CN107370537B - A kind of detection method of Fibre-optical Pilot Protection - Google Patents

A kind of detection method of Fibre-optical Pilot Protection Download PDF

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Publication number
CN107370537B
CN107370537B CN201710474063.4A CN201710474063A CN107370537B CN 107370537 B CN107370537 B CN 107370537B CN 201710474063 A CN201710474063 A CN 201710474063A CN 107370537 B CN107370537 B CN 107370537B
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channel
information
protective device
program
value
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CN107370537A (en
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朱建红
陈亮
石文国
饶剑波
李明
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Integrated Software Co Ltd
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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B10/00Transmission systems employing electromagnetic waves other than radio-waves, e.g. infrared, visible or ultraviolet light, or employing corpuscular radiation, e.g. quantum communication
    • H04B10/07Arrangements for monitoring or testing transmission systems; Arrangements for fault measurement of transmission systems
    • H04B10/075Arrangements for monitoring or testing transmission systems; Arrangements for fault measurement of transmission systems using an in-service signal
    • H04B10/079Arrangements for monitoring or testing transmission systems; Arrangements for fault measurement of transmission systems using an in-service signal using measurements of the data signal
    • H04B10/0793Network aspects, e.g. central monitoring of transmission parameters
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B10/00Transmission systems employing electromagnetic waves other than radio-waves, e.g. infrared, visible or ultraviolet light, or employing corpuscular radiation, e.g. quantum communication
    • H04B10/03Arrangements for fault recovery
    • H04B10/032Arrangements for fault recovery using working and protection systems
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B10/00Transmission systems employing electromagnetic waves other than radio-waves, e.g. infrared, visible or ultraviolet light, or employing corpuscular radiation, e.g. quantum communication
    • H04B10/07Arrangements for monitoring or testing transmission systems; Arrangements for fault measurement of transmission systems
    • H04B10/075Arrangements for monitoring or testing transmission systems; Arrangements for fault measurement of transmission systems using an in-service signal
    • H04B10/079Arrangements for monitoring or testing transmission systems; Arrangements for fault measurement of transmission systems using an in-service signal using measurements of the data signal
    • H04B10/0795Performance monitoring; Measurement of transmission parameters
    • H04B10/07953Monitoring or measuring OSNR, BER or Q
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L1/00Arrangements for detecting or preventing errors in the information received
    • H04L1/004Arrangements for detecting or preventing errors in the information received by using forward error control
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L1/00Arrangements for detecting or preventing errors in the information received
    • H04L1/004Arrangements for detecting or preventing errors in the information received by using forward error control
    • H04L1/0056Systems characterized by the type of code used
    • H04L1/0061Error detection codes
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L1/00Arrangements for detecting or preventing errors in the information received
    • H04L1/0078Avoidance of errors by organising the transmitted data in a format specifically designed to deal with errors, e.g. location
    • H04L1/0083Formatting with frames or packets; Protocol or part of protocol for error control

Abstract

The invention discloses a kind of detection method of Fibre-optical Pilot Protection, from sender and recipient together with complete, the two respectively detects Fibre-optical Pilot Protection in physical layer, data link layer, application layer.The present invention has preferable detection completeness, and classification considers all kinds of channel failures, good with existing design specification compliance;Entire scheme realizes the unique identification in channel, solves the problems, such as that principal and subordinate channel cannot be distinguished in existing scheme under the premise of no increase user's definite value;The detection scheme can be automatically performed the verification of two sides protective device program version, it is ensured that the consistency of two sides program version eliminates operation risk existing for artificial check and correction version;Information coding is high-efficient, and an information word contains gap marker, 2 category information of program version simultaneously, only increases the transmission quantity of 2 bytes, the influence to protective program is minimum.

Description

A kind of detection method of Fibre-optical Pilot Protection
Technical field
The present invention relates to relay protection detection field, especially a kind of detection method of Fibre-optical Pilot Protection.
Background technique
On high pressure, extra high voltage network, the optical fiber pilot protection of duplicate system retrofit is widely used.Optical fiber pilot protection It is to judge fault type by comparing the characteristic quantity of two sides information by the information of optical-fibre channel exchange two sides route protection (troubles inside the sample space, external area error), to decide whether to cut off protected circuit.As the carrier of protection information, optical fiber indulges UNPROFOR Shield channel plays huge effect in the whole series protection, and the quality of optical-fibre channel directly affects the action behavior of protective device. Common Fibre-optical Pilot Protection abnormal conditions have channel interrupt, channel from ring, channel intersection, data packetloss, channel step-out Deng.Detect channel abnormal fast and reliablely, to start corresponding counter-measure as early as possible, this for enhance electric system peace Full stable operation has great realistic meaning.
Currently, the monitoring for Fibre-optical Pilot Protection is usually realized by protective device, basic principle are as follows: Protective device passes through real-time detection optical-fibre channel physical layer parameter (such as light sends out power, light receives power), link layer parameter (such as channel The bit error rate), application layer message (such as two sides channel recognition code), when above-mentioned parameter be unsatisfactory for setting definite value threshold when, device It alerts and is latched pilot protection.Above-mentioned way is able to detect most of channel abnormal, but for following problems there has been no than More perfect solution: (1) the interconnection detection in principal and subordinate channel;(2) consistency detection of two sides protective program version.
About problem (1), common channel interconnection situation has: the interconnection (such as Fig. 1) of adjacent lines, double loop The interconnection (such as Fig. 2) on road, the interconnection (such as Fig. 3) in principal and subordinate channel.In above-mentioned figure, correct connection side a) is indicated Formula, b) indicate wrong connection type.For channel interconnection, general way are as follows: in protective device definite value, respectively This side, contralateral approach set a unique identification code, judge channel by the information of identification code of real-time detection transceiver channel Whether intersect.This scheme can be sentenced schemes single channel cross faults shown in (1), figure (2) out;But scheme principal and subordinate channel shown in (3) Identification code is identical, because channel recognition code is configured by protective device, the corresponding identification code of a device, and the master of a device An identification code is shared from channel, therefore principal and subordinate channel cross faults out can not be sentenced.Due to principal and subordinate channel cross faults concealment pole By force, very big workload is increased to service personnel.
About problem (2), conventional way is that the consistency of two sides protective program version is confirmed by operations staff.It is this by There are operation risk, scene a lot of because of operation caused by protective program version in two sides is inconsistent the way of manual intervention occurred Accident.
Therefore, it is necessary to existing Fibre-optical Pilot Protection detection scheme be improved, to facilitate the day of optical fiber pilot protection Chang Yunwei, field failure maintenance.
Summary of the invention
Technical problem to be solved by the present invention lies in, a kind of detection method of Fibre-optical Pilot Protection is provided, it can It solves the problems, such as that existing scheme can not detect principal and subordinate channel intersection, eliminates the operation wind that manual confirmation program version may cause Danger.
In order to solve the above technical problems, the present invention provides a kind of detection method of Fibre-optical Pilot Protection, including as follows Step:
(1) sender and recipient respectively correspond two sides protective device, this side protective device is using CRC-16 algorithm to dress It sets application program and carries out sum check, generate 16 program ver-ify information;
(2) according to this wing passage identification code definite value in protective device, 16 identification codes for representing this wing passage are generated;
(3) unique 32 bit port letter is generated in conjunction with program ver-ify information and this wing passage identification code according to channel type Cease word;
(4) it sends information word and detection light sends out power, light sends out power real-time display in the case where device monitors menu;
(5) opposite side protective device judges whether received optical power meets the requirements, when optical fiber transport channel interruption or channel decline When consuming exceeded, opposite side protective device report " channel interrupt " or " communication channel delay is excessive " is latched pilot protection at this time;When light-receiving function Rate in the normal range when, starting in next step detect;
(6) opposite side protective device judges communication bit error rates and effectiveness of information: when reception information frame number and sending information frame It when number difference is more than setting threshold or mismatches for information checking code continuous 5 times, is judged to " channel step-out ", is latched vertical UNPROFOR Shield;When above situation is unsatisfactory for, it is normal to be judged to data link layer, and starting detects in next step;
(7) opposite side protective device parses the information word received, extracts contralateral approach identification code, opposite side program version respectively This information;
(8) opposite side protective device judges whether contralateral approach identification code is fixed with " the contralateral approach identification code " in protective device Value matching;When channel intersects from ring or single channel, above-mentioned 2 identification codes are mismatched;When channel is normal, above-mentioned identification code Match, starting detects in next step;When channel is normal, above-mentioned identification code matching, starting detects in next step;
(9) judge whether opposite side program version and this side program version are consistent, wherein this side program version check information has been It is calculated via step (1);When two sides check information is inconsistent, it is inconsistent to be judged to two sides program, is latched pilot protection;Instead It, it is consistent to be judged to program version, open pilot protection.
Preferably, in step (1), CRC-16 algorithm specifically comprises the following steps: to read this side protective device program curing, It is deposited in an array, the byte number ProgSize of logging program, according to generator polynomial g (x)=x16+x12+x2+1 The generation of CRC code is carried out to the byte in the array one by one;In order to improve the formation speed of CRC code, at look-up table Reason, concrete processing procedure are as follows: (1) preset one 16 crc values, initial value 0x0;(2) n-th in array is extracted The value range of byte, N is 1~ProgSize, the least-significant byte exclusive or of the byte and CRC is obtained an index value, and according to this Index value finds corresponding crc value in CRC-16 table;(3) most-significant byte for retaining step (2) value is constant, by its least-significant byte and initial value Most-significant byte exclusive or as new least-significant byte value, combine most-significant byte, least-significant byte obtains a 16 new place values, and executes N=N+1;Weight The verification of process (2), (3) up to completing all procedure bytes is executed again, may finally obtain the CRC check value of this side program.
Preferably, in step (3), channel information word is generated using following rule: under single, information word is high by 16 Position is this wing passage identification code, and low 16 are this side program ver-ify code;Under principal and subordinate's channel pattern, main channel information word is 16 high For this wing passage identification code, low 16 are this side program ver-ify code, be high 16 from channel information word are this wing passage identification code, Low 16 radix-minus-one complements for this side program ver-ify code.
Preferably, in step (9), when complement code characteristic each other occurs in two sides check information, illustrate principal and subordinate channel occurred Cross-connect faults, it is consistent that this also demonstrates two sides program version simultaneously.
Preferably, step (4) and step (5) are carried out in physical layer;Step (6) is carried out in data link layer;Other steps All carried out in application layer.
The invention has the benefit that have preferable detection completeness, classification consider physical layer, data link layer, All kinds of channel failures of application layer are good with existing design specification compliance;Entire scheme is in no premise for increasing user's definite value Under, the unique identification in channel is realized, solves the problems, such as that principal and subordinate channel cannot be distinguished in existing scheme;The detection scheme can be with It is automatically performed the verification of two sides protective device program version, it is ensured that the consistency of two sides program version eliminates artificial check and correction version Operation risk existing for this;Information coding is high-efficient, and an information word contains gap marker, 2 category information of program version simultaneously, The transmission quantity of 2 bytes is only increased, the influence to protective program is minimum.
Detailed description of the invention
Fig. 1 is the Fibre-optical Pilot Protection interconnection schematic diagram of adjacent lines of the invention.
Fig. 2 is the Fibre-optical Pilot Protection interconnection schematic diagram of double-circuit line of the invention.
Fig. 3 is optical fiber pilot protection principal and subordinate channel interconnection schematic diagram of the invention.
Fig. 4 is method flow schematic diagram of the invention.
Specific embodiment
As shown in figure 4, a kind of detection method of Fibre-optical Pilot Protection, includes the following steps:
(1) sender and recipient respectively correspond two sides protective device, this side protective device is using CRC-16 algorithm to dress It sets application program and carries out sum check, generate 16 program ver-ify information;
(2) according to this wing passage identification code definite value in protective device, 16 identification codes for representing this wing passage are generated;
(3) unique 32 bit port letter is generated in conjunction with program ver-ify information and this wing passage identification code according to channel type Cease word;
(4) it sends information word and detection light sends out power, light sends out power real-time display in the case where device monitors menu;
(5) opposite side protective device judges whether received optical power meets the requirements, when optical fiber transport channel interruption or channel decline When consuming exceeded, opposite side protective device report " channel interrupt " or " communication channel delay is excessive " is latched pilot protection at this time;When light-receiving function Rate in the normal range when, starting in next step detect;
(6) opposite side protective device judges communication bit error rates and effectiveness of information: when reception information frame number and sending information frame It when number difference is more than setting threshold or mismatches for information checking code continuous 5 times, is judged to " channel step-out ", is latched vertical UNPROFOR Shield;When above situation is unsatisfactory for, it is normal to be judged to data link layer, and starting detects in next step;
(7) opposite side protective device parses the information word received, extracts contralateral approach identification code, opposite side program version respectively This information;
(8) opposite side protective device judges whether contralateral approach identification code is fixed with " the contralateral approach identification code " in protective device Value matching;When channel intersects from ring or single channel, above-mentioned 2 identification codes are mismatched;When channel is normal, above-mentioned identification code Match, starting detects in next step;
(9) judge whether opposite side program version and this side program version are consistent, wherein this side program version check information has been It is calculated via step (1);When two sides check information is inconsistent, it is inconsistent to be judged to two sides program, is latched pilot protection;Instead It, it is consistent to be judged to program version, open pilot protection.
Currently, associate power company has formulated the standardized designs specification of protective device, protective device function is unified, has determined The user interfaces such as value, menu.For compatibility standard design specification, while the optical-fibre channel detection etc. that protective device can be enhanced again Performance respectively detects channel physical layer, data link layer, application layer using the thinking of layered weighting.As long as above-mentioned There is channel abnormal in one layer of meaning, and protective device provides related warning information, and Latching Fiber pilot protection.Pass through one letter of setting Word (word length is 32) is ceased, uniquely to identify all kinds of optical-fibre channels.Comprehensively consider the configuring condition in field optical fibers channel, The composition of information word does following regulation: the information word of single are as follows: high 16 are this wing passage identification code, and low 16 are this Side program ver-ify code;Under principal and subordinate's channel pattern, main channel information word are as follows: high 16 are this wing passage identification code, and low 16 are this Side program ver-ify code;From channel information word are as follows: high 16 this wing passage identification codes, low 16 are the anti-of this side program ver-ify code Code.
Air conduct measurement, version verification are realized by the way of exchanging information word.This side protective device is protected by extracting opposite side The information word (channel recognition code, program ver-ify code) of protection unit transmitting, respectively with contralateral approach identification code definite value inside device, this Side program ver-ify code is compared, to obtain current passage connection state, program version consensus information.It is tied according to judgement Fruit, protective device start subsequent processing routine.
Entire detection process from sender and recipient together with complete, the two respectively physical layer, data link layer, Application layer detects Fibre-optical Pilot Protection.Sender, recipient respectively correspond two sides protective device.Any side is protected Protection unit all experienced transmission, receive 2 processes, this side protective device needs to send information to opposite side protective device, simultaneously It is also required to receive the information of opposite side protective device transmitting.
The compatible existing Technology design specification of above-mentioned detection scheme can be complete by two sides protective device interactive information word Various Fibre-optical Pilot Protection failures are detected standbyly, while consistency school can be carried out to two sides protective program version automatically It tests, improves detection efficiency, eliminate operation risk existing for artificial check and correction program version, have stronger engineering practicability.
Although the present invention is illustrated and has been described with regard to preferred embodiment, it is understood by those skilled in the art that Without departing from scope defined by the claims of the present invention, variations and modifications can be carried out to the present invention.

Claims (4)

1. a kind of detection method of Fibre-optical Pilot Protection, which comprises the steps of:
(1) sender and recipient respectively correspond two sides protective device, this side protective device answers device using CRC-16 algorithm Sum check is carried out with program, generates 16 program ver-ify information;CRC-16 algorithm specifically comprises the following steps: to read this side guarantor Protection unit program curing is deposited in an array, the byte number ProgSize of logging program, according to generator polynomial g (x)=x16+x12+x2+ 1 carries out the generation of CRC code to the byte in the array one by one;In order to improve the formation speed of CRC code, adopt It is handled with look-up table, concrete processing procedure is as follows: (21) preset one 16 crc value, initial value 0x0;(22) The nth byte in array is extracted, the value range of N is 1~ProgSize, and the least-significant byte exclusive or of the byte and CRC are obtained one A index value, and corresponding crc value is found in CRC-16 table according to the index value;(23) retain the most-significant byte of step (22) value It is constant, using the most-significant byte exclusive or of its least-significant byte and initial value as new least-significant byte value, combine most-significant byte, least-significant byte obtains new 16 Place value, and execute N=N+1;The verification of process (22), (23) up to completing all procedure bytes is repeated, may finally be obtained To the CRC check value of this side program;
(2) according to this wing passage identification code definite value in protective device, 16 identification codes for representing this wing passage are generated;
(3) unique 32 bit port information is generated in conjunction with program ver-ify information and this wing passage identification code according to channel type Word;
(4) it sends information word and detection light sends out power, light sends out power real-time display in the case where device monitors menu;
(5) opposite side protective device judges whether received optical power meets the requirements, when optical fiber transport channel interruption or channel attenuation are super When mark, opposite side protective device report " channel interrupt " or " communication channel delay is excessive " is latched pilot protection at this time;When light receiving power exists When in normal range (NR), starting detects in next step;
(6) opposite side protective device judges communication bit error rates and effectiveness of information: when reception information frame number and transmission information frame number are poor It when value is more than setting threshold or mismatches for information checking code continuous 5 times, is judged to " channel step-out ", is latched pilot protection;When When above situation is unsatisfactory for, it is normal to be judged to data link layer, and starting detects in next step;
(7) opposite side protective device parses the information word received, extracts contralateral approach identification code, opposite side program version letter respectively Breath;
(8) opposite side protective device judge contralateral approach identification code whether with " contralateral approach identification code " definite value in protective device Match;When channel intersects from ring or single channel, above-mentioned 2 identification codes are mismatched;When channel is normal, above-mentioned identification code matching, Starting detects in next step;
(9) judge whether opposite side program version and this side program version consistent, wherein this side program version check information via Step (1) is calculated;When two sides check information is inconsistent, it is inconsistent to be judged to two sides program, is latched pilot protection;Conversely, It is consistent to be judged to program version, open pilot protection.
2. the detection method of Fibre-optical Pilot Protection as described in claim 1, which is characterized in that in step (3), channel letter Cease word to generate using following rule: under single, it is this wing passage identification code that information word, which is high 16, and low 16 are this side Program ver-ify code;Under principal and subordinate's channel pattern, it is this wing passage identification code that main channel information word, which is high 16, and low 16 are this side journey It is this wing passage identification code that sequence check code, which is high 16 from channel information word, low 16 radix-minus-one complements for this side program ver-ify code.
3. the detection method of Fibre-optical Pilot Protection as described in claim 1, which is characterized in that in step (9), work as two sides When complement code characteristic each other occurs in check information, illustrate principal and subordinate channel cross-connect faults occurred, this also demonstrates two sides simultaneously Program version is consistent.
4. the detection method of Fibre-optical Pilot Protection as described in claim 1, which is characterized in that step (4) and step (5) It is carried out in physical layer;Step (6) is carried out in data link layer;Other steps are all carried out in application layer.
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