CN106709656A - System architecture-based avionics system technology state control method - Google Patents
System architecture-based avionics system technology state control method Download PDFInfo
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- CN106709656A CN106709656A CN201611237453.1A CN201611237453A CN106709656A CN 106709656 A CN106709656 A CN 106709656A CN 201611237453 A CN201611237453 A CN 201611237453A CN 106709656 A CN106709656 A CN 106709656A
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q10/00—Administration; Management
- G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
- G06Q10/063—Operations research, analysis or management
- G06Q10/0631—Resource planning, allocation, distributing or scheduling for enterprises or organisations
- G06Q10/06316—Sequencing of tasks or work
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
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- G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
- G06Q10/063—Operations research, analysis or management
- G06Q10/0639—Performance analysis of employees; Performance analysis of enterprise or organisation operations
- G06Q10/06395—Quality analysis or management
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Abstract
The invention belongs to the field of airborne avionics system technology state management, and relates to a system architecture-based avionics system technology state management method. The method involves four technology state information libraries including a system configuration information library, a design state information library, a product information library and an installation state information library, and five technology state management actives including configuration creation, fault dispatching-based design state management, product management and integration delivery. Through work in three aspects of (1) defining contents and formats of storage information of the technology state information library, (2) defining behavior boundaries and behavior guidelines of the technology state management activities, and (3) defining contents of interaction information between the management activities and the information library, the design state management, the product state management and the installation state management of an airborne avionics system are finished.
Description
Technical field
The present invention relates to the management of airborne avionics system state of the art.
Background technology
Existing airborne avionics system is complicated due to function, and part subsystem is generally all using the development mould of incremental development
Formula, so results in these subsystems and other subsystems closely related with it and there are multiple versions simultaneously.
Current existing means mainly include log book, change approval process and software configuration item management, and these are managed
Means all existing defects.
Log book circulates with equipment all the time, and designer cannot at any time obtain status information of equipment；Change approval process with
Software configuration item management lacks reference to function examination ＆ verification and associates easily appearance careless omission.
Inventive technique scheme
A kind of avionics system state of the art control method based on system architecture, it is characterised in that comprise the following steps：
1) system configuration information bank is set up：The arborescence of storage system framework, between descriptive system and its each composition
Relation；
2) design point information bank is set up：Storage system, subsystem/equipment each version technique state content；Adjacent version
The changing content of this technology state；A series of Evolvement of state of the art；Failure sends information；
3) product information storehouse is set up：Storage meets the hardware product information of agreement requirement and by checking by inspection
Software product information；
4) aircraft technology status information storehouse is set up：Deposit all aircrafts at present implement avionics system version, install it is hard
Part sequence number, filling software version number；
5) " configuration establishment " management activity is performed：System configuration is built according to avionics system/subsystem scheme, by system structure
Type is stored in step 1) in system configuration information bank；
6) system of avionics system certain state of the art, subsystem version are chosen and are stored in step 2 as base version) in set
Meter status information storehouse；
7) " being managed based on the design point that failure is sent " activity after breaking down, is performed, based on system configuration, therefore
Barrier is singly distributed as means, and failure is sent into specific subsystem/equipment or software configuration item；
8) repeat step 6), with fixing a breakdown, perfect in shape and function, system upgrade is all carried out on this base version, upgraded
State of the art afterwards is also stored in step 2) in design point information bank；
9) when the hardware of certain version, software product pay chief engineer's unit, perform " management of product activity "：According to exclusion event
The state of the art change and test report that barrier causes complete function and audit；Whether all the product for determining each component according to configuration
Whether storage, system mode is complete；Then from step 2) in design point information bank in read the technical requirements of the version, enter
The examination ＆ verification of row function judges whether product meets requirement；As fruit product is qualified, just product information typing product information storehouse, if produced
Product are unqualified just to be refused back；
10) when avionics system is installed, " integrated payment " management activity is performed, according to installation state of the art requirement from step 2)
In design point information bank in extract the supporting table of system version of the state, with when frontloader epidemic situation comparison, draw needs
The component list of upgrading, and from step 3) in product information storehouse take out the software and satisfactory hardware of this version, it is complete
, system integration test, integrated payment aircraft general assembly unit, and more new equipment log book and step 4 filling into software) in aircraft technology
Status information storehouse.
Brief description of the drawings
Fig. 1 is the schematic flow sheet of technical solution of the present invention.
Fig. 2 is the schematic diagram of the specific embodiment of the invention.
Specific embodiment：
The present invention is described in detail below, refers to accompanying drawing 2：
1) certain type machine avionics system configuration information storehouse A is set up：Avionics system is made up of component X, component Y components Z；
2) design point information bank B is set up：Current design state avionics system is 1.0 versions, and corresponding component X is 1.0
Version, component Y are 1.0 editions, and component Z is 1.0 editions；
3) product information storehouse C is set up：The current product for being delivered to chief engineer's unit is included：Component X, device numbering：160908,
Version：1.0；Component Y, numbering：160920, version：1.0；Component Z, numbering：160922, version：1.0；
4) aircraft technology status information storehouse D is set up：Current 001 frame machine installation state is avionics system version 1.0, wherein group
Part X, device numbering：150908, version：1.0；Component Y, numbering：150920, version：1.0；Component Z, numbering：150922, version
This：1.0；
5) a set of version is that 1.0 avionics system (is included：Component X, device numbering：170908, component Y, numbering：
170920, component Z, numbering：170922) when paying chief engineer's unit, according to the complement version information of A, each component resume is checked
This, whether the version for determining equipment 160908 is 1.0；Whether the version of component 160920 is 1.0；The version of component 160922 is
No is 1.0.If any Non-Compliance, refuse back；C is updated simultaneously；
6) after 001 frame machine avionics system breaks down, the system configuration in A is analyzed to failure, by failure quilt
It is dispatched to the component X that device numbering the is 150908 and component Z that device numbering is 150922；After failure is solved, component X, Z will be with
1.0 is base version, sends modified application, changes component, and to 1.1 editions, component B does not have failure for edition upgrading, and version is constant.Avionics system
The version of system also accordingly upgrades to 1.1 editions；
7) state of the art of the version of avionics system 1.1 is stored in B；
8) the component Z that the device numbering in C storehouses is 160908 component X and device numbering is 160922 upgrades to 1.1 editions
Afterwards, C storehouses also accordingly update；
9) the component Z that original equipment numbering is 150908 component X and device numbering is 150922 is upgrading to 1.1, failure
Exclude after installing again, D storehouses also accordingly update.
Claims (1)
1. a kind of avionics system state of the art control method based on system architecture, it is characterised in that comprise the following steps：
1) system configuration information bank is set up：The arborescence of storage system framework, the relation between descriptive system and its each composition；
2) design point information bank is set up：Storage system, subsystem/equipment each version technique state content；Adjacent version skill
The changing content of art state；A series of Evolvement of state of the art；Failure sends information；
3) product information storehouse is set up：Storage meets the hardware product information and the software by checking of agreement requirement by inspection
Product information；
4) aircraft technology status information storehouse is set up：Deposit the avionics system version that all aircrafts are implemented at present, the hardware sequence installed
Row number, filling software version number；
5) " configuration establishment " management activity is performed：System configuration is built according to avionics system/subsystem scheme, system configuration is deposited
Enter step 1) in system configuration information bank；
6) system of avionics system certain state of the art, subsystem version are chosen and are stored in step 2 as base version) in design shape
State information bank；
7) " being managed based on the design point that failure is sent " activity, based on system configuration, Trouble ticket after breaking down, are performed
Means are distributed as, failure is sent into specific subsystem/equipment or software configuration item；
8) repeat step 6), with fixing a breakdown, perfect in shape and function, system upgrade is all carried out on this base version, after upgrading
State of the art is also stored in step 2) in design point information bank；
9) when the hardware of certain version, software product pay chief engineer's unit, perform " management of product activity "：Draw according to fixing a breakdown
The state of the art change for rising and test report complete function examination ＆ verification；Whether the product for determining each component according to configuration has all entered
Whether storehouse, system mode is complete；Then from step 2) in design point information bank in read the technical requirements of the version, carry out
Function examination ＆ verification judges whether product meets requirement；As fruit product is qualified, just product information typing product information storehouse, such as fruit product
It is unqualified just to refuse back；
10) when avionics system is installed, " integrated payment " management activity is performed, according to installation state of the art requirement from step 2) in
The supporting table of system version of the state is extracted in design point information bank, upgrading is needed with when frontloader epidemic situation comparison, drawing
The component list, and from step 3) in product information storehouse take out the software and satisfactory hardware of this version, complete soft
Part is filling, system integration test, integrated payment aircraft general assembly unit, and more new equipment log book and step 4) in aircraft technology state
Information bank.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201611237453.1A CN106709656A (en) | 2016-12-28 | 2016-12-28 | System architecture-based avionics system technology state control method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201611237453.1A CN106709656A (en) | 2016-12-28 | 2016-12-28 | System architecture-based avionics system technology state control method |
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| CN106709656A true CN106709656A (en) | 2017-05-24 |
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| CN201611237453.1A Pending CN106709656A (en) | 2016-12-28 | 2016-12-28 | System architecture-based avionics system technology state control method |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108427681A (en) * | 2017-02-14 | 2018-08-21 | 北京国基科技股份有限公司 | Total quality management system |
| CN111190819A (en) * | 2019-12-25 | 2020-05-22 | 中国航空工业集团公司西安飞机设计研究所 | State control method for airborne software test project |
| CN113240231A (en) * | 2021-03-31 | 2021-08-10 | 成都飞机工业（集团）有限责任公司 | Finished product technical state management system |
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| CN102968298A (en) * | 2012-10-31 | 2013-03-13 | 山东浪潮齐鲁软件产业股份有限公司 | Software product construction method |
| US20130247025A1 (en) * | 2012-02-20 | 2013-09-19 | Airbus Operations Sas | Method and device for optimizing data updates in operationally approved software applications of aircraft |
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2016
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Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US20130247025A1 (en) * | 2012-02-20 | 2013-09-19 | Airbus Operations Sas | Method and device for optimizing data updates in operationally approved software applications of aircraft |
| CN102968298A (en) * | 2012-10-31 | 2013-03-13 | 山东浪潮齐鲁软件产业股份有限公司 | Software product construction method |
Non-Patent Citations (2)
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| 孙景华: "《ARJ21-700飞机研制项目的机载软件构型管理方案研究及应用》", 《中国优秀硕士学位论文全文数据库（电子期刊）》 * |
| 谭征华: "《关于机载软件加载的管理》", 《2016第五届民用飞机航电系统国际论坛论文集》 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108427681A (en) * | 2017-02-14 | 2018-08-21 | 北京国基科技股份有限公司 | Total quality management system |
| CN111190819A (en) * | 2019-12-25 | 2020-05-22 | 中国航空工业集团公司西安飞机设计研究所 | State control method for airborne software test project |
| CN111190819B (en) * | 2019-12-25 | 2023-05-23 | 中国航空工业集团公司西安飞机设计研究所 | State control method for airborne software test project |
| CN113240231A (en) * | 2021-03-31 | 2021-08-10 | 成都飞机工业（集团）有限责任公司 | Finished product technical state management system |
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Application publication date: 20170524 |