CN106656961A - Flight data decoding analysis method based on ARINC767 specification - Google Patents
Flight data decoding analysis method based on ARINC767 specification Download PDFInfo
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- CN106656961A CN106656961A CN201610864268.9A CN201610864268A CN106656961A CN 106656961 A CN106656961 A CN 106656961A CN 201610864268 A CN201610864268 A CN 201610864268A CN 106656961 A CN106656961 A CN 106656961A
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L69/00—Network arrangements, protocols or services independent of the application payload and not provided for in the other groups of this subclass
- H04L69/03—Protocol definition or specification
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L69/00—Network arrangements, protocols or services independent of the application payload and not provided for in the other groups of this subclass
- H04L69/26—Special purpose or proprietary protocols or architectures
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L2012/40267—Bus for use in transportation systems
- H04L2012/4028—Bus for use in transportation systems the transportation system being an aircraft
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Abstract
The invention discloses a flight data decoding analysis method based on the ARINC767 specification. According to the data record characteristics of the ARINC767 specification, an appropriate decoding library is matched for flight data to complete decoding. Users do not need to have an in-depth understanding of the structure of data and the type of a decoding library. The decoding analysis method of the invention will continue trying until the completion of decoding. After trial decoding succeeds, the current configuration will be updated to backend default configuration. For the processing of a large amount of homogenous data, a lot of trial decoding time and manual configuration time can be saved.
Description
Technical field
The present invention relates to technical field of aerospace, and in particular to a kind of flying quality decoding analysis based on ARINC767 specifications
Method.
Background technology
Traditional flight data recording specification ARINC573/ARINC717/ARINC747, based on subframe, each
Subframe is one second, and 4 subframes constitute a frame, and word groove is 12 data bit.New 787 aircraft, has abandoned completely subframe, word
The concepts such as groove, super frame, introduce a kind of new data record specification ARINC767.On the basis of parameter acquisition frequency, will join
Number packet, the packet is referred to as " frame (Frame) ", and the synchronization character of frame is EB90, and the parameter in each frame is same collection speed
Rate, and journal, without the concept of word groove.One frame is also no longer one second, and is the introduction of " timestamp " (time
Stamp concept), to the order and the record time that judge each frame.
Traditional decoding software can not support the decoding of the data of ARINC767 specifications, need to set up a kind of new calculation
Method, with the perfect decoding for adapting to new types of data.
The content of the invention
For the deficiencies in the prior art, it is an object of the invention to provide a kind of flying quality based on ARINC767 specifications
Decoding analysis method, to adapt to based on the flying quality of ARINC767 specifications.
To achieve these goals, the present invention is adopted the technical scheme that：
A kind of flying quality based on ARINC767 specifications decodes analysis method, including step：
Obtain based on the flying quality of ARINC767 specifications；
The synchronization character of flying quality is searched, the frame ID after synchronization character is extracted；
Aircraft number is parsed according to the filename of flying quality, the supplemental characteristic of initial configuration corresponding with aircraft number is called
Storehouse；
The length of all length characteristics of frame ID of flying quality frame ID corresponding with the parameter database of initial configuration is special
Levy and compare, row decoding is entered to flying quality according to the parameter database of initial configuration if consistent, change one by one if inconsistent
The parameter database of other versions, until the length characteristic of all frame ID of flying quality frame ID corresponding with parameter current database
Length characteristic it is consistent, replace the parameter database of initial configuration with parameter current database, and according to parameter current database
Row decoding is entered to flying quality；
According to the various parameters for decoding out, carry out leg and divide and airport matching.
Compared with prior art, the beneficial effects of the present invention is：
At present when row decoding is entered, the mistake that any point is arranged can all cause the failure for decoding to the decoding software of main flow,
The change of aircraft configuration also results in data decoding and cannot carry out.User needs the configuration current to decoding principle and aircraft to have
Careful understanding, can just complete the setting to backstage, and this needs to carry out substantial amounts of training to user of service in certain degree,
Increase use cost.The present invention, according to the data record feature of ARINC767 specifications, is the suitable decoding storehouse of flying quality matching,
Complete decoding.User to data structure and decoding storehouse type without the need for carrying out deep understanding, the decoding analysis method meeting of the present invention
Constantly try to, till decoding is finished.After trial and error decoding success, can be by current config update backstage preset configuration, at place
When managing a large amount of isomorphism type data, substantial amounts of trial and error decoding time and human configuration time can be saved.
Description of the drawings
Fig. 1 is the schematic flow sheet that flying quality of the present invention based on ARINC767 specifications decodes analysis method.
Specific embodiment
With reference to specific embodiment, the present invention is further illustrated.
The purpose of decoding is, by binary flight data file, to be converted into discernible engineering value.Due to being based on
The flying quality of ARINC767 specifications is entirely different with traditional, thus the algorithm of decoding also difference is very big.
Flying quality decoding analysis method of the present invention based on ARINC767 specifications, as shown in figure 1, including step：
The flying quality of step s101, acquisition based on ARINC767 specifications.
Flying quality, refers to the flying quality downloaded from airplane data record system, and its form is binary file.For
787 aircrafts, flying quality has 3 classes, and a class is by safeguarding EAFR (the Enhanced Airborne that notebook ML is downloaded
Flight Recorder) data, a class is to be synchronized to LSAPL (Loadable Software Airplane Part
Librarian can load aircraft software components library) CPL (Continuous Parameter Logging) data on server,
Another kind of is the CPL data by TCU (Terminal Cellular Unit) using wireless network transmissions to ground-based server.
This three classes data can read in calculator memory by automatic or manual mode.
Step s102, the synchronization character for searching flying quality, extract the frame ID after synchronization character.
EB90 synchronization characters are found, and validity check is done to frame ID and frame length after synchronization character etc., take out the time of frame
Stamp TimeStamp.
Step s103, aircraft number is parsed according to the filename of flying quality, call initial configuration corresponding with aircraft number
Parameter database.
Flying quality, due to the normalization that it is named, can parse some very important information from filename, like flying
Machine number, data download time etc., in order to follow-up data processing.
It is step s104, all length characteristics of frame ID of flying quality and length in the parameter database of initial configuration is special
Levy and compare, row decoding is entered to flying quality according to the parameter database of initial configuration if consistent, call if inconsistent adaptive
The trial and error decoding subalgorithm answered.
Because the aircraft factory chamber of commerce irregularly updates the database software about log, for decoding ginseng
Number database also has corresponding multiple versions, and the purpose of trial and error decoding subalgorithm is to call all default parameter databases successively
Enter row decoding, until finding the database of matching till.Specifically, when the length characteristic of all frame ID of flying quality with initially match somebody with somebody
When length characteristic in the parameter database put is inconsistent, the parameter database of other versions is changed one by one, until flying quality
The length characteristic of all frame ID is consistent with the length characteristic in parameter current database, is replaced with parameter current database and is initially matched somebody with somebody
The parameter database put, and the parameter that included according to frame ID and the length shared by parameter, are entered successively using parameter database
Row decoding, by binary flying quality engineering value is converted to.Alarm is ejected if all parameter databases all attempt failure
Information.
Step s105, according to the various parameters for decoding out, carry out leg divide and airport matching.
Because original flying quality is all continuous recording, all of leg all blends together, and forms one continuously
Binary file.One of purpose of decoding is exactly that Partial key parameter is decoded in advance, such as vacant lot electric switch, UTC, fuel oil
Flow, pressure altitude, radio altitude, ground velocity etc., according to the change of these parameters, binary file are divided into complete one by one
Whole leg file.The division of leg is also always a difficult point during decoding.The unexpected disappearance of such as data record, touches
Go around, this training etc. all can to leg divide interfere, affect divide accuracy.The introducing of novelty of the present invention
Privilege level concept, after the data analyses for combining a large amount of true legs, the perfect leg of a kind of comparison for drawing divides solution
Certainly scheme.
After vacant lot electric switch is detected by ground is switched in the air, activation leg partitioning algorithm monitoring is carried out according to priority
Leg divides.
Limit priority：If radio altitude is changed into 0, ground velocity is 0, after the fuel flow of two is also changed into 0, monitoring
The change of UTC time, if there is breakpoint, then whole machine power-off after explanation boat, aircraft no longer record data, now to leg
Carry out that cutting is ideal, the purpose of leg cutting is the separation of the previous leg and latter leg for finding optimum.
Two grades of priority：If the first situation is not present, such as miss the stop flight, miss the stop during will not power-off, this
When press the second priority, monitor fuel flow to carry out cutting after 0.
Three-level priority：If this training, aircraft is repeated landing training, then second situation also will not be deposited
Leg cutting is now being carried out before take off next time.
Special priority：There are the data that some are special, for some reason, flying quality loss, such as certain segment data are just
Journey, unexpected data outage, the data that next second has directly been arrived before another leg is taken off are flown over flat.Such case just should be supervised
Discontinuous point and height and fuel flow during control, by abnormal special priority, carry out leg cutting near breakpoint.
The advantage of above-mentioned leg partitioning algorithm：Adapt to almost all of leg data to divide, and all the time with optimum side
Formula carries out cutting, can shield interference of the special circumstances such as loss of data to algorithm, accurately divides leg.
The parameter of flight data recording does not have take-off and landing airport, only longitude and latitude parameter.Therefore, when data analysis is arrived
When takeoff point and landing point, need according to longitude and latitude, immediate airport name is matched in default Global Airports database.Together
When airport is matched, often there is the situation of matching error, such as the airport in Seattle airport and Boeing base to class software in Jing, both
It is spaced closely together, if algorithm not enough optimizes, it is easy to matching error.The present invention adopts Allowance Design, and reserved tolerance interface,
User can directly change.
By interface function, obtain user and tolerance is set；
Default airport database is traveled through, according to longitude and latitude tolerance, most possible airport list is filtered out；
Difference of longitude and latitudinal difference are calculated respectively, take the minimum airport of comprehensive deviation as final matching airport.
The advantage of above-mentioned algorithm is that user can pass through reserved interface, adjust tolerance, can correct the knot of decoding
Really.Because the airplane inertial longitude and latitude that calculates of navigation, can have certain deviation, if pilot is not carried out to inertial navigation in time
Correction, cumulative errors can be increasing, is finally possible to airport matching error.And the tolerance of this algorithm, it is allowed to user is carried out
Amendment.
Fly into nearly vertical section, be a new proposition, in conventional domestic and international decoding system, do not referred to and reality
It is existing.The present invention is projected in each location point near procedure that flies on the vertical guide Chong Die with runway centerline, Ran Houhui
What LOC guidance stations processed and GS guidance stations intersected most preferably enters near line.The realization of this kind of algorithm, greatly improves the effect of data analysis
Rate and the degree of accuracy, have intuitively reproduced flying scene very much.
Algorithm details：
The distance into nearly runway head to blind landing platform is obtained from relevant approach, enters the longitude and latitude of near-end runway head, run when entering near
The pressure altitude in road, when VOR (VHF OMNI-DIRECTIONAL RANGE VHF Omnidirection ranges) enters near each obstacle detouring point away from
From and height etc. information；
Origin with Approach End of Runway entrance as reference axis, X-axis be plane distance runway head enter the floor projection of near-end away from
From Y-axis is height of the aircraft relative to runway；
If ILS (Instrument landing system instrument-landing-systems) enters closely, the transmitting of blind landing platform is drawn
3 degree or 5 degree are entered near line, and by airport, actual data of announcing are defined；
If NDB (Non-Directional Beacon Non Direction Beasons) enters closely, each obstacle detouring point and its height are drawn；
The distance of current aircraft longitude and latitude and runway threshold longitude and latitude is calculated, is painted with reference to the height of the relative airport plane of aircraft
Aircraft profile line processed.
Aircraft enters the drafting of nearly vertical section, intuitively presents very much aircraft location, and aircraft altitude is near with entering
Relative position of line etc., can be data analysis, and FOQA saves the substantial amounts of time.
After all decoding terminates, will preserve in decoding information and early warning information write background data base, preserve necessary day
Will, backup significant data etc..
The following aspects is included to the improvement of business after above-mentioned algorithm realization：
1st, the complexity in user's use is alleviated
During data decoding, user need not know the corresponding parameter database of frame format of current original flying quality, this
It is bright to attempt various parameters database automatic code translation, and the parameter library of current trial and success can be preserved, can be straight when decoding next time
Connect and call.This mode can reduce the complexity that software is used, and reduce software and use the training time.
2nd, algorithm is increased income, and user's customization degree is high
User can write analysis and patrol to data analysis logic of propositions, parameter database secondary development according to the demand of oneself
Volume, event-monitoring and super-limit prewarning, improve data user rate.Data can be provided for aircraft maintenance and flight quality to support, in time
The each system of early warning transfinites, troubleshooting in advance, reduces aircraft and stops field time.
3rd, data analysis process is simplified
Parameter engineering value after decoding shows that in friendly way support diagram curve mode shows, is easy to user directly perceived
Judgement Parameter Variation.Support for flying quality to import Online Map simultaneously, draw complete leg flight path, draw
Flight vertical section when aircraft is left the theatre or marched into the arena, user can effectively judge the problem for existing of flying, and save analysis time,
Simplified analysis process.
4th, use cost is saved
Existing decoding system, after aircraft configuration change or Airborne Software update, original decoding data storehouse is no longer fitted
With, even trickle variation, is required for purchasing new decoding storehouse again, the substantial amounts of fund of consuming.The present invention can support to use
Family is self-defined to be created modification or directly producer's file is converted into into new decoding storehouse, greatly shortens renewal and solve problem
Cycle, saved the cost for using.
Above-listed detailed description is illustrating for possible embodiments of the present invention, and the embodiment simultaneously is not used to limit this
Bright the scope of the claims, all equivalence enforcements or change without departing from carried out by the present invention, in being intended to be limited solely by the scope of the claims of this case.
Claims (5)
1. a kind of flying quality based on ARINC767 specifications decodes analysis method, it is characterised in that including step：
Obtain based on the flying quality of ARINC767 specifications；
The synchronization character of flying quality is searched, the frame ID after synchronization character is extracted；
Aircraft number is parsed according to the filename of flying quality, the parameter database of initial configuration corresponding with aircraft number is called；
By the length characteristic ratio of all length characteristics of frame ID of flying quality frame ID corresponding with the parameter database of initial configuration
Compared with, row decoding is entered to flying quality according to the parameter database of initial configuration if consistent, other are changed one by one if inconsistent
The parameter database of version, until the length of the length characteristic of all frame ID of flying quality frame ID corresponding with parameter current database
Degree feature is consistent, and with parameter current database the parameter database of initial configuration is replaced, and according to parameter current database to flying
Row data enter row decoding；
According to the various parameters for decoding out, carry out leg and divide and airport matching.
2. the flying quality based on ARINC767 specifications according to claim 1 decodes analysis method, it is characterised in that institute
Stating the step of leg divides includes：
The various parameters that monitoring is decoded out, after vacant lot electric switch by ground is switched in the air, according to following priority to flying quality
Carry out leg division：
Limit priority：When radio altitude is 0, ground velocity is 0, and the fuel flow of all engines is 0, and UTC time occurs
During breakpoint, cutting is carried out to leg；
Two grades of priority：Fuel flow carries out cutting when being 0 to leg；
Three-level priority：Leg cutting is carried out before taking off next time；
Special priority：When flying quality interrupts, in UTC time breakpoint leg cutting is carried out.
3. the flying quality based on ARINC767 specifications according to claim 2 decodes analysis method, it is characterised in that institute
Stating the step of airport matches includes：
The longitude and latitude of takeoff point or landing point is extracted from the parameter for decoding out；
By interface function, the longitude and latitude tolerance of the airport matching that user is arranged is obtained；
Default airport longitude and latitude database is traveled through, is filtered out with the longitude and latitude deviation of takeoff point or landing point in longitude and latitude tolerance
In the range of airport list；
Difference of longitude and latitudinal difference are calculated respectively, take the minimum airport of comprehensive deviation as final matching airport.
4. the flying quality based on ARINC767 specifications according to claim 1 or 2 or 3 decodes analysis method, its feature
It is that the drafting flown into nearly vertical section is also carried out after decoding, step includes：
Obtain runway head enter near-end to the distance of blind landing platform, runway head enter the longitude and latitude of near-end, enter near when runway pressure altitude,
And the distance and height of VOR each obstacle detouring points when entering near；
Origin with Approach End of Runway entrance as reference axis, X-axis enters the floor projection distance of near-end, Y for plane distance runway head
Axle is height of the aircraft relative to runway；
If ILS enters closely, that draws the transmitting of blind landing platform enters near line；
If NDB enters closely, each obstacle detouring point and its height are drawn in a coordinate system；
Calculate the current longitude and latitude of aircraft and enter the distance of near-end longitude and latitude with runway head, paint with reference to the height of the relative airport plane of aircraft
Aircraft processed enters nearly vertical section line.
5. the flying quality based on ARINC767 specifications according to claim 1 or 2 or 3 decodes analysis method, its feature
It is, also including step：
In seconds, by the frame after decoding according to timestamp ordering.
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108016610A (en) * | 2017-12-13 | 2018-05-11 | 任红叶 | A kind of aircraft and method of work with buffer structure |
| CN110782549A (en) * | 2019-09-06 | 2020-02-11 | 中国商用飞机有限责任公司 | ARINC767 specification-based flight recorder data decoding method and system |
| CN110990470A (en) * | 2019-11-19 | 2020-04-10 | 深圳市比一比网络科技有限公司 | QAR data decoding method, system and storage medium based on distributed computation |
| CN114884928A (en) * | 2022-04-18 | 2022-08-09 | 中国民航科学技术研究院 | EAFR data downloading processing method and system of in-process computer type C919 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7039509B2 (en) * | 2002-12-30 | 2006-05-02 | Lucent Technologies Inc. | Wireless supplement and/or substitute for aircraft flight recorders |
| CN102075290A (en) * | 2010-12-23 | 2011-05-25 | 西北工业大学 | Aerial bus data coding and decoding methods |
| US8005581B2 (en) * | 2007-09-28 | 2011-08-23 | United Technologies Corp. | Systems and methods for communicating aircraft data |
| CN103577154A (en) * | 2012-07-26 | 2014-02-12 | 中国航空工业集团公司第六三一研究所 | ARINC 659 protocol based instruction decoding method |
| CN104331278A (en) * | 2014-10-15 | 2015-02-04 | 南京航空航天大学 | Instruction filtering method and device for specifications of ARINC661 |
-
2016
- 2016-09-29 CN CN201610864268.9A patent/CN106656961B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7039509B2 (en) * | 2002-12-30 | 2006-05-02 | Lucent Technologies Inc. | Wireless supplement and/or substitute for aircraft flight recorders |
| US8005581B2 (en) * | 2007-09-28 | 2011-08-23 | United Technologies Corp. | Systems and methods for communicating aircraft data |
| CN102075290A (en) * | 2010-12-23 | 2011-05-25 | 西北工业大学 | Aerial bus data coding and decoding methods |
| CN103577154A (en) * | 2012-07-26 | 2014-02-12 | 中国航空工业集团公司第六三一研究所 | ARINC 659 protocol based instruction decoding method |
| CN104331278A (en) * | 2014-10-15 | 2015-02-04 | 南京航空航天大学 | Instruction filtering method and device for specifications of ARINC661 |
Non-Patent Citations (2)
| Title |
|---|
| 程科: ""飞机操纵系统状态监测与故障预测方法研究"", 《中国优秀硕士学位论文全文数据库-工程科技Ⅱ辑》 * |
| 袁剑: ""一种基于ARINC767的飞行记录系统概述"", 《硅谷》 * |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108016610A (en) * | 2017-12-13 | 2018-05-11 | 任红叶 | A kind of aircraft and method of work with buffer structure |
| CN108016610B (en) * | 2017-12-13 | 2020-12-29 | 浙江黎盛新材料科技有限公司 | Aircraft with buffer structure and working method |
| CN110782549A (en) * | 2019-09-06 | 2020-02-11 | 中国商用飞机有限责任公司 | ARINC767 specification-based flight recorder data decoding method and system |
| CN110782549B (en) * | 2019-09-06 | 2022-03-22 | 中国商用飞机有限责任公司 | ARINC767 specification-based flight recorder data decoding method and system |
| CN110990470A (en) * | 2019-11-19 | 2020-04-10 | 深圳市比一比网络科技有限公司 | QAR data decoding method, system and storage medium based on distributed computation |
| CN114884928A (en) * | 2022-04-18 | 2022-08-09 | 中国民航科学技术研究院 | EAFR data downloading processing method and system of in-process computer type C919 |
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