoring and handover module.
It is decomposed according to emulation granularity, from can be analyzed to comprising subsystem angle, Subsystem emulates, multiple subsystem emulates, complete
Subsystem emulates, can be from low fidelity ideal subsystem model to sophisticated subsystems model decomposition at more from subsystem emulation granularity
Kind granularity can be analyzed to ideal components model, the partial model that global error is added, the portion that failure is added from partial model granularity
Part model, part component level high fidelity partial model etc..
Digital aircraft source code is decomposed into minimum level, i.e. minimal decomposition as a result, implementing using a variety of decomposition methods
To engineering, file, variable, function.Also there are many decomposition methods in addition to foregoing description, and this is no longer going to repeat them.
Step S102：It establishes digital aircraft source code and writes decision tree.
The step can be subdivided into following two small steps：
(1) minimal decomposition result is clustered, provides the applicable object and applicable elements of branch after cluster
Cluster is according to including versatility, work-based logic mode.
Application layer code is clustered according to versatility, including all aircraft are general, same type aircraft is general,
The different special three parts of aircraft model.Such as component source code portion, the component of all aircraft is substantially general, and realizes
Mode is consistent, therefore all aircraft component source codes are gathered for one kind.
It is clustered according to work-based logic mode, attitude and orbit control subsystem source code mainly determines mould including posture in satellite
Block, gesture stability module, mode monitoring and handover module, missile guidance control system include fly event monitoring and switching mould
Block, guiding module, control module, two kinds of aircraft work-based logic modes are almost the same, therefore realization method gathers for one kind, cluster
Aircraft source code motion control portion is divided into three parts by result afterwards, and first part is flight state determining module, and second
Part is the status monitoring of flight course and meets specific condition switch logic module, and Part III is aircraft motion control mould
Block.
(2) it establishes programmer and writes the complete decision tree of digital aircraft source code
After source code decomposition result is clustered, decision tree is established, digital aircraft source code decision tree as shown in Figure 2 is decomposed
Element branches result.
Step S103：The artificial intelligence program person for executing specification writing operation is established according to decision tree branches situation.
Execution method is write to source code and is selected according to the scope of application, change frequency, variation pattern factor, establishes intelligence
It can programmer.
It includes saving as file, saving as database, be fixed on writing logic manually to write working specification and execute method
In intelligent program person.
According to scope of application decomposition result, all system layer source codes are unrelated with aircraft, are fixed code, therefore use
The mode of glue file is saved as, intelligent program person copies when writing digital aircraft source program to respective paths.
According to change frequency, according to wherein variable, different, information transmits different, partial model not to each component source code
Same, a variety of ranks of partial model can all change when generation every time, therefore each component source generation of all digital aircrafts
Code is realized by the way of it will write logic and be fixed in artificial intelligence program person.Component source code includes variable-definition, portion
Part sends information, component receives information, partial model, unit status promote, parts data filing, wherein partial model, component
State promotes, parts data filing is basically unchanged, and variable-definition, part of original code of receiving and sending messages information content are larger, and changes
Frequency is high, also to be decomposed to whole part source code file, and partial model, unit status promote, parts data files 3
Source code is divided to be realized using fixed code mode, variable-definition, part of original code of receiving and sending messages are using generation program according to generation
Logic generates, and generates writing or copy that program completes source code using hybrid mode, is finally completed whole part source code text
Part generates.
Aircraft source code motion control portion described further below.The part of original code is divided into flight according to decision tree
Device state determine file, aircraft motion control file, flight course status monitoring and meet specific condition switch logic text
3 part of part.
Flight state determines that file is mainly to be transferred to the detection information of controller using state determining part part to be flown
Row device state determines, includes mainly that location determination and posture determine that algorithm is general-purpose algorithm, including gyro angular velocity, gyro
Integrate measuring angle, earth sensor measuring angle, magnetic strength measurement magnetic field intensity, accelerometer measuring acceleration, GPS receiver location information
The method that glue file is Least-cost is saved as Deng, algorithm.The state determining part part and shape used according to different aircraft
State determining module splices copy into line code by configuration result in reading database and completes this document generation.
Aircraft motion control file realization method is similar with file is determined, equally controls pid control module, momenttum wheel
Logic, thruster phase plane control logic, servos control logic save as logic-control file, are obtained and are flown by reading database
Row device executes method, completion code splicing copy.
The status monitoring of flight course includes a series of states switching monitoring letters with specific condition switch logic file is met
Number, controller parameter initialization function, state of flight defined function etc..
The state switching monitoring each fly event of function may have multiple, and aircraft is according to the state of current flight pattern
Different switch logics respectively have by judging that status information determines whether to be switched to some other event likewise as aircraft
Difference, best realization method be it is fixed in intelligent program person generate logic, according to the switching condition of configuration and target pattern into
Row generates.
Controller parameter initialization function every time switching offline mode when call, with type of aircraft, control algolithm,
Offline mode, flying scene it is different and different, therefore each aircraft has the parameter that it sets, by most preferably realizing
Mode is the fixed generation logic in intelligent program person, is generated according to the control parameter of configuration.
State of flight defined function successively calls the state of present mode to determine algorithm, state switching according to flight flow
Function, gesture stability algorithm are monitored, completes to measure the entire control process of control.Each aircraft, each pattern are different, most
Good realization method is to read configuration file by intelligent program person, is generated according to the fixed logic completion function call that generates.
Step S104：The configuration information that scene is generated needed for reading generates digital aircraft emulation source program.
The step can be subdivided into following two small steps：
(1) it includes aircraft configuration information that intelligent program person, which reads the required scene that generates,
The artificial intelligence program person formed using step S103 reads the configuration file input letter write needed for digital flight
Breath.
Configuration file includes database, formatted file (xml document), library etc. according to file type decomposition.
Configuration file is decomposed according to applicability, including all aircraft are general, each type aircraft is general, each
Model is special.
The library file of the general predominantly storage unit information of all aircraft, storage information includes unit type, each portion
The different number of element types for including under part type, variable, partial model, the interface etc. that each model component includes.
The general predominantly dynamics correlation library file of each type aircraft.
Each model Special Main will include each subsystem operating parameter of aircraft, include component and mount message, aircraft
Configuration information, information transmission processing configuration file etc..
(2) successively judged according to decision tree branches applicable elements, obtain source code and write operation execution method, execute
It writes operation and automatically generates source code
Condition criterion and sieve are met according to each level branch of decision tree branches sentence progress decision tree in intelligent program person
The affiliated minimum branch often walked in writing process is searched in choosing.
According to the Writing method of each branch, program writing is generated by source code, database reads writing, file is direct
Copy, file replace copy mode, complete whole number aerocraft system source code and write.
Digital aircraft source code specifications decision is write to artificial intelligence program person provided by the invention above and executes method
It is described in detail, part concrete case used herein is expounded the principle of the present invention and embodiment, above
Specific implementation explanation is merely used to help understand the method and core concept of the present invention；Meanwhile for those skilled in the art,
According to the thought of the present invention, in specific implementation mode and using upper there will be changes, change and improvement to the present invention are
It is possible, without the conception and scope beyond claim defined, in conclusion this specification should not be construed as to this hair
Bright limitation.
Each embodiment is described by the way of progressive in this specification, the highlights of each of the examples are with other
The difference of embodiment, just to refer each other for identical similar portion between each embodiment.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so description is fairly simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest range caused.
Claims (6)
1. a kind of artificial intelligence program person writes digital aircraft source code specifications decision and executes method, which is characterized in that including
Following steps：
Step 1 decomposes digital aircraft source code using a variety of dimension decomposition methods, obtains minimal decomposition knot at many levels
Fruit；
Step 2 clusters the minimal decomposition result, and establishes digital aircraft source code and write decision tree；
Step 3 establishes the artificial intelligence program person for executing specification writing operation according to decision tree branches situation；
Step 4 reads the required configuration information for generating scene using the artificial intelligence program person and generates digital aircraft emulation
Source program.
2. artificial intelligence program person according to claim 1 writes digital aircraft source code specifications decision and executes method,
It is characterized in that, a variety of dimension decomposition methods include at least in the step 1：Code level, type of aircraft, system dimension, emulation
Combined crosswise between granularity and a variety of dimension decomposition methods.
According to code hierachical decomposition, including system layer and application layer；
Include guided missile, satellite, unmanned plane, rocket by type of aircraft decomposition；
It includes subsystem, component, element to each type of aircraft decompose by system dimension；Source code is carried out by system dimension
Decomposition includes engineering, file, variable, function.
It is decomposed by emulation granularity, from being that Subsystem emulation, multiple subsystem emulation, full subsystem are imitative comprising subsystem angle decomposition
Very, granularity is emulated according to subsystem for the subsystem from low fidelity ideal subsystem model to sophisticated subsystems model to divide
Solution is decomposed into ideal components model at a variety of granularities, from partial model emulation granularity, the partial model that global error is added, is added
Partial model, the part component level high fidelity partial model of failure.
3. artificial intelligence program person according to claim 1 writes digital aircraft source code specifications decision and executes method,
It is characterized in that, the step 2 specifically includes：
(1) the minimal decomposition result is clustered, provides the applicable object and applicable elements of branch after cluster；
(2) after clustering the minimal decomposition result, decision tree is established.
4. artificial intelligence program person according to claim 3 writes digital aircraft source code specifications decision and executes method,
It is characterized in that, the cluster is according to including versatility, work-based logic mode：
The application layer code in code level is clustered according to versatility, including all aircraft are general, same type flies
Row device is general, the different special three parts of aircraft model；
It is clustered according to aircraft work-based logic mode, including in aircraft operation control, aircraft energy control, aircraft
Portion's PERCOM peripheral communication.
5. artificial intelligence program person according to claim 1 writes digital aircraft source code specifications decision and executes method,
It is characterized in that, in the step 3：
Execution method is write to source code and is selected according to the scope of application, change frequency, variation pattern factor, establishes intelligent journey
Sequence person；
It includes saving as file, saving as database, writing logic is fixed on artificial intelligence to write working specification and execute method
In programmer.
6. artificial intelligence program person according to claim 1 writes digital aircraft source code specifications decision and executes method,
It is characterized in that, the step 4 specifically includes：
(1) it includes aircraft configuration information that intelligent program person, which reads the required scene that generates,；
(2) the aircraft configuration information is successively judged according to decision tree branches applicable elements, obtains source code and writes
Execution method is operated, writing operation is executed and automatically generates source code.
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| CN109189376B (en) * | 2018-07-20 | 2021-06-04 | 北京航空航天大学 | Artificial intelligence writing method for digital aircraft cluster source code |
| CN109214043B (en) * | 2018-07-20 | 2023-04-07 | 北京航空航天大学 | Artificial intelligence writing method for digital aircraft dynamics environment information transmission source code |
| CN109240672B (en) * | 2018-07-20 | 2022-02-11 | 北京航空航天大学 | Artificial intelligence writing method for information transmission source code of single machine component of digital aircraft |
| CN109213473B (en) * | 2018-07-20 | 2022-03-11 | 北京航空航天大学 | Artificial intelligence generation method for daily operation process of satellite |
| CN109062549B (en) * | 2018-07-20 | 2022-07-01 | 北京航空航天大学 | Method and device for writing satellite channel telemetering decoding program by artificial intelligence |
| CN109194381A (en) * | 2018-09-11 | 2019-01-11 | 北京航空航天大学 | Between digital satellite star and star networking be wirelessly transferred code artificial intelligence Writing method |
| CN113703726A (en) * | 2021-08-26 | 2021-11-26 | 北京航空航天大学 | Iterative method for extracting and zeroing decision knowledge of source code construction of digital aircraft |
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Application publication date: 20180717 Assignee: Beijing Haiwei Technology Co.,Ltd. Assignor: BEIHANG University Contract record no.: X2023990000036 Denomination of invention: Execution method of source code of digital aircraft written by AI programmers Granted publication date: 20210504 License type: Common License Record date: 20230105 |
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