CN113869004A - Missile digital model identification coding method - Google Patents
Missile digital model identification coding method Download PDFInfo
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Abstract
The invention relates to a missile digital model identification coding method, and belongs to the field of industrial internet. The method comprises the following steps: s1: and (3) formulating a draft of missile identification analysis coding specification, and specifying terms and definitions of missile part industrial internet identification codes, coding structures and coding rules to code missile parts. S2: and building a plurality of servers, and storing different identification codes under corresponding prefix codes on databases of different servers to realize the storage of the identification codes at different levels.
Description
Technical Field
The invention belongs to the field of industrial internet, and relates to a missile digital model identification coding method.
Technical Field
The industrial internet represents the latest development direction of informatization of the manufacturing industry and is receiving more and more attention from the industrial and academic circles. The industrial internet firstly helps to improve the industrial production efficiency, promotes the popularization of intellectualization in the industrial industry, is beneficial to promoting the fusion of various industries and helps the upstream and downstream enterprises of an industrial chain to cooperatively develop, so that a plurality of production elements of industrial economy can be shared on a unified platform. The industrial internet identification analysis system is an important component of an industrial internet network and is an important infrastructure for establishing various information sharing platforms. The identification code is the core foundation for establishing an identification analysis system, and standardized coding is carried out on various production data through unified identification to form the foundation for realizing information sharing and promoting industrial intelligence. At present, the related research of identification analysis mainly focuses on civil manufacturing industry, but the research focuses on the related system construction research of aerospace.
Disclosure of Invention
In view of the above background, the present invention provides a missile digital model identification coding method, which includes the following steps:
s1: and (3) making a draft of identification, analysis and coding specifications of the missile digital model, and specifying terms and definitions of identification codes of missile digital model parts, coding structures and coding rules to code the missile digital model parts.
S2: and building a plurality of servers, and storing different identification codes under corresponding identification prefix codes on databases of different servers to realize storage of identification codes of different levels.
Optionally, the step S1 specifically includes the following steps:
s11: the identification code consists of two parts, namely an identification prefix and an identification postfix, wherein the identification prefix and the identification postfix are separated by '/'.
S12: the identification prefix is composed of a country code, an industry code and an enterprise code.
S13: the identification suffix is composed of a classification code, a model code, a lot number, a serial number, an extended data code, which is optional.
Optionally, the step S13 specifically includes the following steps:
s131: the classification code is composed of letters 'F' and two digits, and comprises the following composition structure of a missile digital model: the system comprises a whole body, guidance control, terminal guidance detection, a guidance system, pneumatics, power, a structure and electrics.
S132: the model code consists of the letter "M" and a 2-digit number.
S133: the batch number consists of the letter "P" and a 3 digit number.
S134: the serial number consists of the letters "X" and 5 digits.
S135: the extension data includes: the code of the model on the client side, the manufacturer code of the supplier on the client side, the self-defined code, the model establishing date and the model valid period.
Drawings
FIG. 1 shows the specific steps of a missile digital model identification coding method
Detailed Description
The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the present application, and it is obvious that the described embodiments are only illustrative and are not intended to limit the present application.
As shown in fig. 1, the invention provides a missile digital model identification coding method, which comprises the following steps:
s1: and (3) making a draft of identification, analysis and coding specifications of the missile digital model, and specifying terms and definitions of identification codes of missile digital model parts, coding structures and coding rules to code the missile digital model parts.
S2: and building a plurality of servers, and storing different identification codes under corresponding identification prefix codes on databases of different servers to realize storage of identification codes of different levels.
Optionally, the step S1 specifically includes the following steps:
s11: the identification code consists of two parts, namely an identification prefix and an identification postfix, wherein the identification prefix and the identification postfix are separated by '/'.
S12: the identification prefix is composed of a country code, an industry code and an enterprise code.
S13: the identification suffix is composed of a classification code, a model code, a lot number, a serial number, an extended data code, which is optional.
Optionally, the step S13 specifically includes the following steps:
s131: the classification code is composed of letters 'F' and two digits, and comprises the following composition structure of a missile digital model: the system comprises a whole body, guidance control, terminal guidance detection, a guidance system, pneumatics, power, a structure and electrics.
S132: the model code consists of the letter "M" and a 2-digit number.
S133: the batch number consists of the letter "P" and a 3 digit number.
S134: the serial number consists of the letters "X" and 5 digits.
S135: the extension data includes: the code of the model on the client side, the manufacturer code of the supplier on the client side, the self-defined code, the model establishing date and the model valid period.
Optionally, the step S131 specifically includes the following steps:
s1311: the general comprises: the system comprises a missile general arrangement model, a missile quality characteristic design model, a missile general performance characteristic analysis model, a missile general parameter prediction model, a missile non-control (with) particle trajectory model, a missile non-control (with) rigid body trajectory model, a missile guidance trajectory model, a missile general performance index model, a power coefficient calculation model, an initial dispersion calculation model, a missile theoretical kill zone calculation model and the like.
S1312: the guidance control includes: the system comprises a navigation system model, a guidance model, a stable control system model, a rudder system model, a projectile motion model, a measurement error model, a flight control logic model and the like.
S1313: the terminal guidance control includes: the system comprises a seeker mathematical model, an interference model, a binding parameter model related to the seeker, an A frame parameter model, a bullet channel data, a last guidance shift-changing error model in a weapon system, a seeker structure model and the like.
S1314: the war induction system comprises: the system comprises a general parameter model of the warfare induction system, a warfare cooperation model, a fuze model, a warhead model, a target vulnerability model, a warhead ground static explosion model, a safety execution mechanism model, a killing probability evaluation model, a warhead general performance model and the like.
S1315: the pneumatics includes: the system comprises a pneumatic layout and appearance model, a full-elasticity pneumatic force calculation model, a part pneumatic force calculation model, a pneumatic thermal calculation model, a pneumatic load calculation model, a pneumatic elasticity calculation model and the like.
S1316: the power comprises the following steps: the system comprises an engine overall parameter prediction model, a solid rocket engine internal trajectory analysis model, an engine internal flow field simulation analysis model, an engine flame characteristic analysis model and the like.
S1317: the structure includes: the missile system/subsystem three-dimensional structure model comprises a cabin section prototype, a full missile prototype and the like, a framework model, a missile structure model, a cable wiring model, equipment models, a missile structure static strength analysis model, a missile structure stability analysis model, a missile structure rigidity analysis model, a missile structure thermal strength analysis model, a structure thermal protection performance analysis model, a missile structure mechanical and thermal strength analysis model, a missile structure dynamic strength analysis model, a modal analysis model, a mechanism dynamics analysis model, a structure separation and impact response analysis model, a structure random vibration response analysis model, a wing/rudder surface (thermal) flutter characteristic analysis model, a missile structure fatigue, durability and reliability design analysis model, a missile virtual reality analysis model and the like.
S1318: the electric machine comprises: the device comprises an on-bomb battery structure three-dimensional model, an electric control device structure three-dimensional model, a secondary power supply structure three-dimensional model, an on-bomb cable net structure three-dimensional model, an electric connector three-dimensional model, an on-bomb equipment electric interface circuit model, an on-bomb battery electric performance model, an electric control device electric performance model, a secondary power supply electric performance model, an on-bomb cable net electric performance model and the like.
The missile digital model identification coding method provided by the invention can be used for carrying out standardized coding on the missile digital model through unified identification, realizing information sharing and further promoting industrial intellectualization.
Claims (3)
1. A missile digital model identification coding method is characterized by comprising the following steps: the method comprises the following steps:
s1: and (3) making a draft of identification, analysis and coding specifications of the missile digital model, and specifying terms and definitions of identification codes of missile digital model parts, coding structures and coding rules to code the missile digital model parts.
S2: and building a plurality of servers, and storing different identification codes under corresponding identification prefix codes on databases of different servers to realize storage of identification codes of different levels.
2. The missile digital model identification coding method of claim 1, wherein the missile digital model identification coding method comprises the following steps: the step S1 specifically includes the following steps:
s11: the identification code consists of two parts, namely an identification prefix and an identification postfix, wherein the identification prefix and the identification postfix are separated by '/'.
S12: the identification prefix is composed of a country code, an industry code and an enterprise code.
S13: the identification suffix is composed of a classification code, a model code, a lot number, a serial number, an extended data code, which is optional.
3. The missile digital model identification coding method of claim 2, wherein the missile digital model identification coding method comprises the following steps: the step S13 specifically includes:
s131: the classification code consists of letters 'F' and 4 digits, and comprises the following composition structure of a missile digital model: the system comprises a whole body, guidance control, terminal guidance detection, a guidance system, pneumatics, power, a structure and electrics.
S132: the model code consists of the letter "M" and an indefinite-length arabic numeral.
S133: the batch number consists of the letter "P" and an indefinite number of arabic numerals.
S134: the serial number consists of the letter "X" and an Arabic number of indefinite length.
S135: the extension data includes: the code of the model on the client side, the manufacturer code of the supplier on the client side, the self-defined code, the model establishing date and the model valid period.
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| CN202111005213.XA CN113869004A (en) | 2021-08-30 | 2021-08-30 | Missile digital model identification coding method |
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Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070162412A1 (en) * | 2003-03-03 | 2007-07-12 | Richard Percy | System and method using alphanumeric codes for the identification, description, classification and encoding of information |
| CN112215321A (en) * | 2020-10-12 | 2021-01-12 | 四川长虹电器股份有限公司 | Identification coding method |
| CN112653774A (en) * | 2020-12-16 | 2021-04-13 | 北京航天智造科技发展有限公司 | Industrial internet identification coding method and device |
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- 2021-08-30 CN CN202111005213.XA patent/CN113869004A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070162412A1 (en) * | 2003-03-03 | 2007-07-12 | Richard Percy | System and method using alphanumeric codes for the identification, description, classification and encoding of information |
| CN112215321A (en) * | 2020-10-12 | 2021-01-12 | 四川长虹电器股份有限公司 | Identification coding method |
| CN112653774A (en) * | 2020-12-16 | 2021-04-13 | 北京航天智造科技发展有限公司 | Industrial internet identification coding method and device |
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