CN106874962A - The fusion method and device of multi-source satellite data - Google Patents

The fusion method and device of multi-source satellite data Download PDF

Info

Publication number
CN106874962A
CN106874962A CN201710146872.2A CN201710146872A CN106874962A CN 106874962 A CN106874962 A CN 106874962A CN 201710146872 A CN201710146872 A CN 201710146872A CN 106874962 A CN106874962 A CN 106874962A
Authority
CN
China
Prior art keywords
data
satellite data
satellite
fused
latent period
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201710146872.2A
Other languages
Chinese (zh)
Other versions
CN106874962B (en
Inventor
王得举
黄华文
刘黎明
潘红章
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pervasive Navtech Inc Co In Shanghai
Original Assignee
Pervasive Navtech Inc Co In Shanghai
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Pervasive Navtech Inc Co In Shanghai filed Critical Pervasive Navtech Inc Co In Shanghai
Priority to CN201710146872.2A priority Critical patent/CN106874962B/en
Publication of CN106874962A publication Critical patent/CN106874962A/en
Application granted granted Critical
Publication of CN106874962B publication Critical patent/CN106874962B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F18/00Pattern recognition
    • G06F18/20Analysing
    • G06F18/25Fusion techniques
    • G06F18/251Fusion techniques of input or preprocessed data

Abstract

The invention discloses a kind of multi-source satellite data fusion method and device, including:It is provided for depositing the caching chained list of data, the satellite data received by multiple receiving devices is continuously acquired respectively, and satellite data is stored in caching chained list as data cached at least a portion;Byte length similarity according to each first satellite data formerly received by a receiving device in multiple receiving devices and by another receiving device in multiple receiving devices between each second satellite data of rear reception, determines the satellite data being mutually matched between each first satellite data and each second satellite data as fused data.The fusion method and device of multi-source satellite data of the invention, can solve to merge the multi-source satellite data for receiving while shortage of data when receiving satellite data is reduced, and prevent the satellite data of output from the problem of substantial amounts of redundant data occur.

Description

The fusion method and device of multi-source satellite data
Technical field
The present invention relates to communication technical field, more particularly to a kind of multi-source satellite data fusion method and device.
Background technology
In the Big Dipper receives data set, the form for often being coordinated using commander's machine and network special line receives satellite data.Its In, commander's machine equipment receives satellite data by airlink;Network special line is then connected to satellite master station, using UDP message bag Form receive satellite data.
Because commander's machine equipment is susceptible to the influence of surrounding environment, such as block, wireless signal interference, therefore, lose number According to situation than more serious.In addition, UDP networks there is also the situation of loss.It can be seen that, any data insertion equipment or system All exist loss of data, it is imperfect situations such as, so as to cannot accomplish that 100% data are complete, so often using multi-source mode (i.e. Multiple receiving devices receive the mode of data simultaneously) realize the Big Dipper data, services of reliable stabilization to receive satellite data.
Although receiving data by multi-source mode can greatly improve the reliability of system, because data source is more The reason for source, while also bringing the phenomenon of Data duplication, so as to produce substantial amounts of redundant data, brought much not to system The erroneous judgement of certainty and many jammers.
For in the prior art because using multi-source mode to receive the Data duplication problem of Big Dipper data, it is desirable to provide Yi Zhongke Data fusion is carried out with to multi-source data, so as to export the method and device of unique, healthy and strong Big Dipper data.
The content of the invention
To solve the above problems, the present invention provides the fusion method and device of a kind of multi-source satellite data, to the multi-source Big Dipper Data are collected and fusion treatment, so as to avoid the occurrence of the problem of Data duplication.
To achieve the above object, a kind of fusion method of multi-source satellite data of the invention, comprises the following steps:
S1, the caching chained list for being provided for depositing data, continuously acquire the satellite number received by multiple receiving devices respectively According to, and satellite data is stored in caching chained list as data cached at least a portion, satellite data at least includes by many The first satellite data that a receiving device in individual receiving device is formerly received connects with by another in multiple receiving devices Second satellite data of the receiving unit in rear reception;
S2, according to the byte length similarity between each first satellite data and each second satellite data, determine each first The satellite data being mutually matched between satellite data and each second satellite data is used as fused data.
Further also include:
Matching latent period is set, according to the respective reception of the first satellite data and the second satellite data being mutually matched Whether time interval determines fused data for fused data in the cycle or number is merged outside the cycle in the range of matching latent period According to;
The redundant data of fused data in the cycle is deleted in chained list is cached.
Further, also include, the initial value of matching latent period is set, and according to the reception time interval of fused data Carry out dynamic and update matching latent period.
Further, it is determined that the fused data reception time interval as the sample information in sample table, according to Current sample information in sample table updates matching latent period.
Further, matching latent period is mathematical expectation and the standard side of the current whole sample informations in sample table Difference sum.
Further, also include, maximum latent period is set, storage time in caching chained list is more than maximum latent period Satellite data delete.
Further, also include, will determine as unmatched satellite data, cycle outer fused data and fusion number in the cycle According to exporting data as a result together.
A kind of fusing device of multi-source satellite data of the invention, it is characterised in that including:
Data buffer storage unit, is configured to deposit the satellite data received by multiple receiving devices for continuously acquiring respectively Used as data cached at least a portion, satellite data at least includes first by a receiving device in multiple receiving devices for storage Receive the first satellite data with by another receiving device in multiple receiving devices rear reception the second satellite data;
Data fusion unit, is configured to according to each first satellite data in data buffer storage unit and each second satellite data Between byte length similarity, determine the satellite data being mutually matched between each first satellite data and each second satellite data As fused data.
Further, data fusion unit includes:
Matching module, is configured to the satellite number for determining to be mutually matched between each first satellite data and each second satellite data According to;
Fused data determining module, is configured to set matching latent period, and according to being mutually matched that matching module determines The first satellite data and the second satellite data respective reception time interval whether in matching in the range of latent period, really It is fused data in the cycle or cycle outer fused data to determine fused data;
Redundant data cleaning modul, is configured to delete the redundant data of fused data in the cycle in data buffer storage unit Remove.
Further, fused data determining module is further configured to the reception time interval according to fused data come dynamic Update matching latent period.
Further, data buffer storage unit is configured to the satellite data more than predetermined maximum latent period by storage time Delete.
Further, also including data outputting unit, be configured to by matching unit be defined as unmatched satellite data with And the cycle outer fused data that determines of fused data determining module and fused data exports data as a result together in the cycle.
The fusion method and device of multi-source satellite data of the invention, satellite data is received using by multiple receiving devices Mode, reduces shortage of data when receiving satellite data;After satellite data is obtained, formerly received according to by a receiving device Each first satellite data it is similar to the byte length by another receiving device between each second satellite data of rear reception Degree, judges the matching degree of each first satellite data and each second satellite data, and by each first satellite data and each second The satellite data being mutually matched between satellite data used as fused data, melted by the multi-source satellite data for receiving that achieves a butt joint Close, so as to the phenomenon of substantial amounts of redundant data occurs in the satellite data for preventing output.
Brief description of the drawings
Fig. 1 is the flow chart of the fusion method of multi-source satellite data of the invention;
Fig. 2 is a kind of schematic flow sheet of embodiment of the fusion method of multi-source satellite data of the invention;
Fig. 3 is the operation result schematic diagram of embodiment illustrated in fig. 2;
Fig. 4 is the schematic block diagram of the fusing device of multi-source satellite data of the invention.
Specific embodiment
Below, with reference to accompanying drawing, structure of the invention and operation principle etc. are further described.
As shown in figure 1, a kind of fusion method of multi-source satellite data of the invention, comprises the following steps:
S1, the caching chained list for being provided for depositing data, continuously acquire the satellite number received by multiple receiving devices respectively According to, and satellite data is stored in caching chained list as data cached at least a portion, satellite data at least includes by many The first satellite data that a receiving device in individual receiving device is formerly received connects with by another in multiple receiving devices Second satellite data of the receiving unit in rear reception.
Wherein, caching chained list in addition to for temporarily depositing pending satellite data, or data processing container. After a satellite data is reached, corresponding data processing can be carried out to it in caching chained list, and according to result Removed in caching chained list or increase corresponding satellite data.Satellite data is being purged or is increasing to caching chained list During operation, while data cached being updated to satellite data composition, it is ensured that caching chained list and data cached big I With the result dynamic change according to data processing, such that it is able to reducing the load pressure of system, improving running efficiency of system.
In embodiments of the present invention, satellite data at least includes formerly being connect by a receiving device in multiple receiving devices Receive the first satellite data with by another receiving device in multiple receiving devices rear reception the second satellite data.At this Invent in another embodiment, satellite data can also be including the data content for receiving time and source etc. of satellite data.Defend The reception time of sing data, it is used to calculate reception time interval and the satellite between the satellite data and other satellite datas Storage time of the data storage in chained list is cached;The source of satellite data, is used to judge the satellite data and other satellite numbers It is same source data or different source data between, same source data is the satellite data and other satellite datas are by same reception The satellite data that equipment is obtained, different source data is that the satellite data is by defending that different receiving devices are obtained from other satellite datas Sing data.
S2, according to the byte length similarity between each first satellite data and each second satellite data, determine each first The satellite data being mutually matched between satellite data and each second satellite data is used as fused data.
Because same source data is the satellite data that is temporally continuously acquired by same receiving device, therefore it is not in number According to the phenomenon for repeating, and different source data is the satellite data synchronously continuously acquired by multiple different receiving devices, is only possible to There is the inconsistent situation of indivisible data, now, the different source data of acquisition is the phenomenon that substantial amounts of Data duplication occurs. Therefore it may only be necessary to whether be mutually matched between judging different source data, you can judge whether to have received the data of repetition.
In embodiments of the present invention, it is right to be carried out by the byte length to the first satellite data and the second satellite data Than analysis, the byte length similarity Sim according to satellite data judge between the first satellite data and the second satellite data whether Be mutually matched, so as to identify whether receive received before the second satellite data of rear reception similarity it is very high The first satellite data for first receiving, and as fused data.
Specifically, first, regard the first satellite data and the second satellite data as two vectors respectively to be processed, by Each byte in one satellite data and the second satellite data regards a dimension in corresponding vector as respectively.Then, then The distance between first satellite data and the corresponding vector of the second satellite data d are calculated by Euclidean distance.
Byte length similarity Sim and the computing formula apart from d are:
Wherein, VCi、VNjThe first satellite data, the second satellite data are represented respectively.
Due to the first satellite data VCi, the second satellite data VNjThe inconsistent situation of byte length is likely to occur, therefore, The contrast of byte length is carried out by the way of head alignment, will the first satellite data VCi, the second satellite data VNjThe first word Section alignment, then the byte length again to two satellite datas is compared.
Now, it may appear that the first satellite data VCiByte length be more than the second satellite data VNj(being shown in Table 1), first are defended Sing data VCiByte length be less than the second satellite data VNj(being shown in Table 2), the first satellite data VCiByte length be equal to the Two satellite data VNjThree kinds of situations (being shown in Table 3).As the first satellite data VCi, the second satellite data VNjByte length differ During cause, average value 128 is typically taken as dummy bytes difference.
The VC of table 1iWith VNjByte comparing result table (1)
The VC of table 2iWith VNjByte comparing result table (2)
The VC of table 3iWith VNjByte comparing result table (3)
Can be learnt from above-mentioned analysis, d (VCi,VNj)∈[0,∞);Sim(VCi,VNj)∈(0,1].When apart from d (VCi, VNj) it is bigger when, byte length similarity Sim (VCi,VNj) smaller, now the first satellite data VCi, the second satellite data VNj's Difference is bigger.As Sim (VCi,VNjDuring)=1, the first satellite data VC is representedi, the second satellite data VNjByte length it is complete It is complete consistent.
In embodiments of the present invention, as byte length similarity Sim (VCi,VNj) more than or equal to 99.5% when, you can really It is fixed to be mutually matched between first satellite data and the second satellite data, and the first satellite data that will be mutually matched and the second satellite Data are used as fused data.
In an alternative embodiment of the invention, also including setting matching latent period, according to the first satellite number being mutually matched According to the respective reception time interval with the second satellite data whether in matching in the range of latent period, determine that fused data is Fused data or cycle outer fused data in cycle;The redundant data of fused data in the cycle is deleted in chained list is cached.
For convenience of subsequent descriptions, matching latent period can be expressed as Twait
The reason for setting dynamically matches latent period is, because receiving device may be interfered, it is understood that there may be receive The equipment factors of instability, the satellite data arrival time that can at this time cause different receiving devices to receive may be inconsistent. Further, since different receiving devices are different according to current load, data arrival time can also change.Different receptions are caused to set The standby reception time for receiving satellite data that is possible identical or being mutually matched may be inconsistent.Therefore, it can set matching Latent period, then when fused data is judged, whether the reception time interval according to fused data is in matching latent period It is interior, it is determined whether to delete the redundant data of the fused data, so as to realize the fusion of data.
But, if setting the matching latent period of fixation in data anastomosing algorithm, in the case where change is loaded, meeting Substantial amounts of data are caused to judge by accident so that fusion failure.Need to set dynamic matching latent period for this, make matching latent period As the current ruuning situation of system and processing condition data are dynamically adjusted.At this point it is possible to first set the first of matching latent period Initial value, and according to fused data, that is, the first satellite data for having matched carrys out dynamic with the reception time interval of the second satellite data Update matching latent period so that the matching latent period in the present invention with the carrying out of data processing dynamic change.
In embodiments of the present invention, the renewal to the matching latent period includes:Sample table is set, predetermined quantity is obtained The reception time interval of the fused data of individual newest determination is used as the sample information in sample table, the current sample in sample table This information updating matches latent period.Wherein, matching latent period can be, for example, the current whole sample informations in sample table Mathematical expectation and standard deviation square value sum.In the embodiment of the present invention, in sample table the quantity of sample information can be more than or Equal to 10.
As shown in table 4, as a example by when the quantity of sample information is 10, at this point it is possible in the minimum number of sample information When, relatively reliable matching latent period is obtained, so as to reduce the workload of operation of system.When sample chained list is full, will The sample information being stored at first in sample table is taken out, and is put into the sample information of newest acquisition.First sample that will be in table 4 This information is removed, and other sample informations move forward one successively, and new sample information is put into last position.And removed sample letter Breath is not output as merging successful data, because the sample information had been recorded once before sample table is entered.
The acquisition time interval sample table of two satellite datas that table 4 is mutually matched
When system and device starts first, now sample table is sky, acquiescence matching latent period TwaitEqual to set Initial value, then collection is mutually matched reception time of the first satellite data and the second satellite data as sample information, successively It is put into sample table and is calculated.
Wherein, the computing formula of reception time interval (unit second) is:T=| TCi-TNj|。
Due to receiving time interval for discrete sample data, therefore its mathematic expectaion isIts variance ForIts standard variance is
After sample information according to respective amount in the sample of current time calculates E (T) and σ, calculate new matching and wait Cycle:Twait=E (T)+σ.
Knowable to above-mentioned calculating process, due to matching latent period TwaitComprising mathematic expectaion E (T) and standard variance σ, because This, matching latent period TwaitCan change with the change of load, so as to reflect the situation of system present load change.
But, not the redundant data of whole fused datas is deleted, only when the reception time interval of fused data When in the range of matching latent period, it is confirmed as in the cycle in the case of fused data, just will merges number in the cycle According to redundant data delete.And for receiving the cycle outer fused data that time interval is in outside matching latent period scope, protect Stay its redundant data.In one embodiment of the invention, redundant data can be formerly to obtain in the satellite data being matched Satellite data.
In embodiments of the present invention, it is similar when first satellite data and byte length for the second satellite data When degree is more than 99.5%, just it is believed that be mutually matched between first satellite data and second satellite data, i.e., now this One satellite data and second satellite data are confirmed as fused data.
In an alternative embodiment of the invention, also include, maximum latent period is set, storage time in caching chained list is more than The satellite data of maximum latent period is deleted.When getting new satellite data per subsystem, can all judge to have been stored in Whether the storage time of chained list centre halfback's sing data is cached more than maximum latent period, if greater than maximum latent period, then slow Deposit and delete this satellite data in chained list, it is new data cached so as to obtain.
Because the load of system and operational capability are limited, excessive satellite data deposit in caching chained list in when, can cause The workload increase of storage and computing, also, satellite data too early between the docking time receiving carries out follow-up data treatment, and it is to data Result is nonsensical, can only increase the operation burden of system.Therefore, maximum latent period is set, in chained list is cached only Satellite data of the storage time in maximum latent period is preserved and processed, load and the operation of system can be not only reduced Amount, also improves the efficiency of system, so as to improve the efficiency of fusion and the accuracy of fusion results.
In embodiments of the present invention, maximum latent period can be the fixed value that operator is set, for convenience of subsequent descriptions, Maximum latent period can represent T_MAX.
In an alternative embodiment of the invention, can also will determine as unmatched satellite data, cycle outer fused data and Fused data exports data as a result together in cycle.In addition to this it is possible to as needed, each reception device be received Data bulk, each reception device receive the retained cycle in fused data quantity, each reception device receive nonredundancy The cycle of data outer fused data quantity and unmatched satellite data, cycle outer fused data and fused data in the cycle Quantity together as result data export.
As shown in Fig. 2 being one embodiment of the fusion method of multi-source satellite data of the invention.In this embodiment, Receiving device is 2, respectively commands machine and network special line, in other embodiments, the quantity of receiving device can with more, But fusion method and principle are identical with the present embodiment.It is initial value, the sample letter for matching latent period to set maximum latent period Breath quantity is 10, and is set when similarity is more than 99.9%, determines that the first satellite data is matched with the second satellite data.
Whether the concrete operation process of the present embodiment is, when satellite data is received, first to judge there is caching in caching chained list , when caching chained list is space-time, directly be stored in the satellite data in caching chained list by data, is not space-time when caching in chained list, Whether the storage time for caching each satellite data stored in chained list is first judged successively more than maximum latent period, and deletes storage Time is more than the satellite data of maximum latent period;Then judge the source of remaining satellite data in caching chained list, sentence successively The disconnected satellite data received by the receiving device different from the satellite data that this receives whether the satellite received with this It is mutually matched between data, if matching, using two satellite datas as fused data;Finally, the reception of decision fusion data Whether time interval deletes the redundant data of fused data in the cycle in the range of matching latent period, and will be newest The reception time interval of whole fused datas is put into sample table, updates matching latent period.
According to above-described embodiment, operation result as shown in Figure 3 can be obtained.After system operation 233 seconds, can be by number It is as shown in table 5 according to collecting:
The results of running data summary table of table 5
It is most of by upper table it is known that the data that the relative commander's machine of data that network special line is obtained is obtained reach fast Go to merge the data that matching network special line is obtained all referring to the data for waving machine acquisition, fusion have matched 1400.Matching waits week The data merged outside phase have reacted the dynamic change situation of system, and the data merged outside matching latent period only account for whole fusions The 2.6% of data, and other 97.4% data can be merged in matching latent period.
While it can also be seen that, all there is the situation of loss of data by any one receiving device, using multi-source of the invention The fusion method of satellite data the satellite data that many source devices are received is carried out combing, collect, unified output after fusion treatment Effect data far better than single source device, so as to improve the reliability of system, the shortcomings of compensate for single source data and lose.
As shown in figure 4, a kind of fusing device of multi-source satellite data of the invention, including data buffer storage unit and data are melted Close unit, data buffer storage unit is used to obtaining and be stored with the satellite data that multiple receiving devices are received, data fusion unit pair The satellite data that received in data buffer storage unit carries out data processing.
Wherein, data buffer storage unit, is configured to the satellite data received by multiple receiving devices to continuously acquiring respectively Stored as data cached at least a portion, satellite data at least includes being set by a reception in multiple receiving devices Standby the first satellite data for formerly receiving with by another receiving device in multiple receiving devices rear reception the second satellite Data.The data cached data that can be purged according to follow-up data processing or increase satellite data update, it is ensured that slow The size of deposit data can be according to the result dynamic change of data processing, such that it is able to reducing the load pressure of system, improving system System operational efficiency.
In embodiments of the present invention, the reception time of satellite data is at least included as data cached satellite data and is come The data content in source etc..The reception time of satellite data, it is used to calculate the reception between the satellite data and other satellite datas Time interval and the satellite data are stored in the storage time in caching chained list;The source of satellite data, is used to judge that this is defended It is same source data or different source data between sing data and other satellite datas.
In embodiments of the present invention, because the load of system and operational capability are limited, excessive satellite data is deposited in slow When depositing in chained list, the workload of storage and computing can be caused to increase, also, satellite data too early between the docking time receiving is carried out subsequently Data processing, it is nonsensical to data processed result, can only increase the operation burden of system.Therefore, maximum wait week is set Phase, data buffer storage unit is configured to delete storage time more than the satellite data of predetermined maximum latent period, is to reduce The load of system simultaneously improves the efficiency of data processing.
Data fusion unit, is configured to according to each first satellite data in data buffer storage unit and each second satellite data Between byte length similarity, determine the satellite data being mutually matched between each first satellite data and each second satellite data As fused data.
In embodiments of the present invention, as byte length similarity Sim (VCi,VNj) more than or equal to 99.5% when, you can really It is fixed to be mutually matched between first satellite data and the second satellite data, and the first satellite data that will be mutually matched and the second satellite Data are used as fused data.
In embodiments of the present invention, data fusion unit includes matching module, fused data determining module and redundant data Cleaning modul.
Specifically, matching module, is configured to determine to be mutually matched between each first satellite data and each second satellite data Satellite data.Fused data determining module, is configured to set matching latent period, and mutual determined according to matching module The first satellite data matched somebody with somebody is matched in the range of latent period with whether the respective reception time interval of the second satellite data is in, Determine that fused data is fused data in the cycle or cycle outer fused data.Redundant data cleaning modul, is configured to delay data The redundant data of fused data is deleted in cycle in memory cell.
In another embodiment, fused data determining module is further configured to the reception according to fused data Time interval carrys out dynamic and updates matching latent period.At this point it is possible to the initial value of matching latent period is first set, and according to fusion Data, that is, the first satellite data for having matched carrys out dynamic renewal and matches wait week with the reception time interval of the second satellite data Phase, so that the matching latent period in the present invention can carry out dynamic change with the result of data processing.
In another embodiment, also including data outputting unit, it is configured to not be defined as matching unit not Cycle outer fused data and fused data is exported together in the cycle that the satellite data and fused data determining module matched somebody with somebody determine Data as a result.In addition to this it is possible to as needed, data bulk, each reception device that each reception device is received The cycle of the Non-redundant data that fused data quantity, each reception device are received outer fused data number in the retained cycle for receiving Amount and unmatched satellite data, cycle outer fused data and in the cycle fused data quantity together as result data Output, to facilitate operating personnel to judge for the effect of Data Fusion.
More than, schematic description only of the invention, it will be recognized by those skilled in the art that without departing from work of the invention Make on the basis of principle, various improvement can be made to the present invention, this belongs to protection scope of the present invention.

Claims (12)

1. a kind of fusion method of multi-source satellite data, it is characterised in that comprise the following steps:
S1, the caching chained list for being provided for depositing data, continuously acquire the satellite data received by multiple receiving devices respectively, and The satellite data is stored in the caching chained list and is at least wrapped as data cached at least a portion, the satellite data The first satellite data formerly received by a receiving device in the multiple receiving device is included to be set with by the multiple reception The second satellite data of another receiving device in standby in rear reception;
S2, according to the byte length similarity between each first satellite data and each second satellite data, determine each first satellite The satellite data being mutually matched between data and each second satellite data is used as fused data.
2. the fusion method of multi-source satellite data as claimed in claim 1, it is characterised in that also include:
Matching latent period is set, according to the respective reception of first satellite data and the second satellite data being mutually matched Whether time interval determines that the fused data is fused data or cycle in the cycle in the range of the matching latent period Outer fused data;
The redundant data of fused data in the cycle is deleted in the caching chained list.
3. the fusion method of the multi-source satellite data as described in right wants 2, it is characterised in that also include, sets described matching etc. The initial value in cycle is treated, and the matching latent period is updated come dynamic according to the reception time interval of the fused data.
4. the fusion method of multi-source satellite data as claimed in claim 3, it is characterised in that to the matching latent period Renewal includes:Sample table is set, and the reception time interval for obtaining the fused data of the newest determination of predetermined quantity is made It is the sample information in the sample table, the current sample information in the sample table updates the matching latent period.
5. the fusion method of multi-source satellite data as claimed in claim 4, it is characterised in that the matching latent period is institute State the mathematical expectation and standard deviation square value sum of current whole sample informations in sample table.
6. the fusion method of the multi-source satellite data as any one of claim 1-5, it is characterised in that also include, if Maximum latent period is put, storage time in the caching chained list is deleted more than the satellite data of the maximum latent period.
7. the fusion method of the multi-source satellite data as any one of claim 2-5, it is characterised in that also include, will It is defined as unmatched satellite data, the cycle outer fused data and fused data exports count as a result together in the cycle According to.
8. a kind of fusing device of multi-source satellite data, it is characterised in that including:
Data buffer storage unit, is configured to carry out storage work to the satellite data received by multiple receiving devices for continuously acquiring respectively It is data cached at least a portion, the satellite data at least includes by a receiving device in the multiple receiving device The first satellite data for formerly receiving is defended with by another receiving device in the multiple receiving device the second of rear reception Sing data;
Data fusion unit, is configured to according to each first satellite data in the data buffer storage unit and each second satellite data Between byte length similarity, determine the satellite data being mutually matched between each first satellite data and each second satellite data As fused data.
9. the fusing device of the multi-source satellite data as described in right wants 8, it is characterised in that the data fusion unit includes:
Matching module, is configured to the satellite data for determining to be mutually matched between each first satellite data and each second satellite data;
Fused data determining module, is configured to set matching latent period, and the institute being mutually matched determined according to matching module Whether the respective reception time interval for stating the first satellite data and the second satellite data matches latent period scope in described It is interior, determine that the fused data is fused data in the cycle or cycle outer fused data;
Redundant data cleaning modul, is configured to the redundant data of fused data in the cycle in the data buffer storage unit Delete.
10. the fusing device of multi-source satellite data as claimed in claim 9, it is characterised in that the fused data determines mould Block is further configured to update the matching latent period come dynamic according to the reception time interval of the fused data.
The fusing device of the 11. multi-source satellite data as any one of right wants 8-10, it is characterised in that the data are delayed Memory cell is configured to delete storage time more than the satellite data of predetermined maximum latent period.
The fusing device of the 12. multi-source satellite data as described in right wants 9 or 10, it is characterised in that also including data output list Unit, is configured to for the matching unit to be defined as the institute that unmatched satellite data and the fused data determining module determine State cycle outer fused data and fused data exports data as a result together in the cycle.
CN201710146872.2A 2017-03-13 2017-03-13 Fusion method and device of multi-source satellite data Active CN106874962B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710146872.2A CN106874962B (en) 2017-03-13 2017-03-13 Fusion method and device of multi-source satellite data

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710146872.2A CN106874962B (en) 2017-03-13 2017-03-13 Fusion method and device of multi-source satellite data

Publications (2)

Publication Number Publication Date
CN106874962A true CN106874962A (en) 2017-06-20
CN106874962B CN106874962B (en) 2020-09-01

Family

ID=59171106

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710146872.2A Active CN106874962B (en) 2017-03-13 2017-03-13 Fusion method and device of multi-source satellite data

Country Status (1)

Country Link
CN (1) CN106874962B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109143301A (en) * 2018-09-21 2019-01-04 中国航空无线电电子研究所 A kind of redundance management system of Satellite Navigation Set
CN116704306A (en) * 2023-06-29 2023-09-05 阳光农业相互保险公司 Planet satellite data fusion and color homogenizing method

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110160986A1 (en) * 2009-12-28 2011-06-30 Nec (China) Co., Ltd. Method and apparatus for traffic information conversion using traffic information element knowledge base
CN103033814A (en) * 2012-12-21 2013-04-10 中国船舶重工集团公司第七一○研究所 Multi-source data mixed platform and method for sonar detection positioning
CN103209328A (en) * 2013-04-19 2013-07-17 中国科学院遥感与数字地球研究所 Multi-source satellite image real-time online processing technical method and device
CN104699818A (en) * 2015-03-25 2015-06-10 武汉大学 Multi-source heterogeneous multi-attribute POI (point of interest) integration method
CN105160593A (en) * 2015-08-18 2015-12-16 国家电网公司 Power transmission and transformation equipment multidimensional heterogeneous data fusion method and system facing big data
CN105320805A (en) * 2015-08-21 2016-02-10 浙江大学 Pico-satellite multi-source reliability information fusion method
CN105512130A (en) * 2014-09-24 2016-04-20 中兴通讯股份有限公司 Method and device for data source fusion
CN105528399A (en) * 2015-12-01 2016-04-27 中国联合网络通信集团有限公司 Multi-source terminal parameter data fusion method and apparatus
CN105553630A (en) * 2014-10-30 2016-05-04 刘万洪 Multi-channel data integration method of aviation flight parameters
CN106407634A (en) * 2015-07-30 2017-02-15 中国科学院遥感与数字地球研究所 Inverse variance weighted average-based satellite AOD data fusion method and system
CN206002114U (en) * 2016-05-14 2017-03-08 中卫物联成都科技有限公司 A kind of hybrid navigation equipment based on Multi-source Information Fusion

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110160986A1 (en) * 2009-12-28 2011-06-30 Nec (China) Co., Ltd. Method and apparatus for traffic information conversion using traffic information element knowledge base
CN103033814A (en) * 2012-12-21 2013-04-10 中国船舶重工集团公司第七一○研究所 Multi-source data mixed platform and method for sonar detection positioning
CN103209328A (en) * 2013-04-19 2013-07-17 中国科学院遥感与数字地球研究所 Multi-source satellite image real-time online processing technical method and device
CN105512130A (en) * 2014-09-24 2016-04-20 中兴通讯股份有限公司 Method and device for data source fusion
CN105553630A (en) * 2014-10-30 2016-05-04 刘万洪 Multi-channel data integration method of aviation flight parameters
CN104699818A (en) * 2015-03-25 2015-06-10 武汉大学 Multi-source heterogeneous multi-attribute POI (point of interest) integration method
CN106407634A (en) * 2015-07-30 2017-02-15 中国科学院遥感与数字地球研究所 Inverse variance weighted average-based satellite AOD data fusion method and system
CN105160593A (en) * 2015-08-18 2015-12-16 国家电网公司 Power transmission and transformation equipment multidimensional heterogeneous data fusion method and system facing big data
CN105320805A (en) * 2015-08-21 2016-02-10 浙江大学 Pico-satellite multi-source reliability information fusion method
CN105528399A (en) * 2015-12-01 2016-04-27 中国联合网络通信集团有限公司 Multi-source terminal parameter data fusion method and apparatus
CN206002114U (en) * 2016-05-14 2017-03-08 中卫物联成都科技有限公司 A kind of hybrid navigation equipment based on Multi-source Information Fusion

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PAN ZHANG 等: "A New Fusion Structure Model for Real-time Urban Traffic State Estimation by multisource traffic data fusion", 《 2016 18TH ASIA-PACIFIC NETWORK OPERATIONS AND MANAGEMENT SYMPOSIUM (APNOMS)》 *
李敏 等: "多模全球导航卫星系统融合精密定轨", 《测绘学报》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109143301A (en) * 2018-09-21 2019-01-04 中国航空无线电电子研究所 A kind of redundance management system of Satellite Navigation Set
CN109143301B (en) * 2018-09-21 2022-12-27 中国航空无线电电子研究所 Redundancy management system of satellite navigation device
CN116704306A (en) * 2023-06-29 2023-09-05 阳光农业相互保险公司 Planet satellite data fusion and color homogenizing method

Also Published As

Publication number Publication date
CN106874962B (en) 2020-09-01

Similar Documents

Publication Publication Date Title
JP5230645B2 (en) System and method for optimizing data set changes
CN107728941A (en) A kind of block chain data compression method and system
CN108737333A (en) A kind of data detection method and device
CN108876335A (en) A kind of management of balance method and system, equipment and storage medium
CN106874962A (en) The fusion method and device of multi-source satellite data
CN110493148A (en) A kind of block processes, block common recognition and block synchronous method and device
CN109684284A (en) Sliding piecemeal data de-duplication method based on edge calculations
US20110055666A1 (en) Receiver for error-protected packet-based frame
EP3611879A1 (en) Data traffic statistics method and device based on block chain
CN106648994A (en) Method, equipment and system for backup operation on log
CN107370809A (en) Method of data synchronization and data search system
CN105792131A (en) Positioning method and system
CN106294611A (en) Core banking system and the old and new's core system data exchange method
CN108900621B (en) Fog computing mode-based difference cloud synchronization method
CN107506438A (en) A kind of data processing storage method and device for Internet of Things
CN113134828B (en) Positioning tracking system and time delay compensation method based on linear trend prediction
CN112988892A (en) Distributed system hot spot data management method
CN107197042A (en) A kind of resource synchronization method and device
CN109905597A (en) Eyeglass color-changing control method, device, glasses and readable storage medium storing program for executing
CN109446200A (en) A kind of method and device of data processing
CN115984723A (en) Road damage detection method, system, device, storage medium and computer equipment
CN111161397B (en) Human face three-dimensional reconstruction method and device, electronic equipment and readable storage medium
CN114528154A (en) Electric energy meter data recovery method, device, equipment and computer storage medium
CN107222548B (en) The reading/writing method of I/O data, device and system in distributed block storage system
CN116527169B (en) System and method for detecting wireless signal intensity in low population density area

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant