CN108549784A - Artificial intelligence writes Satellite TT and power coupled thermomechanics simulated program method and device - Google Patents
Artificial intelligence writes Satellite TT and power coupled thermomechanics simulated program method and device Download PDFInfo
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Abstract
The present invention relates to artificial intelligence to write Satellite TT and power coupled thermomechanics simulated program method and device, and this method includes：Description is formatted to Satellite TT subsystem design result；It establishes source code and writes decision tree, determine that Satellite TT and power coupled thermomechanics emulate the rules for writing and observing and controlling and power coupled thermomechanics computation rule of source code according to the decision tree；According to Green Formula data, the rules for writing and the computation rule that the Satellite TT subsystem designs, the writing that source code is emulated to Satellite TT and power coupled thermomechanics is completed.The design result of the Satellite TT subsystem of this method Green Formula, the rules for writing and computation rule determined according to decision tree, the writing that source code is emulated to multi-satellite observing and controlling and power coupled thermomechanics can be automatically performed, communication subsystem coupling Simulation research can quickly be carried out, the workload of people is reduced, efficiency of research and development is improved.
Description
Technical field
The present invention relates to a kind of source code intelligent writing method, more particularly to a kind of artificial intelligence writes Satellite TT and power
Coupled thermomechanics simulated program method and device.
Background technology
Emulation technology is a kind of technology simulated to real world using digital world, has controllability height, without broken
Bad property allows to be repeated several times, is limited the advantages such as small by current conditions.Emulation technology can promote the development efficiency and quality of product,
Shorten the R＆D cycle.
Since 20th century mid-terms, with the development of space industry, emulation technology is provided for space flight and is effectively assisted.Especially
Its nearly more than 20 years, with computer, visualization technology rapid development with merge, emulation technology is in space product development process
In obtain large-scale application, especially design etc. key links play very important effect, become space product number
The chief component of word development mode.
Observing and controlling emulation is the important component of space flight digital product.Communication subsystem system is to ensure safety satellite flight
Important system.System has the function of record flight data, is collection analysis telemetry, the in-orbit state of verifying satellites, control
The important means of satellite transit processed.It studies communication subsystem and control subsystem, thermal control subsystem, power supply subsystems couple is imitative
Very, communication subsystem state can be really assessed in dynamic environment, and support is provided for design of satellites and decision.Difference is defended
Star, there is a corresponding communication subsystem, and when for multi-satellite, it is required for individually developing a set of communication subsystem, work
Work amount is big, the period is long.
Invention content
In view of the above problems, it is proposed that the present invention overcoming the above problem in order to provide one kind or solves at least partly
A kind of artificial intelligence for stating problem writes Satellite TT and power coupled thermomechanics simulated program method and device.
In a first aspect, the embodiment of the present invention, which provides artificial intelligence, writes Satellite TT and power coupled thermomechanics simulated program side
Method, this method include：
Description is formatted to Satellite TT subsystem design result；
It establishes source code and writes decision tree, determine that Satellite TT emulates source code with power coupled thermomechanics according to the decision tree
Rules for writing and observing and controlling and power coupled thermomechanics computation rule；
According to Green Formula data, the rules for writing and the calculating rule of Satellite TT subsystem design
Then, the writing to Satellite TT and power coupled thermomechanics emulation source code is completed.
In one embodiment, description is formatted to Satellite TT subsystem design result, including：
Component names, configuration information, communication link and the channel information for including to communication subsystem design result carry out lattice
Formulaization describes；The data of Green Formula are saved in XML file and database.
In one embodiment, the rules for writing of the Satellite TT and power coupled thermomechanics emulation source code, including：
Observing and controlling and power coupled thermomechanics emulation source code are divided into the related source code of dynamics environment and physical components model phase
Close source code；
By way of copying and being inserted into, the writing to dynamics environment correlation source code is completed；
To the component names of communication subsystem, configuration information, communication link and led to according to XML file and database preservation
Road information completes the writing to physical components model correlation source code.
In one embodiment, the observing and controlling and power coupled thermomechanics computation rule, including：
The calculating that communication subsystem is coupled with control subsystem；
The calculating of communication subsystem and power supply subsystems couple；
The calculating of communication subsystem and thermal control subsystems couple.
Second aspect, the embodiment of the present invention provide artificial intelligence and write Satellite TT and power coupled thermomechanics simulated program dress
It sets, including：
Formatting module, for being formatted description to Satellite TT subsystem design result；
Determining module is established, decision tree is write for establishing source code, Satellite TT and power is determined according to the decision tree
The rules for writing of coupled thermomechanics emulation source code and observing and controlling and power coupled thermomechanics computation rule；
Module is write, Green Formula data, the rules for writing for being designed according to the Satellite TT subsystem
With the computation rule, the writing that source code is emulated to Satellite TT and power coupled thermomechanics is completed.
In one embodiment, the formatting module, specifically for the component for including to communication subsystem design result
Title, configuration information, communication link and channel information are formatted description；The data of Green Formula are saved in XML texts
Part and database.
In one embodiment, described to establish determining module, determining Satellite TT emulates source code with power coupled thermomechanics
Rules for writing, including：Observing and controlling and power coupled thermomechanics emulation source code are divided into the related source code of dynamics environment and entity portion
Part model correlation source code；By way of copying and being inserted into, the writing to dynamics environment correlation source code is completed；According to XML
File, to the component names of communication subsystem, configuration information, communication link and channel information, is completed to reality with database preservation
The writing of body component model correlation source code.
In one embodiment, described to establish determining module, the observing and controlling got determined is calculated with power coupled thermomechanics and is advised
Then, including：The calculating that communication subsystem is coupled with control subsystem；The calculating of communication subsystem and power supply subsystems couple；It surveys
Control the calculating of subsystem and thermal control subsystems couple.
The advantageous effect of above-mentioned technical proposal provided in an embodiment of the present invention includes at least：
Artificial intelligence provided in an embodiment of the present invention writes Satellite TT and power coupled thermomechanics simulated program method and device,
This method includes：Description is formatted to Satellite TT subsystem design result；It establishes source code and writes decision tree, according to institute
It states decision tree and determines that the rules for writing of Satellite TT and power coupled thermomechanics emulation source code and observing and controlling are calculated with power coupled thermomechanics
Rule；It is complete according to Green Formula data, the rules for writing and the computation rule that the Satellite TT subsystem designs
The writing of pairs of Satellite TT and power coupled thermomechanics emulation source code.The design of the star communication subsystem of this method Green Formula
As a result, determining determining rules for writing and computation rule according to decision tree, can be automatically performed to multi-satellite observing and controlling and power heat
It is electrically coupled the writing of emulation source code, can quickly carry out communication subsystem coupling Simulation research, reduce the workload of people, raising is ground
Send out efficiency.
Other features and advantages of the present invention will be illustrated in the following description, also, partly becomes from specification
It obtains it is clear that understand through the implementation of the invention.The purpose of the present invention and other advantages can be by the explanations write
Specifically noted structure is realized and is obtained in book, claims and attached drawing.
Below by drawings and examples, technical scheme of the present invention will be described in further detail.
Description of the drawings
Attached drawing is used to provide further understanding of the present invention, and a part for constitution instruction, the reality with the present invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings：
Fig. 1 is that artificial intelligence provided in an embodiment of the present invention writes Satellite TT and power coupled thermomechanics simulated program method
Flow chart；
Fig. 2 is the schematic diagram of the TTC channel of an example provided in an embodiment of the present invention；
Fig. 3 is that artificial intelligence provided in an embodiment of the present invention writes Satellite TT and power coupled thermomechanics simulated program device
Block diagram.
Specific implementation mode
The exemplary embodiment of the disclosure is more fully described below with reference to accompanying drawings.Although showing the disclosure in attached drawing
Exemplary embodiment, it being understood, however, that may be realized in various forms the disclosure without should be by embodiments set forth here
It is limited.On the contrary, these embodiments are provided to facilitate a more thoroughly understanding of the present invention, and can be by the scope of the present disclosure
Completely it is communicated to those skilled in the art.
Satellite TT according to the present invention emulates source code with power coupled thermomechanics, can be directed to multi-satellite and use, often
One satellite has one's own communication subsystem, the communication subsystem design of different satellites both to have similar frame knot
Structure, and with information such as different configurations.Shown in referring to Fig.1, artificial intelligence provided in an embodiment of the present invention writes Satellite TT
With power coupled thermomechanics simulated program method, including step S101~S103：
S101, description is formatted to Satellite TT subsystem design result；
S102, source code writing decision tree is established, determines that Satellite TT is emulated with power coupled thermomechanics according to the decision tree
The rules for writing of source code and observing and controlling and power coupled thermomechanics computation rule；
S103, Green Formula data, the rules for writing and the meter designed according to the Satellite TT subsystem
Rule is calculated, the writing for emulating source code to Satellite TT and power coupled thermomechanics is completed.
Green Formula data in step S101, for example the data type generated is consistent, unit is consistent；Either by data
Storage mode is consistent, for example is unified into binary format data and (octal system true form, hexadecimal is all converted to binary system
Source code).
Source code is established in step S102 and writes decision tree, determines that Satellite TT is emulated with power coupled thermomechanics according to decision tree
The rules for writing of source code and observing and controlling and power coupled thermomechanics computation rule are mainly conducive to artificial intelligence and write.
Step S103 is realized and is write according to the rules for writing and computation rule in the data and S102 of S101 Green Formulas
Satellite TT emulates source code with power coupled thermomechanics.
In the present embodiment, the design result of the Satellite TT subsystem of this method Green Formula is determined according to decision tree
Rules for writing and computation rule, the book that each Satellite TT and power coupled thermomechanics are emulated with source code can be automatically performed
It writes, can quickly carry out communication subsystem coupling Simulation research for multi-satellite, reduce the workload of people, improve efficiency of research and development.
In one embodiment, step S101 is embodied as being formatted description to communication subsystem design result；
Then the data of Green Formula are saved in XML (eXtensible Markup Language, extensible markup language) texts
In part and database.Communication subsystem Green Formula process is by interface program to communication subsystem design result into row format
Change record, and design result is preserved using Xml design documents and database.
The data of Green Formula can be stored in formatted document, such as extensible markup language (eXtensible
Markup Language, XML) formatted document or lightweight data interchange format (JavaScript Object
Notation, JSON) document.Wherein XML document and JSON document be easy to people read and write, while be also easy to machine parsing and
It generates.The embodiment of the present disclosure does not limit this.In addition can be according to the programming language for writing code, selection is using such as
The databases such as Access, Oracle, DB2, Sybase, MS SQL Server, Informax, MySQL, such as program language is
When ASP.NET, using ACCESS or MS SQL Server databases.The embodiment of the present disclosure does not limit this.
Further, description is formatted to communication subsystem design result, including：To communication subsystem design result
Including component names, configuration information, communication link and channel information be formatted description.
Communication subsystem design process includes that subsystem includes subassembly selection and configures, communication link and channel selecting.It surveys
Control subsystem component includes but not limited to ordinary antennas, omnidirectional antenna, transceiver, power amplifier, spread spectrum answering machine, duplex
Device, power splitter.The communication subsystems core parameters such as antenna gain, power amplifier gain, transceiver signal-to-noise ratio are defined in corresponding component.
According to design of satellites result or design requirement, the suitable component of selection parameter configures installation point and Installation posture, complete
At communication subsystem subassembly selection.
It determines uplink, downlink, and corresponding communication subsystem component is selected according to link requirements.According to data transmission need
It asks, selects antenna channels.
In the present embodiment, design result is saved in Xml files and database.Wherein, Xml files preserve subsystem component
Configuration result, including but not limited to component mount message.It flows design database and preserves link design result.Parts data library preserves
Component detail parameters.
Such as：Some design of satellites is as a result, the component of its observing and controlling with having star TT＆C antenna, power splitter, duplexer, spread spectrum
Answering machine, solid-state amplifier, spaceborne computer etc..Its TTC channel formed is with reference to shown in Fig. 2.
By taking TT＆C antenna A1 as an example, main design parameters are with reference to table 1；
1 TT＆C antenna parameter of table
| Upstream frequency | 12GHz |
| Downstream frequency | 8GHz |
| Antenna transmission power | 16W |
| Antenna transmitting gain | 4dBi |
| Antenna launch loss | -1dB |
| Antenna receives loss | -1dB |
| Noise power | -128.6dBW |
| Minimum angle of elevation | 5° |
| Antenna half-power beamwidth | 90° |
It is translated into Green Formula record.By taking the installation of antenna A1 components as an example, the installation matrix of component uses xml languages
Speech record, format are
The part design parameter of antenna records in the database, such as shown in table 2；
2 TT＆C antenna reference record of table
Antenna channels are stored in database, and use numeral index.Channel selecting result is in xml document using corresponding
Number is recorded, and if routine observing and controlling channel A is formed by primary antenna communication link in Fig. 2, recording mode is
In one embodiment, the writing of the Satellite TT determined in step S102 and power coupled thermomechanics emulation source code is advised
Then, specially：
Artificial intelligence program person writes Satellite TT power coupled thermomechanics emulation source code process and is related to acquisition of information, writes and determine
Plan tree establishes, writes module automatically.
Data obtaining module reads the design result that artificial intelligence program person writes Satellite TT subsystem under current working
Green Formula record, specifically include the component and its configuration information that communication subsystem includes, communication link and channel information.
Intelligent writing module realizes that Satellite TT power coupled thermomechanics emulation source code writes the foundation of decision tree.By existing
The corresponding emulation source code of different satellites and satellite operating mode forms source code program collection.Procedure set is decomposed into function, it is right
Function involved by simulated program is clustered by versatility, and simulated program is divided into and is all suitable for all satellites by cluster result
With the satellite operating mode scene being only applicable to corresponding to current design result.Under the read current working of combining information acquisition module
Satellite TT subsystem design result intelligent writing decision tree is established according to cluster module division result, determine each module
Normalized written.
For the versatility module that cluster result is obtained, major function is to realize the dynamics environment emulation of satellite, can be fitted
For structure, different, component configures different satellites.The corresponding simulated program source code of the module is relatively more fixed, saves as C/C+
The form of+program source file and header file forms code library.The calculating need that artificial intelligence program person is related to according to simulation process
It asks, corresponding source code is chosen from code library, computing module is formed after splicing.Specifically, imitative in observing and controlling power coupled thermomechanics
In very, artificial intelligence program person calculates demand for observing and controlling, mechanics, thermal control, extracted from code library observing and controlling simulation calculation code,
Mechanics Simulation calculation code, thermal control simulation calculation code, observing and controlling Coupling with Mechanics calculation code, observing and controlling thermal control coupling calculation code,
Observing and controlling obtains coupling computing module for being electrically coupled calculation code, splicing.
For the emulation module for being only applicable to present satellites scene that cluster obtains, satellite component mould is functionally corresponded to
Type source code.Physical components model is the digital expression of real satellite component, has gathered functional mode involved by component, power
, calorifics, electricity rule.The partial code uses rule-based writing since different components has different characteristics
Method.Component models rules for writing predetermined member emulates source code package containing sub-portions such as initialization, the refreshings of dynamics interface, state
Point, it is retrieved from code library, xml record results and database by artificial intelligence program person and extracts number needed for automatic write
According to, such as parameters of operating part and state information, component function model source code segment, complete the writing of emulation source code.
By emulation source code Function Decomposition, observing and controlling and power coupled thermomechanics emulation source code are divided into dynamics environment correlated source
Code source code related to physical components model.
Dynamics environment is resolved, content has versatility, is applicable to structure difference, component configures different defend
Star.Its source code content is fixed, and is stored in the form of C language project file in general file folder.Writing program is by directly copying
The mode of shellfish completes the writing to dynamics environment file.
Physical components model is the digital expression of real satellite component, has gathered functional mode involved by component, power
, calorifics, electricity rule.Dynamics environment resolves information of the code according to component, and the real-time dynamic for completing simulation parameter calculates.
Physical components model correlated source code is write, document architecture is solidificated in source code writing program.In conjunction with
The parameters of operating part that database preserves is write with state information and with the component function model source code segment that document form preserves
Program completes the writing to partial model file.
In one embodiment, the observing and controlling and power coupled thermomechanics computation rule that step S102 is determined, include the meter of three aspects
It calculates：
(1), the calculating that communication subsystem is coupled with control subsystem exists for calculating communication subsystem with control subsystem
Interact the influence of generation in simulation process；
(2), the calculating of communication subsystem and power supply subsystems couple exists for calculating communication subsystem with power supply subsystem
Interact the influence of generation in simulation process；
(3), the calculating of communication subsystem and thermal control subsystems couple exists for calculating communication subsystem with thermal control subsystem
Interact the influence of generation in simulation process.
The calculating of above-mentioned three aspect is described in detail below.
(1) communication subsystems and control subsystem coupling calculation；
The coupling of communication subsystem and control subsystem is mainly reflected in satellite position, posture, antenna direction can to observing and controlling
The influence of opinion property and satellite orbital altitude influence antenna transmission power free space loss.
Include the calculating of three aspects.
A. dynamics environment calculates；
Suffered external force and moment of face are obtained according to satellite current location and posture, exports to obtain according to satellite control subsystem
Control force and control moment.Satellite accelerations are obtained by the resultant force of external force and control force, by the resultant force of moment of face and control moment
Square obtains satellite angular acceleration.Satellite velocities and angular speed can be obtained by integral operation, and then update Satellite Orbital Attitude.
B. observing and controlling visibility；
Communication subsystem earth station visibility is mainly influenced by the attitude of satellite and antenna direction.
It can geometrically calculated in conjunction with antenna mounting locations and Installation posture according to real-time satellite orbit, posture information
The coverage area of antenna in space.According to ground control station information, observing and controlling visibility is judged.
C. loss calculation；
Communication subsystem communication link gain is influenced by orbit altitude.
Dominant loss is free space loss to the radio wave that space communication is relied in the air.Free space loss by
Propagation distance influences, and distance is remoter, and transmission loss is bigger.According to satellite orbital altitude meter earth station height above sea level, calculate in real time
Radio range resolves free space loss.
(2) communication subsystems and power supply subsystem coupling calculation；
The coupling of communication subsystem and power supply subsystem is mainly reflected in measuring and controlling equipment working condition to whole star plant capacity
Influence.
I. power supply environment calculates；
According to satellite orbit, posture information, solar vector is obtained.According to solar vector and windsurfing corner, it is defeated to calculate windsurfing
Go out power.The equipment that real-time statistics satellite is in open state, computing device general power.In conjunction with charge and discharge electric equilibrium rule, to electricity
The data such as source charging or discharging current, parallel regulator electric current carry out real-time resolving.
II. observing and controlling influences thermal control；
Satellite TT equipment peak working load power can account for nearly the 50% of the total peak power of satellite.Measuring and controlling equipment switching on and shutting down will
Satellite equipment general power statistical result is seriously affected, battery charging and discharging stream, parallel regulator curent change are caused.
(3) communication subsystems and thermal control subsystems couple computational methods；
The coupling of communication subsystem and power supply subsystem is mainly reflected in measuring and controlling equipment working condition to whole star thermal power
It influences.
1. surroundings calculate；
According to satellite real time position and posture, calculate current time earth vector, solar vector, resolve solar radiation,
Ball albedo radiation, earth infra-red radiation, obtain satellite Orbital heat flux.According to each component thermal power of satellite, the real-time heat production of computing device
Amount, statistics obtain hot-fluid in satellite.According to equation of heat balance principle, to satellite surface radiation heat transfer and internal radiation, conduction
Heat transfer process is calculated, and each part temperatures of satellite are obtained.
2. observing and controlling influences thermal control；
Measuring and controlling equipment works a large amount of heat production, and local temperature is caused to increase.Calculation of thermodynamics according to heat balance principle, in conjunction with
Heater button state change updates whole star temperature field.
In the present embodiment, emulated by communication subsystem and control subsystem, power supply subsystem, thermal control subsystems couple,
Communication subsystem simulation result is resolved, reference is provided for the design and review double calculation of communication subsystem.
Artificial intelligence provided by the invention writes Satellite TT and power coupled thermomechanics simulated program method, such as according to flight
Device (satellite) design result emulates source code rules for writing in conjunction with digital satellite, realizes that Satellite TT is emulated with power coupled thermomechanics
The automatic writing of source code.The simulated program of generation can cope with different artificial tasks, be not necessarily to secondary development.This solution avoids
The overlapping development of people works, and improves program development efficiency.
Based on same inventive concept, the embodiment of the present invention additionally provides artificial intelligence and writes Satellite TT and power coupled thermomechanics
Simulated program device, since principle and the aforementioned artificial intelligence of the solved problem of the device write Satellite TT and power coupled thermomechanics
Simulated program method is similar, therefore the implementation of the device may refer to the implementation of preceding method, and overlaps will not be repeated.
Second aspect, the embodiment of the present invention provide artificial intelligence and write Satellite TT and power coupled thermomechanics simulated program dress
It sets, with reference to shown in Fig. 3, including：
Formatting module 31, for being formatted description to Satellite TT subsystem design result；
Establish determining module 32, for establish source code write decision tree, according to the decision tree determine Satellite TT with
The rules for writing of power coupled thermomechanics emulation source code and observing and controlling and power coupled thermomechanics computation rule；
Module 33 is write, the Green Formula data, the writing for being designed according to the Satellite TT subsystem are advised
Then with the computation rule, the writing that source code is emulated to Satellite TT and power coupled thermomechanics is completed.
In one embodiment, the formatting module 31, specifically for the portion for including to communication subsystem design result
Part title, configuration information, communication link and channel information are formatted description；The data of Green Formula are saved in XML
File and database.
In one embodiment, the Satellite TT for establishing the determination of determining module 32 emulates source code with power coupled thermomechanics
Rules for writing, including：Observing and controlling and power coupled thermomechanics emulation source code are divided into the related source code of dynamics environment and entity portion
Part model correlation source code；By way of copying and being inserted into, the writing to dynamics environment correlation source code is completed；According to XML
File, to the component names of communication subsystem, configuration information, communication link and channel information, is completed to reality with database preservation
The writing of body component model correlation source code.
In one embodiment, the observing and controlling for establishing the determination of determining module 32 and power coupled thermomechanics computation rule, including：
The calculating that communication subsystem is coupled with control subsystem；The calculating of communication subsystem and power supply subsystems couple；Communication subsystem
With the calculating of thermal control subsystems couple.
It should be understood by those skilled in the art that, the embodiment of the present invention can be provided as method, system or computer program
Product.Therefore, complete hardware embodiment, complete software embodiment or reality combining software and hardware aspects can be used in the present invention
Apply the form of example.Moreover, the present invention can be used in one or more wherein include computer usable program code computer
The shape for the computer program product implemented in usable storage medium (including but not limited to magnetic disk storage and optical memory etc.)
Formula.
The present invention be with reference to according to the method for the embodiment of the present invention, the flow of equipment (system) and computer program product
Figure and/or block diagram describe.It should be understood that can be realized by computer program instructions every first-class in flowchart and/or the block diagram
The combination of flow and/or box in journey and/or box and flowchart and/or the block diagram.These computer programs can be provided
Instruct the processor of all-purpose computer, special purpose computer, Embedded Processor or other programmable data processing devices to produce
A raw machine so that the instruction executed by computer or the processor of other programmable data processing devices is generated for real
The device for the function of being specified in present one flow of flow chart or one box of multiple flows and/or block diagram or multiple boxes.
These computer program instructions, which may also be stored in, can guide computer or other programmable data processing devices with spy
Determine in the computer-readable memory that mode works so that instruction generation stored in the computer readable memory includes referring to
Enable the manufacture of device, the command device realize in one flow of flow chart or multiple flows and/or one box of block diagram or
The function of being specified in multiple boxes.
These computer program instructions also can be loaded onto a computer or other programmable data processing device so that count
Series of operation steps are executed on calculation machine or other programmable devices to generate computer implemented processing, in computer or
The instruction executed on other programmable devices is provided for realizing in one flow of flow chart or multiple flows and/or block diagram one
The step of function of being specified in a box or multiple boxes.
Obviously, various changes and modifications can be made to the invention without departing from essence of the invention by those skilled in the art
God and range.In this way, if these modifications and changes of the present invention belongs to the range of the claims in the present invention and its equivalent technologies
Within, then the present invention is also intended to include these modifications and variations.
Claims (8)
1. artificial intelligence writes Satellite TT and power coupled thermomechanics simulated program method, which is characterized in that including：
Description is formatted to Satellite TT subsystem design result；
It establishes source code and writes decision tree, the book of Satellite TT and power coupled thermomechanics emulation source code is determined according to the decision tree
Write rule and observing and controlling and power coupled thermomechanics computation rule；
It is complete according to Green Formula data, the rules for writing and the computation rule that the Satellite TT subsystem designs
The writing of pairs of Satellite TT and power coupled thermomechanics emulation source code.
2. the method as described in claim 1, which is characterized in that be formatted and retouch to Satellite TT subsystem design result
It states, including：
Component names, configuration information, communication link and the channel information for including to communication subsystem design result are formatted
Description；The data of Green Formula are saved in XML file and database.
3. method as claimed in claim 2, which is characterized in that the book of the Satellite TT and power coupled thermomechanics emulation source code
Rule is write, including：
Observing and controlling and power coupled thermomechanics emulation source code are divided into the related source code of dynamics environment and physical components model correlated source
Code；
By way of copying and being inserted into, the writing to dynamics environment correlation source code is completed；
The component names of communication subsystem, configuration information, communication link and channel are believed according to what XML file and database preserved
Breath completes the writing to physical components model correlation source code.
4. method as described in any one of claims 1-3, which is characterized in that the observing and controlling and power coupled thermomechanics computation rule,
Including：
The calculating that communication subsystem is coupled with control subsystem；
The calculating of communication subsystem and power supply subsystems couple；
The calculating of communication subsystem and thermal control subsystems couple.
5. artificial intelligence writes Satellite TT and power coupled thermomechanics simulated program device, which is characterized in that including：
Formatting module, for being formatted description to Satellite TT subsystem design result；
Determining module is established, decision tree is write for establishing source code, Satellite TT and power thermoelectricity is determined according to the decision tree
The rules for writing of coupling Simulation source code and observing and controlling and power coupled thermomechanics computation rule；
Module is write, Green Formula data, the rules for writing and institute for being designed according to the Satellite TT subsystem
Computation rule is stated, the writing for emulating source code to Satellite TT and power coupled thermomechanics is completed.
6. device as claimed in claim 5, which is characterized in that the formatting module, specifically for being set to communication subsystem
Component names, configuration information, communication link and the channel information that meter result includes are formatted description；By Green Formula
Data are saved in XML file and database.
7. device as claimed in claim 8, which is characterized in that described to establish determining module, determining Satellite TT and power heat
The rules for writing of emulation source code are electrically coupled, including：Observing and controlling and power coupled thermomechanics emulation source code are divided into dynamics environment phase
Close source code source code related to physical components model；By way of copying and being inserted into, complete to dynamics environment correlated source generation
The writing of code；According to XML file and database preserve to the component names of communication subsystem, configuration information, communication link and
Channel information completes the writing to physical components model correlation source code.
8. such as claim 5-7 any one of them devices, which is characterized in that the observing and controlling for establishing determining module determination and power
Coupled thermomechanics computation rule, including：The calculating that communication subsystem is coupled with control subsystem；Communication subsystem and power supply subsystem
The calculating of coupling；The calculating of communication subsystem and thermal control subsystems couple.
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