CN110175051A - The integrated telemetering configuring management method in star ground - Google Patents
The integrated telemetering configuring management method in star ground Download PDFInfo
- Publication number
- CN110175051A CN110175051A CN201910291099.8A CN201910291099A CN110175051A CN 110175051 A CN110175051 A CN 110175051A CN 201910291099 A CN201910291099 A CN 201910291099A CN 110175051 A CN110175051 A CN 110175051A
- Authority
- CN
- China
- Prior art keywords
- telemetering
- frame
- packet
- telemetry
- star
- 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
Links
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F9/00—Arrangements for program control, e.g. control units
- G06F9/06—Arrangements for program control, e.g. control units using stored programs, i.e. using an internal store of processing equipment to receive or retain programs
- G06F9/44—Arrangements for executing specific programs
- G06F9/445—Program loading or initiating
- G06F9/44505—Configuring for program initiating, e.g. using registry, configuration files
Abstract
The present invention relates to the star in satellite development process and in-orbit telemetering programming technique field integrated telemetering configuring management method；Described method includes following steps: star integrated frame table configuration file automatically generate, satellite telemetry stratification parsing, the star based on the equivalent generation of stratification telemetering telemetering closed loop compare；The present invention is using the big table design of stratification telemetering, ground telemetering can be automatically generated and parse big table, Star Service framing configuration file and telemetering On-board programming note number, it has been well adapted to the demand that satellite development stage telemetering tissue is frequently changed, has reduced the workload of comprehensive survey, observing and controlling and the framing layout of Star Service and telemetering parsing configuration；The present invention improves in-orbit telemetering programming modification ability on the long guard system fast adaptation star at ground observing and controlling center；The present invention is configured using three-dimensional telemetering, improves telemetering trackability, enhances Tracking Through Telemetry stationkeeping ability, quick position telemetry point and transmission path, is checked convenient for problem.
Description
Technical field
The present invention relates to satellite development process and in-orbit telemetering programming technique fields, and in particular to a kind of star it is integrated
Telemetering configuring management method.
Background technique
As shown in Fig. 7, for satellite telemetry there are a variety of telemetry modes, every kind of telemetry mode has corresponding frame table to configure,
In satellite development process, telemetry frame table layout scheme repeatedly changes, and consumes the great effort of observing and controlling Yu Star Service subsystem.It surveys
Control is with Star Service subsystem personnel first and under information in the quantity, size, packet of each satellite subsystem communication and coordination telemetering packet
The frequency is passed, telemetering packet is distributed according to the required frequency to the respective section of telemetry frame, if telemetering inadequate resource, considers adjustment
Telemetry frame subregion division mode, or coordinate with each subsystem, the requirement of the biography frequency down of telemetering cell is reduced, by repeatedly round-trip
Coordinate, determine each telemetering pack arrangement and pass frequency demand down, on this basis layout Star Service frame table and telemetering framing filing text
Part.
After satellite telemetry scheme determines, telemetering archive file is delivered comprehensive survey personnel by tracking-telemetry and command subsystem, and comprehensive survey personnel start
It configures telemetering and parses big table, the telemetering amount of the whole each subsystem of star is huge, and in satellite development stage, telemetering framing and processing
Method repeatedly converts, and input file has the problems such as writing mistake, seriously consumes the energy of comprehensive survey.It is set to observing and controlling and Star Service
After counting Star Service frame table, comprehensive survey is just initially configured ground telemetering and parses big table, fails to star collaborative design, the comprehensive examining system in ground
It is difficult to telemetering on fast adaptation star to modify, increases the urgency of comprehensive survey personnel telemetering configuration work.After satellite is in-orbit, certain feelings
Take remote measurement On-board programming under condition, rearrange Star Service telemetering programming note number and configuration ground telemetering parse big table be both needed to expend it is big
Measure energy, it is difficult to the On-board programming of telemetering and the fast adaptation of ground long tube system telemetry parsing be rapidly completed, delay satellite
Problem investigation.
Through the literature search of existing technologies, Chinese invention patent 201410163232.9 is disclosed using modularization
Configurable telemetry parameter dissection process system, is designed using modular architecture, by telemetry parameter dissection process process point
Be cut into multiple modules, each module keeps certain functional independence, can it is individually designed, upgrading or replacement, use simultaneously
The mode of basic database realizes the flexible configuration of Various types of data processing method, can quickly support the synchronism detection of more spacecrafts,
Can be good at adapting to the variation that Large-scale satellite integrated test system is tested telemetry parameter demand, versatility and flexibility compared with
It is good.But the prior art does not solve the tool of with how realizing satellite telemetry configuration star integrated management proposed by the invention
Body problem.
Summary of the invention
In view of the drawbacks of the prior art, the purpose of the present invention is to provide a kind of star integrated telemetering configuration management side
Method.Method of the invention is applied to satellite development process and in-orbit telemetering programs.Method of the invention comprising star telemetering configuration
The integration of file automatically generates, star in the test of the stratification parsing of satellite telemetry and ground semi physical telemetering closed loop compare
Method design, this method with taking the star of observing and controlling, Star Service and comprehensive survey integrative coordinated design, reduces observing and controlling, Star Service and comprehensive survey
Workload, the speed and the telemetering of ground long tube for improving in-orbit telemetering programming parses fast adaptation ability, improves telemetering production
Tracking and positioning capabilities of the raw point with transmission path.
The present invention is realized by following technical solution, the present invention relates to a kind of star integrated telemetering configuration pipe
Reason method, integrated frame table configuration file automatically generates with including the following steps: star, and satellite telemetry stratification parsing is based on layer
The star of the equivalent generation of secondaryization telemetering telemetering closed loop compare；
The star integrated frame table configuration file automatically generate and include the following steps: based on subsystem slave computer tissue
The property relevant constraint at same frame of cell passed down between frequency needs, cell in telemetering pack arrangement, packet, based on observing and controlling and Star Service point
The telemetering packet two-dimensional storage management strategy and telemetry frame Partition Mask of system, the synchronous Star Service framing configuration file, in-orbit distant of generating
It surveys the instruction of programming note number, telemetering archive file and ground telemetering and parses configuration file；
The satellite telemetry stratification parsing includes the following steps: that ground telemetering parsing first is matched according to the stratification generated
Big table is set, identification passes down telemetry mode and time division multiplexing counts, and corresponding parsing frame table is selected, according to frame table, by whole frame true form
Several segments are resolved into, by the telemetering packet of fragment update to corresponding subcontract layer, and indicate the Flushing status of segment；Time then
Each telemetering packet is gone through, the parsing of more new segment, the telemetering cell that will be parsed are completed according to the cells structure table of telemetering packet
Amount is updated to cell layer；The calculating and judgement that telemetering cell is finally completed in cell layer, telemetering physical quantity and judging result are existed
It is presented in application software；
The star based on the equivalent generation of telemetering stratification telemetering closed loop comparison include the following steps: ground observing and controlling with
In the test of Star Service semi physical, identical telemetering cell amount by star is shared, ground is given birth to according to the big table of stratification by telemetering cell
At telemetering packet, telemetry frame is generated by telemetering packet, then compares the telemetry frame that ground generates and the telemetering that star passes up and down, closed loop is completed
Satellite telemetry is collected and framing functional verification.
Preferably, the star integrated frame table configuration file automatically generate and include the following steps:
Step 1, each subsystem of satellite provides the cells structure for the telemetering packet that each system generates, and includes three category informations:
(1) information of telemetering cell Physical Quantity Calculation；
(2) property at same frame between telemetering cell requires relevant constraint, is used for multiple cell combinations into inseparable segment；
(3) down biography frequency demand information of the telemetering cell under each telemetry mode；
For software according to the property related constraint at same frame between the whole byte and cell of adjacent continuous cell combination in packet, Jiang Yibao is distant
If survey is divided into a minimum independent segments；For being multiplexed telemetering packet, the minimum independent segments of telemetering packet should own telemetering packet thus
The maximum union for each minimum independent segments that multiplex mode marks off；
For PCM telemetering, associated clip is the minimum unit of framing, and for packet telemetry, telemetering packet is minimum framing list
Position, but telemetering packet must be able to be the separation of these minimum independent segments across telemetry frame, the cut-point of across frame telemetering packet；
Step 2, the telemetering coating observing and controlling of slave computer tissue and Star Service subsystem are collected and are stored, by Star Service according to corresponding telemetering
The frame table of mode picking frame member from telemetering packet, is organized under telemetry frame and passes；For PCM, two-dimensional storage structure is established, under storage
Position machine telemetering packet, if certain telemetering package definition of slave computer is the r row data in two-dimensional storage structure, the then information in this telemetering packet
Positioning can be completed to position by (r, c), for the source of each frame member, with an initial position (r, c) and frame member length information
Description；To meet the actual software and hardware telemetering management of satellite, increase and the corresponding attribute information of (r, c) information；It is distant for subpackage
It surveys, telemetering Framing unit is indexed using " Bale No.+packet is long ", use " Bale No.+packet is long " description subpackage frame table that can meet ground solution
Analysis demand is further added by " Bale No.+packet is long " corresponding Star Service telemetering packet index configurations attribute letter to adapt to Star Service framing configuration file
Breath；
Step 3, the input information provided based on step 1 and step 2, generates framing basic unit -- frame member, PCM system
Frame member is the telemetering segment in packet, and the frame member of CCSDS subpackage system is telemetering packet；Frame member includes length, source index information；Frame
Member packet is under different telemetry modes, with the different requirements of the biography frequency down；
Step 4, there are different telemetry modes different telemetry frames to be multiplexed partitioned mode, and foundation draws each section of telemetry frame
Divide situation, for PCM telemetering system, the frame member in each telemetering packet is sequentially placed to the telemetry frame section for accordingly passing the frequency down
In, it is index with (r, c), generates the framing frame table of ground parsing；For packet telemetry system, telemetering packet is evenly distributed on
The subpackage area of telemetry frame guarantees that in the systemic circulation period, the biography interval down of the telemetering packet repeatedly passed down is uniform, generate with " Bale No.+
Packet length " is that the telemetering of index parses frame table.；
Step 5, the biography frequency demand down according to the telemetry frame subregion of each mode and telemetering cell under corresponding modes, according to
It is secondary to generate the frame table that corresponding ground telemetering parsing is used under each telemetry mode；
Step 6, PCM telemetering and packet telemetry have different frame table structure；For PCM telemetering, ground parses frame table and uses
Two-dimentional row-column configuration (r, c) mode indexes, and (r, c) has corresponding configuration attribute, converts star for (r, c) table that ground uses
The ram table related pattern make sure, then convert the hex configuration file on satellite for Star Service table, that is, meet satellite PCM frame table and matches
Set use；For packet telemetry, ground frame table uses " Bale No.+packet is long " structure to describe, and each telemetering Bao Jun has Star Service framing to match
Attribute is set, converts table used in Star Service for ground " Bale No.+packet is long " frame table, then convert Star Service table to hex used on satellite
Configuration file meets the configuration of satellite subpackage frame table and uses；
Step 7, the process that parsing frame table in ground is inversely generated by telemetering framing configuration file used on star, will be on star
Hex configuration file is converted into Star Service table, according to frame meta-attribute information and ground frame table in Star Service table frame member index information it
Between one-to-one relationship, can inversely generate ground telemetering parsing frame table, complete Star Service table and ground frame table bumpless transfer；
Step 8, the Star Service frame table configuration file that above step generates, is configured on star in frame table configuration ROM, completes star
Upper predefined frame table configuration；
Step 9, after Star Service initialization, the frame table in ROM is loaded into frame table configuration RAM, satellite is read in RAM in real time
Configuration framing frame table, complete telemetering framing；
Step 10, telemetry frame table has in-orbit modification ability all or in part, and ground is repaired for Star Service framing frame table
Change area, according to the note number format of agreement, is packaged into in-orbit telemetering programming note number instruction；
Step 11, ground sends in-orbit telemetering programming note number instruction, modifies the frame table configured in Star Service RAM, completes frame table
In-orbit modification；Simultaneously because integration generates management, ground telemetering parses frame table being capable of programming modification on synchronous adaptation star；
Step 12, ground exports the cell parameters processing method file of framing frame table Yu each telemetering packet simultaneously, as entering
Library filing and file for future reference, reduce the workload of telemetering processing file edit.
Preferably, the satellite telemetry stratification parsing includes the following steps:
Step 1, each slave computer of satellite collects telemetering amount, such as voltage, temperature analog quantity, the number such as switching on and shutting down, application state
Word amount；
Step 2, each slave computer tissue of satellite generates telemetering packet, is sent to Star Service, and Star Service carries out storage management to telemetering packet；
Step 3, according to the telemetry mode of current setting, respective frame table is selected.
Step 4, respective frame table is read from RAM.
Step 5, beat is counted according to corresponding telemetry frame table and multiplexing, it is distant needed for being extracted from telemetering storage management buffer area
Measured data；
Step 6, Star Service framing module completes the telemetry frame tissue that certain multiplexing under certain telemetry mode counts beat, by whole frame
It is passed under telemetry；The above process is repeated, completes to pass under being continuously generated of telemetry frame；
Step 7, ground receiver telemetry carries out stratification parsing；The ground parsing frame table of corresponding telemetry mode is read,
Telemetry frame is resolved into discrete segments, segment is distributed to corresponding telemetering packet；For PCM telemetering, the byte in telemetry frame is pressed
It is indexed according to frame table (r, c), at c-th of byte of distribution to packet r, and shows that this byte has refreshed in packet；For packet telemetry,
Refresh corresponding telemetering package informatin if telemetry frame is resolved into a packet according to " Bale No.+packet is long " index frame table；
Step 8, each telemetering packet is traversed, if information is refreshed in packet, to more new information according to telemetering packet cells
Telemetering cell one by one is resolved into structure table, step-by-step, by telemetering cell true form information update to the corresponding telemetering amount of cell layer.If distant
It surveys packet and there is multiplexing, then according to multiplexed situation, select corresponding telemetering packet cells structure table, packet to the telemetering that takes remote measurement is believed
The decomposition of member；
Step 9, it to the telemetering cell of update, is calculated according to the processing method of configuration, obtains the physics of telemetering cell
Amount judges whether physical quantity is abnormal according to the criterion of configuration；
Step 10, the telemetering cell physics parsed is shown, distinguishes real-time telemetry and delayed telemetry amount, and show
Physical quantity judging result.
Preferably, the star based on the equivalent generation of telemetering stratification telemetering closed loop comparison include the following steps:
Step 1, in the test of Star Service semi physical, identical telemetering amount is shared to star；Swashed with the telemetering amount that test equipment is simulated
It encourages each slave computer of satellite and generates telemetering packet, or generate telemetering packet, each slave computer or slave computer using slave computer interface simulator
Telemetering packet is sent to Star Service and carries out framing by interface simulator；
Step 2, the telemetering amount of simulation is sent to the cell layer of the big table of stratification by Star Service semi physical test equipment, updates letter
The telemetering cell amount of first layer；
Step 3, according to the cells structure table of telemetering packet, telemetering packet is generated with the telemetering amount tissue of cell layer；
Step 4, the scheduling according to telemetering group frame pattern and multiplexing time controller, selects respective frame table and corresponding counts section
It claps, extracts information in telemetering packet and generate telemetry frame；
Step 5, after the equivalent generation of stratification for completing telemetry frame, telemetry frame is sent to telemetering closed loop comparison module；
Step 6, telemetering closed loop comparison module receives Star Service telemetry frame, and the telemetry frame generated with comparing star completes telemetry frame
Closed loop compare, verify telemetering framing correctness；The telemetry frame passed down to satellite carries out stratification parsing, compare parse it is distant
It whether consistent with the telemetering amount of test equipment simulation surveys cell physical quantity, verifies the correctness of Star Service framing.
Compared with prior art, the present invention achieve it is following the utility model has the advantages that
1, the present invention can automatically generate the big table of ground telemetering parsing, Star Service framing is matched using the big table design of stratification telemetering
It sets file and telemetering On-board programming infuses number, be well adapted to the demand that satellite development stage telemetering tissue is frequently changed, reduced
The workload of comprehensive survey, observing and controlling and the framing layout of Star Service and telemetering parsing configuration；
2, the present invention improves in-orbit telemetering programming modification ability on the long guard system fast adaptation star at ground observing and controlling center；
3, the present invention is configured using three-dimensional telemetering, improves telemetering trackability, enhances Tracking Through Telemetry stationkeeping ability, quickly
Position telemetry point and transmission path are checked convenient for problem；
4, the present invention can be combined with satellite hub unit semi physical test macro, by star share identical telemetering
Amount compares the telemetry frame of the telemetry frame and the equivalent generation of ground telemetering that generate on star, completes telemetering closed loop and compares, abundant on ground
Verify framing function on star.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon:
Fig. 1 is the present invention is based on the star of the big table structure of stratification integrated telemetering configuration management schematic diagram；
Fig. 2 is that PCM system telemetry frame table of the present invention configuration automatically generates flow diagram；
Fig. 3 is PCM system telemetry frame stratification process of analysis schematic diagram of the present invention；
Fig. 4 is that CCSDS subpackage system telemetry frame table of the present invention configuration automatically generates process；
Fig. 5 is CCSDS system telemetry frame stratification process of analysis schematic diagram of the present invention；
Fig. 6 be the present invention is based on the telemetering of the big table of stratification parsing, it is equivalent with compare flow chart；
Fig. 7 is satellite telemetry mode type schematic diagram of the present invention；
Fig. 8 is the multiplexing frequency and radio frequency channel space schematic diagram in 4 frame areas；
Fig. 9 is the multiplexing section schematic diagram in discontinuous 4 frame area；
Figure 10 is telemetering packet storage management schematic diagram；
Figure 11 is the subpackage area template schematic diagram of packet telemetry system；
Figure 12 is telemetering packet storage management schematic diagram；
Figure 13 is that the multiplexing of PCM telemetry frame divides (left side) and packet telemetry subpackage plot structure (right side) schematic diagram；
Figure 14 is PCM telemetering packet storage management structure (left side) and packet telemetry packet storage management structure (right side) schematic diagram.
Specific embodiment
The present invention is described in detail combined with specific embodiments below.Following embodiment will be helpful to the technology of this field
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill of this field
For personnel, without departing from the inventive concept of the premise, several changes and improvements can also be made.These belong to the present invention
Protection scope.
Embodiment
For with solving the problems, such as satellite telemetry configuration star integrated management, the present invention provides a kind of star integrated telemetering
Configuring management method, integrated frame table configuration file automatically generates with including the following steps: star, satellite telemetry stratification parsing,
Star based on the equivalent generation of stratification telemetering telemetering closed loop compare.
Present pre-ferred embodiments are provided with reference to the accompanying drawing, in order to explain the technical scheme of the invention in detail.
The present invention proposes a kind of completely new method for solving the problems, such as satellite telemetry configuration star integrated management.This
Invention provides a kind of Star Service frame table, ground telemetering parsing frame table, in-orbit telemetering programming note number and telemetering archive file one metaplasia
At the method for management: the star of PCM telemetering system as shown in Figure 2 ground frame table integration automatic generation method, as shown in Figure 3
The stratification telemetering analytic method of PCM telemetering system, the star of packet telemetry system as shown in Figure 4 the integration of frame table it is automatic raw
At method, the stratification telemetering analytic method of packet telemetry system as shown in Figure 5 is as shown in FIG. 6 to be based on the big table of stratification
Telemetering parsing, the telemetering equivalent star with Star Service semi physical in test ground telemetering closed loop comparison method.As shown in fig. 7, satellite is distant
There are a variety of telemetry modes, every kind of telemetry mode has corresponding frame table to configure for survey, and in satellite development process, telemetry frame table is compiled
Row's scheme repeatedly changes, and consumes the great effort of observing and controlling Yu Star Service subsystem.Fig. 1 is for the star based on the big table structure of stratification
Integrated telemetering configuration management schematic diagram.
1, the star of PCM telemetering system ground frame table automatic generation method (such as Fig. 2)；
Template definition: telemetry frame includes frame head area, postamble area, frame data domain area, as defined in the table below under certain telemetry mode
Frame data domain is divided into 1 frame/period, 4 frames/period, 16 frames/period, 32 frames/period etc. (with 2 by frame data domain multiplex moden
Frame/period is divided).Framing basic unit generate: according to subsystem provide offer telemetering packet cells structure table,
Processing generates basic Framing unit (abbreviation frame member).
Certain telemetry mode frame structure template of 1 PCM telemetering of table
2 telemetering packet cells structure table of table
According to whole byte constraint condition, telemetering packet is divided into several segments, each segment is integer byte, if comprising
Dry telemetering cell.Property at same frame according to telemetering cell constrains (the biography time consistencies down of i.e. multiple cells), will have property at same frame to want
The multiple segments asked are bundled into a combination segment, combine each sub-piece in segment have it is identical under pass the frequency.By adjacent
The constraints such as the property at same frame between the whole byte and cell of consecutive cell combination, telemetering packet is divided into and isolates segment one by one, these
Isolated segment is the minimum thread of framing, abbreviation frame member.
For multiplexing telemetering packet, (i.e. a telemetering packet has a variety of cells forms, a variety of cells mode timesharing
Be multiplexed the same telemetering packet resource), the frame member of telemetering packet should multiplex mode used in telemetering packet marks off thus each frame member most
Big union.
Frame member has different biography frequency demands down under different telemetry modes, and different telemetry modes have not
With telemetering Partition Mask.Partition Mask bearing capacity evaluation: being directed to certain telemetry mode M, is divided according to observing and controlling and the telemetering of Star Service,
Determine each partition size (can adjust according to the actual situation).
It is divided according to template, is divided into 4 frame areas, 16 frame areas, 64 frame areas.By taking 4 frame areas as an example, this section is W30~W70 (41
Byte), then total bearing capacity is 4*41=164 byte.According to the telemetering packet source data that each subsystem provides, delta frame
Member counts wherein 4 frames/period frame member summation, assesses the bearing capacity of current subregion.If cannot carry, adjustment source is considered
The frequency demand or adjustment partition size of data, guarantee each subregion adaptation.It can also be assessed according to each input information requirement
The size requirement situation in 1 frame area, 4 frame areas, 16 frame areas, 64 frame areas instructs subregion with this, or feeds back to each family, adjustment input
The frequency demand of information is to adapt to radio frequency channel resource.
Radio frequency channel automatic editing in subregion: by taking 4 frame areas as an example, this area's schematic diagram as shown in figure 8,4 frames one recycle, be divided into one,
Two, three, four totally four time division multiplexing areas.It is assessed by early period, bearing capacity is with meet demand.The frame member that telemetering packet is generated according to
It is secondary to be put into lower template.
Constraint condition: it is necessary in the frontier district (being herein one, the W70 of two, three, four each subdivisions) of each subdivision
The ending for completing frame member does not allow frame member to be divided, i.e. frame member is not divided in time-domain, and blank parts temporarily fill AA.
Recommend with frequency multiplexing area to be continuous section, but actual conditions may change, such as: it is distributed in and several does not connect there are 4 frame areas
On continuous section, sample situation is as shown in Fig. 9 Partition Mask.Constraint condition at this time is still: the ending of each sub-segments is
One in a frame telemetering of the ending (it is the ending of whole frame member that situation, which is W70, W211, in figure) of one frame member, i.e. frame member
Do not allow to be divided in sub-segments.
Ground telemetering parsing frame table automatically generates: ground describes telemetering packet in (r, c) (Bale No., packet in byte location) mode
Middle information position, therefore each frame member has oneself corresponding (r, c) coordinate section.As shown in Figure 10.
Frame member is completed by above step to distribute into telemetering Partition Mask, its (r, c) coordinate section of frame member is retouched
It states, can be obtained ground telemetering frame parsing frame table, see the table below.
Star Service frame table automatically generates: according to telemetering packet (r, c) coordinate and Star Service storage management address (such as address ram) one
One corresponding relationship can obtain Star Service frame table, see the table below.
After obtaining Star Service frame table, Star Service frame table is converted into hex configuration file, programming enters Star Service frame table configuration ROM.Simultaneously
According to having reverse ability, ground telemetering can be inversely gone out from Star Service frame table configuration file and parse frame table, with completing star telemetry frame table
Bumpless transfer.
In-orbit telemetering programming note number automatically generates: can export the programming telemetering area radio frequency channel table in Star Service frame table, be packaged into
It programs telemetering and infuses number packet format, upper note satellite modifies the frame table configuration of Star Service, completes in-orbit telemetry frame table change, while ground
The long tube hub of observing and controlling can also the modification of fast adaptation Star Service frame table.
Telemetering archive file automatically generates: exporting the telemetering framing file and telemetering cell parameters processing method text of filing
Part reduces the workload of file edit, reduces file edit error probability.
2, the star of packet telemetry system ground frame table automatic generation method (such as Fig. 4)；
Template definition: configuration telemetering frame structure, the section (W056-W254) in definition subpackage area and multiplexing period (such as 32 frames/
Period).
3 packet telemetry frame of table
Framing basic unit generates: the minimum group frame unit (frame member) of packet telemetry is telemetering packet, and telemetering packet is according to whole word
Section and the constraints such as property at same frame, which are divided into, several cuts inseparable segment.Telemetering packet exists across frame, i.e. telemetering coating is segmented in two frames,
The cut-point of telemetering packet must be that (for being multiplexed telemetering packet, the independent segments of telemetering packet should be each multiplexing used to independent segments
Model split go out each independent segments maximum union) separation, do not allow a segment to be divided in two frames.
4 telemetering packet cells structure table of table
Partition Mask bearing capacity evaluation: first determine subpackage area size, further according to each family under this telemetry mode frame table
In packet loop number, complete subpackage frame table and automatically generate.
It is divided according to template, determines subpackage area and entire cycle period, therefore the bearing capacity in subpackage area is " subpackage area
Size * cycle period ".The telemetering packet provided according to each subsystem and its cycle-index in the period calculate telemetering and carry demand
1 long * packet of=packet+2 long * packets of packet+packet 3 long * packets ... .+ packet n long * packet.Compare subpackage area carrier ability to hold with telemetering
Load demand adjusts subpackage area size or packet frequency demand if mismatching, and the vacant area in part can be filled AA or use infilled frame.
Can also be according to the remote control packet and frequency demand of each family, subpackage area size required for determining instructs subpackage zoning fixed with this.
Radio frequency channel automatic editing in subregion: by taking Figure 11 as an example, subpackage area is W56-W255, amounts to 200 bytes, systemic circulation period
It is 64, therefore total bearing capacity is 200*64 byte.
The telemetering packet and frequency demand provided according to each subsystem, calculates total telemetering space requirement amount, guarantees through toning
After whole, bearing capacity is with meet demand.There is the telemetering packet of multiplexing frequency demand, should ensure that the interval occurred in systemic circulation is more equal
It is even, guarantee certain isochronism as far as possible.
Above packet telemetry system is the subpackage system for the fixed schedule strategy according to the systemic circulation period.For adopting
It, can not predefined frame table with the dynamic frame table of prioritized contention mechanism.Use priority scheduling strategy framing, ground on star
Parsing is parsed according to the mode of (first top guide pointer+pack arrangement).
Ground telemetering parsing frame table automatically generates: ground describes information position in telemetering packet in such a way that Bale No., packet are long, therefore
Each frame first (i.e. telemetering packet) has oneself corresponding packet APID and packet to grow.As shown in figure 12.
It completes frame member by above step to distribute into telemetering Partition Mask, by frame member Bale No. and the long description of packet, i.e.,
It can get ground telemetering frame and parse frame table.
5 packet telemetry ground telemetering of table parses frame table
Star Service frame table automatically generates: with parsing big table (Bale No.+packet is long) coordinate and Star Service storage management according to ground telemetering
Location one-to-one relationship can obtain Star Service frame table.
6 packet telemetry Star Service framing table of table
| Frame number | Packet queue |
| 0 | 2853 6C55 2854 0000 0000 |
| 1 | 2853 2683 3C23 3834 0000 |
| 2 | 2853 44C4 2A33 2AC3 0000 |
| 3 | 2853 8644 0CB3 0000 0000 |
| 4 | A442 1025 0000 0000 0000 |
| 5 | 2853 6C55 2854 0000 0000 |
| 6 | 2853 7C22 0000 0000 0000 |
| ... | .............................. |
| ... | .............................. |
| 63 | B463 1435 0000 0000 0000 |
After obtaining Star Service frame table, Star Service frame table is converted into hex configuration file, programming enters Star Service frame table configuration ROM.Simultaneously
According to having reverse ability, ground telemetering can be inversely gone out from Star Service frame table configuration file and parse frame table, with completing star telemetry frame table
Bumpless transfer.
In-orbit telemetering programming note number automatically generates: can export the programming telemetering area radio frequency channel table in Star Service frame table, be packaged into
It programs telemetering and infuses number packet format, upper note satellite modifies the frame table configuration of Star Service, completes in-orbit telemetry frame table change.Ground simultaneously
The long guard system of observing and controlling can also the modification of fast adaptation Star Service frame table.
Telemetering archive file automatically generates: exporting the telemetering framing file and telemetering cell parameters processing method text of filing
Part reduces file and summarizes the workload write, reduces file edit error probability.
3, the telemetry frame stratification process of analysis (such as Fig. 3) of PCM telemetering system；
Ground receiver telemetry carries out stratification parsing.The ground parsing frame table for reading corresponding telemetry mode, by telemetering
Frame resolves into discrete segments, and segment is distributed to corresponding telemetering packet.For PCM telemetering, by the byte in telemetry frame according to frame table
(r, c) index, distribution is extremely wrapped at c-th of byte of r, and shows that this byte has refreshed in packet.
Each telemetering packet is traversed, if information is refreshed in packet, to more new information according to telemetering packet cells structure table,
Telemetering cell one by one is resolved into, by telemetering cell true form information update to the corresponding telemetering amount of cell layer.If telemetering packet exists multiple
With, then according to multiplexed situation, select corresponding telemetering packet cells structure table, take remote measurement packet to telemetering cell decomposition.
It to the telemetering cell of update, is calculated according to the processing method of configuration, obtains the physical quantity of telemetering cell, according to
The criterion of configuration judges whether physical quantity is abnormal.The telemetering cell physics parsed is shown, real-time telemetry is distinguished and prolongs
When telemetering amount, and show physical quantity judging result.
4, the telemetry frame stratification process of analysis (such as Fig. 4) of packet telemetry system；
Two ways can be used in the decomposition of packet telemetry frame to telemetering packet: it is a kind of using precognition frame table, read corresponding telemetering
The ground of mode parses frame table, according to the index frame table of (Bale No.+packet is long), if telemetry frame is resolved into a packet, refreshes corresponding distant
Survey package informatin；A kind of mode based on first top guide pointer+pack arrangement parses, and according to first top guide pointer, finds first packet, then according to first
Packet length, finds next telemetering packet, long according to this telemetering packet, finds next telemetering packet, so completes telemetry frame to distant
The decomposition for surveying packet, refreshes corresponding telemetering package informatin.
Each telemetering packet is traversed, if information is refreshed in packet, to more new information according to telemetering packet cells structure table,
Telemetering cell one by one is resolved into, by telemetering cell true form information update to the corresponding telemetering amount of cell layer.If telemetering packet exists multiple
With, then according to multiplexed situation, select corresponding telemetering packet cells structure table, take remote measurement packet to telemetering cell decomposition.
It to the telemetering cell of update, is calculated according to the processing method of configuration, obtains the physical quantity of telemetering cell, according to
The criterion of configuration judges whether physical quantity is abnormal.The telemetering cell physics parsed is shown, real-time telemetry is distinguished and prolongs
When telemetering amount, and show physical quantity judging result.
5, telemetering stratification is equivalent and compares process；
In ground observing and controlling and the test of Star Service semi physical, identical telemetering cell amount, ground foundation can by star be shared
The big table of stratification, by telemetering cell generate telemetering packet, by telemetering packet generate telemetry frame, then compare ground generate telemetry frame with
The telemetering that star passes up and down, closed loop are completed satellite telemetry and are collected and framing functional verification.
In the test of Star Service semi physical, identical telemetering amount is shared to star.Satellite is motivated with the telemetering amount that test equipment is simulated
Each slave computer generates telemetering packet, or generates telemetering packet, each slave computer or slave computer interface mould using slave computer interface simulator
Telemetering packet is sent to Star Service and carries out framing by quasi- device.
The telemetering amount of simulation is sent to the cell layer of the big table of stratification by Star Service semi physical test equipment, updates cell layer
Telemetering cell amount.According to the cells structure table of telemetering packet, telemetering packet is generated with the telemetering amount tissue of cell layer.
According to the scheduling of telemetering group frame pattern and multiplexing time controller, respective frame table and corresponding counts beat are selected, is mentioned
Information in telemetering packet is taken to generate telemetry frame；After the equivalent generation of stratification for completing telemetry frame, telemetry frame is sent to telemetering closed loop
Comparison module.Telemetering closed loop comparison module receives Star Service telemetry frame, and the telemetry frame generated with comparing star completes the closed loop of telemetry frame
It compares.
The telemetry frame passed down to satellite simultaneously carries out stratification parsing, compare the telemetering cell physical quantity that parses whether with
The telemetering amount of test equipment simulation is consistent, verifies the correctness of Star Service framing.
A kind of the present invention provides star the method for integrated telemetering configuration management.The present invention realizes the configuration of Star Service framing
File, in-orbit telemetering programming note number, telemetering archive file and ground telemetering parse big synchronizing for table configuration file and automatically generate, real
Telemetering closed loop compares with having showed the star of stratification parsing and the test of ground semi physical of satellite telemetering data.
Measure method disclosed in this invention has centainly the satellite of various PCM telemetering systems and packet telemetry system
Versatility.For PCM and subpackage mixing telemetering system (such as PCM+PCM, PCM+ subpackage), it is decomposed into PCM and two bases of subpackage
This type, therefore the present invention is also suitable and hybrid scheme.
There is following examples process again, comprising: step 1, comprehensive survey cooperate with tracking-telemetry and command subsystem, formulate big table construction strategy,
The telemetering packet that each slave computer generates is managed in a manner of set；It in telemetering group frame pattern and the multiplexing period for determining satellite, establishes big
Table macroscopic frame.Step 2, each subsystem provide detailed telemetering packet cells structure and describe table: comprising telemetering cell title
Code name, processing method, Rule of judgment, for generating the distant measurement processing and abnormal judgement of cell layer；Comprising under mould telemetry mode
The biography frequency down require and property at same frame require etc. Framing units divide constraint condition, decompose to several segments for telemetering packet.
The cells structure table of 7 telemetering packet of table
Step 3, as Figure 13 observing and controlling and Star Service determine under each telemetry mode telemetry frame subregion (PCM telemetering it is each under
Pass the subpackage area in frequency area, packet telemetry) division mode, generate framing template.
Whether assessment telemetering partitioned resources meet each subsystem applicable requirements, if not satisfied, adjustment partitioned mode or drop
The biography frequency demand down of low subsystem telemetering cell, matches telemetry frame template with each subsystem applicable requirements.
Step 4, such as the storage management table of Figure 14 observing and controlling and Star Service personnel layout telemetering packet, the storage RAM of PCM telemetering
Location, Star Service telemetering packet index code name of packet telemetry etc..
Step 5, according to the requirement of the biography frequency down of information in each slave computer telemetering packet, distribution to corresponding telemetry frame area.It is such as attached
Fig. 2 is PCM telemetry frame table product process, and frame member is distributed to its required Xia Chuan frequency area, if attached drawing 4 is CCSDS subpackage
Telemetry frame table product process distributes telemetering packet to subpackage area, and for across frame packet, the cut-point of packet is point of independent segments in packet
The biography interval time down of boundary's point, the telemetering packet repeatedly passed down in a large period is uniform as far as possible.
Step 6 generates the telemetry frame frame table of ground parsing, configures text according to frame table on following ground frame table index and star
The corresponding relationship of part generates Star Service frame table, then Star Service frame table is converted into hex configuration file, is configured to frame table on star and configures
ROM.When Star Service opening initialization, ROM frame table is loaded onto RAM automatically, completes Star Service group according to the frame table configuration in RAM
Frame.
Step 7 can inversely go out Star Service frame table, it is big to re-map into ground telemetering parsing inversely from Star Service framing hex file
Table, thus with the completing star bumpless transfer of frame table.
Step 8, according to the telemetering packet cells structure table of frame table and subsystem, generate observing and controlling frame table archive file with
Telemetry parameter handles archive file.
Step 9 when in-orbit telemetering programs, according to the telemetry frame table of layout, generates Star Service frame table, will be in Star Service frame table
Programmed fraction is encapsulated according to note on formats, generates note note number instruction in telemetering programming, is sent to satellite, and change frame table configures RAM
File completes frame table modification on star, while the telemetering of ground long tube parses big table synchronous adaptation.It is with completing star above integrated
Telemetering configuration management.Simultaneously can with stratification complete telemetry frame parsing, it is equivalent with compare.The present invention is by constructing one kind by group
The big table structure of stratification of frame-layer, subcontract layer, cell layer, group frame-layer are completed telemetry frame according to the frame table under various telemetry modes and are arrived
The decomposition of telemetering packet, subcontract layer complete decomposition of the telemetering packet to telemetering amount, cell according to the telemetering pack arrangement table of slave computer tissue
Layer completes the telemetering Physical Quantity Calculation and judgement of real-time delay, completes the stratification parsing of satellite telemetering data；Equally using inverse
To process, also the stratification of achievable telemetry frame is generated equivalent, is cooperated Star Service semi-physical simulation test platform, is shared telemetering to star
Cell, framing and the equivalent framing of ground telemetering on comparison star compare the telemetering amount that ground floor time neutralizing analysis satellite telemetry frame obtains
With the physical quantity of semi physical test equipment output, the correctness that satellite telemetry collects framing function is completed.
In conclusion the present invention can be automatically generated ground telemetering and be parsed big table, Star Service using the big table design of stratification telemetering
Framing configuration file and telemetering On-board programming infuse number, have been well adapted to the need that satellite development stage telemetering tissue is frequently changed
It asks, reduces the workload of comprehensive survey, observing and controlling and the framing layout of Star Service and telemetering parsing configuration；The present invention improves in ground observing and controlling
In-orbit telemetering programs modification ability on the long guard system fast adaptation star of the heart；The present invention is configured using three-dimensional telemetering, is improved distant
Trackability is surveyed, Tracking Through Telemetry stationkeeping ability, quick position telemetry point and transmission path are enhanced, is checked convenient for problem；The present invention
It can be combined with satellite hub unit semi physical test macro, by star share identical telemetering amount, compared and generated on star
Telemetry frame and the equivalent generation of ground telemetering telemetry frame, complete telemetering closed loop compare, sufficiently verify framing function on star on ground
Energy.
It is discussed in detail although the contents of the present invention have passed through above preferred embodiment, but it should be appreciated that above-mentioned
Description is not considered as limitation of the present invention.After those skilled in the art have read above content, for of the invention
A variety of modifications and substitutions all will be apparent.Therefore, protection scope of the present invention should be limited to the appended claims.
Claims (4)
1. a kind of integrated telemetering configuring management method in star ground, which is characterized in that described method includes following steps: star one
Body frame table configuration file automatically generates, satellite telemetry stratification parsing, the telemetering of the ground of the star based on the equivalent generation of stratification telemetering
Closed loop compares；
The star integrated frame table configuration file automatically generate and include the following steps: the telemetering based on subsystem slave computer tissue
The property relevant constraint at same frame of cell passed down between frequency needs, cell in pack arrangement, packet, based on observing and controlling and Star Service subsystem
Telemetering packet two-dimensional storage management strategy and telemetry frame Partition Mask, it is synchronous generate Star Service framing configuration file, in-orbit telemetering is compiled
Journey infuses number instruction, telemetering archive file and ground telemetering and parses configuration file；
The satellite telemetry stratification parsing includes the following steps: that ground telemetering parsing first is big according to the stratification configuration generated
Table, identification passes down telemetry mode and time division multiplexing counts, and corresponding parsing frame table is selected to decompose whole frame true form according to frame table
At several segments, by the telemetering packet of fragment update to corresponding subcontract layer, and the Flushing status of segment is indicated；Then traversal is each
A telemetering packet completes the parsing of more new segment according to the cells structure table of telemetering packet, more by the telemetering cell amount parsed
Newly to cell layer；The calculating and judgement that telemetering cell is finally completed in cell layer, telemetering physical quantity and judging result are being applied
It is presented on software；
The star based on the equivalent generation of telemetering stratification telemetering closed loop comparison include the following steps: in ground observing and controlling and Star Service
In semi physical test, identical telemetering cell amount by star is shared, ground is generated distant according to the big table of stratification by telemetering cell
Packet is surveyed, telemetry frame is generated by telemetering packet, then compares the telemetry frame that ground generates and the telemetering that star passes up and down, closed loop completes satellite
Telemetering collection and framing functional verification.
2. the integrated telemetering configuring management method in star as described in claim 1 ground, characterized in that the integrated frame in star ground
Table configuration file, which automatically generates, to be included the following steps:
Step 1, each subsystem of satellite provides the cells structure for the telemetering packet that each system generates, and includes three category informations:
(1) information of telemetering cell Physical Quantity Calculation；
(2) property at same frame between telemetering cell requires relevant constraint, is used for multiple cell combinations into inseparable segment；
(3) down biography frequency demand information of the telemetering cell under each telemetry mode；
Software draws a packet telemetering according to the property related constraint at same frame between the whole byte and cell of adjacent continuous cell combination in packet
If being divided into a minimum independent segments；For being multiplexed telemetering packet, the minimum independent segments of telemetering packet should all multiplexings of telemetering packet thus
The maximum union for each minimum independent segments that model split goes out；
For PCM telemetering, associated clip is the minimum unit of framing, and for packet telemetry, telemetering packet is minimum group frame unit, but
Telemetering packet must be able to be the separation of these minimum independent segments across telemetry frame, the cut-point of across frame telemetering packet；
Step 2, the telemetering coating observing and controlling of slave computer tissue and Star Service subsystem are collected and are stored, by Star Service according to corresponding telemetry mode
Frame table from telemetering packet picking frame member, be organized under telemetry frame and pass；For PCM, two-dimensional storage structure is established, stores slave computer
Telemetering packet, if certain telemetering package definition of slave computer is the r row data in two-dimensional storage structure, the then Information locating in this telemetering packet
It can complete to position by (r, c), for the source of each frame member, be described with an initial position (r, c) and frame member length information；
To meet the actual software and hardware telemetering management of satellite, increase and the corresponding attribute information of (r, c) information；For packet telemetry, make
Telemetering Framing unit is indexed with " Bale No.+packet is long ", uses " Bale No.+packet is long " description subpackage frame table that can meet ground parsing need
It asks, to adapt to Star Service framing configuration file, is further added by " Bale No.+packet is long " corresponding Star Service telemetering packet index configurations attribute information；
Step 3, the input information provided based on step 1 and step 2, generates framing basic unit -- frame member, the frame member of PCM system
For the telemetering segment in packet, the frame member of CCSDS subpackage system is telemetering packet；Frame member includes length, source index information；Frame member packet
Under different telemetry modes, with the different requirements of the biography frequency down；
Step 4, there are different telemetry modes different telemetry frames to be multiplexed partitioned mode, according to the division feelings to each section of telemetry frame
Frame member in each telemetering packet is sequentially placed in the telemetry frame section for accordingly passing the frequency down PCM telemetering system by condition,
It is index with (r, c), generates the framing frame table of ground parsing；For packet telemetry system, telemetering packet is evenly distributed on distant
The subpackage area for surveying frame guarantees that the biography interval down of the telemetering packet repeatedly passed down in the systemic circulation period is uniform, generates with " Bale No.+packet
It is long " it is that the telemetering indexed parses frame table；
Step 5, the biography frequency demand down according to the telemetry frame subregion of each mode and telemetering cell under corresponding modes, successively gives birth to
At ground telemetering corresponding under each telemetry mode parsing frame table used；
Step 6, PCM telemetering and packet telemetry have different frame table structure；For PCM telemetering, ground parses frame table using two dimension
Row-column configuration (r, c) mode indexes, and (r, c) has corresponding configuration attribute, and converting Star Service for (r, c) table that ground uses makes
Ram table related pattern, then convert the hex configuration file on satellite for Star Service table, that is, meeting the configuration of satellite PCM frame table makes
With；For packet telemetry, ground frame table uses " Bale No.+packet is long " structure to describe, and each telemetering Bao Jun has the configuration of Star Service framing to belong to
Property, table used in Star Service is converted by ground " Bale No.+packet is long " frame table, then convert hex used on satellite for Star Service table and configure
File meets the configuration of satellite subpackage frame table and uses；
Step 7, the process that parsing frame table in ground is inversely generated by telemetering framing configuration file used on star, by the hex on star
Configuration file is converted into Star Service table, between the frame member index information according to frame meta-attribute information and ground frame table in Star Service table
One-to-one relationship can inversely generate ground telemetering parsing frame table, complete the bumpless transfer of Star Service table and ground frame table；
Step 8, the Star Service frame table configuration file that above step generates, is configured on star in frame table configuration ROM, completes pre- on star
Define the configuration of frame table；
Step 9, after Star Service initialization, the frame table in ROM is loaded into frame table configuration RAM, satellite reads matching in RAM in real time
Framing frame table is set, telemetering framing is completed；
Step 10, telemetry frame table has in-orbit modification ability all or in part, and area is modified for Star Service framing frame table in ground,
According to the note number format of agreement, it is packaged into in-orbit telemetering programming note number instruction；
Step 11, ground sends in-orbit telemetering programming note number instruction, modifies the frame table configured in Star Service RAM, complete frame table
Rail modification；Simultaneously because integration generates management, ground telemetering parses frame table being capable of programming modification on synchronous adaptation star；
Step 12, ground exports the cell parameters processing method file of framing frame table Yu each telemetering packet simultaneously, returns as storage
Shelves and file for future reference reduce the workload of telemetering processing file edit.
3. the integrated telemetering configuring management method in star as described in claim 1 ground, characterized in that the satellite telemetry level
Neutralizing analysis includes the following steps:
Step 1, each slave computer of satellite collects telemetering amount；
Step 2, each slave computer tissue of satellite generates telemetering packet, is sent to Star Service, and Star Service carries out storage management to telemetering packet；
Step 3, according to the telemetry mode of current setting, respective frame table is selected；
Step 4, respective frame table is read from RAM；
Step 5, beat is counted according to corresponding telemetry frame table and multiplexing, telemetering number needed for extracting from telemetering storage management buffer area
According to；
Step 6, Star Service framing module completes the telemetry frame tissue that certain multiplexing under certain telemetry mode counts beat, by whole frame telemetering
Data down transmission；The above process is repeated, completes to pass under being continuously generated of telemetry frame；
Step 7, ground receiver telemetry carries out stratification parsing；The ground parsing frame table for reading corresponding telemetry mode, will be distant
It surveys frame and resolves into discrete segments, segment is distributed to corresponding telemetering packet；For PCM telemetering, by the byte in telemetry frame according to frame
Table (r, c) index, distribution is extremely wrapped at c-th of byte of r, and shows that this byte has refreshed in packet；For packet telemetry, foundation
" Bale No.+packet is long " index frame table refreshes corresponding telemetering package informatin if telemetry frame is resolved into a packet；
Step 8, each telemetering packet is traversed, if information is refreshed in packet, to more new information according to telemetering packet cells structure
Telemetering cell one by one is resolved into table, step-by-step, by telemetering cell true form information update to the corresponding telemetering amount of cell layer.If telemetering packet
There are multiplexings, then according to multiplexed situation, select corresponding telemetering packet cells structure table, take remote measurement and wrap to telemetering cell
It decomposes；
Step 9, it to the telemetering cell of update, is calculated according to the processing method of configuration, obtains the physical quantity of telemetering cell, root
Judge whether physical quantity is abnormal according to the criterion of configuration；
Step 10, the telemetering cell physics parsed is shown, distinguishes real-time telemetry and delayed telemetry amount, and show physics
Measure judging result.
4. the integrated telemetering configuring management method in star as described in claim 1 ground, characterized in that described to be based on telemetering level
With changing the star of equivalent generation telemetering closed loop comparison includes the following steps:
Step 1, in the test of Star Service semi physical, identical telemetering amount is shared to star；The telemetering amount excitation simulated with test equipment is defended
Each slave computer of star generates telemetering packet, or generates telemetering packet, each slave computer or slave computer interface using slave computer interface simulator
Telemetering packet is sent to Star Service and carries out framing by simulator；
Step 2, the telemetering amount of simulation is sent to the cell layer of the big table of stratification by Star Service semi physical test equipment, updates cell layer
Telemetering cell amount；
Step 3, according to the cells structure table of telemetering packet, telemetering packet is generated with the telemetering amount tissue of cell layer；
Step 4, the scheduling according to telemetering group frame pattern and multiplexing time controller, selects respective frame table and corresponding counts beat,
It extracts information in telemetering packet and generates telemetry frame；
Step 5, after the equivalent generation of stratification for completing telemetry frame, telemetry frame is sent to telemetering closed loop comparison module；
Step 6, telemetering closed loop comparison module receives Star Service telemetry frame, and the telemetry frame generated with comparing star completes closing for telemetry frame
Ring compares, and verifies telemetering framing correctness；Stratification parsing is carried out to the telemetry frame that satellite passes down, compares the telemetering letter parsed
Whether first physical quantity is consistent with the telemetering amount of test equipment simulation, verifies the correctness of Star Service framing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910291099.8A CN110175051B (en) | 2019-04-11 | 2019-04-11 | Satellite-ground integrated remote measurement configuration management method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910291099.8A CN110175051B (en) | 2019-04-11 | 2019-04-11 | Satellite-ground integrated remote measurement configuration management method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110175051A true CN110175051A (en) | 2019-08-27 |
| CN110175051B CN110175051B (en) | 2022-03-29 |
Family
ID=67689711
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910291099.8A Active CN110175051B (en) | 2019-04-11 | 2019-04-11 | Satellite-ground integrated remote measurement configuration management method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110175051B (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110391840A (en) * | 2019-09-17 | 2019-10-29 | 中国人民解放军国防科技大学 | Method and system for judging abnormality of telemetry parameters of sun synchronous orbit satellite |
| CN110932929A (en) * | 2019-11-12 | 2020-03-27 | 上海卫星工程研究所 | Method, system and medium for classifying and extracting satellite telemetry packets in CCSDS system |
| CN111126020A (en) * | 2019-12-03 | 2020-05-08 | 航天东方红卫星有限公司 | Tabular autonomous security mode design method and system |
| CN111427685A (en) * | 2020-03-23 | 2020-07-17 | 中国人民解放军国防科技大学 | Space-based network intelligent satellite development system and method based on task requirements |
| CN112910544A (en) * | 2021-02-05 | 2021-06-04 | 上海航天测控通信研究所 | On-orbit configurable satellite-borne L/S frequency band data broadcast distribution system |
| CN112988120A (en) * | 2021-03-12 | 2021-06-18 | 上海卫星工程研究所 | Satellite telemetering downlink scheduling parameter dynamic online binding method and system for Ada language |
| CN113315567A (en) * | 2020-09-30 | 2021-08-27 | 中国科学院微小卫星创新研究院 | Telemetering scheduling method based on two-stage packet system |
| CN113364511A (en) * | 2021-05-11 | 2021-09-07 | 上海卫星工程研究所 | Equilibrium transfer computing method and system based on CCSDS packet telemetry |
| CN113535259A (en) * | 2021-06-28 | 2021-10-22 | 北京国科华路航天科技有限公司 | Configuration method and device for aerospace measurement and control station |
| CN113777928A (en) * | 2021-09-15 | 2021-12-10 | 上海卫星工程研究所 | Thermal control parameter analysis and closed-loop method and system based on burst remote measurement |
| CN113791433A (en) * | 2021-08-18 | 2021-12-14 | 上海卫星工程研究所 | Satellite remote bit error rate test system, test method and system |
| CN115426026A (en) * | 2022-07-29 | 2022-12-02 | 上海卫星工程研究所 | Intensive ground measurement and control test system suitable for satellite constellation parallel test |
| CN116886179A (en) * | 2023-09-07 | 2023-10-13 | 长光卫星技术股份有限公司 | On-orbit satellite telemetry data management and downlink method |
| CN116916192A (en) * | 2023-09-11 | 2023-10-20 | 长光卫星技术股份有限公司 | Satellite telemetry management method based on Beidou short message |
Citations (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7274305B1 (en) * | 2002-10-16 | 2007-09-25 | Carina Technology, Inc. | Electrical utility communications and control system |
| CN101170345A (en) * | 2007-11-30 | 2008-04-30 | 航天东方红卫星有限公司 | An unpacking method for satellite packet remote sensing data |
| CN102520619A (en) * | 2011-11-15 | 2012-06-27 | 上海卫星工程研究所 | General-purpose satellite remote sensing simulator |
| CN103473056A (en) * | 2013-09-06 | 2013-12-25 | 北京控制工程研究所 | Automatic generation method for telemetering configuration files |
| CN104331035A (en) * | 2014-09-30 | 2015-02-04 | 航天东方红卫星有限公司 | Mini-satellite test remote measurement and remote control monitoring system based on service-oriented architecture and method thereof |
| CN104597854A (en) * | 2013-10-30 | 2015-05-06 | 北京临近空间飞行器系统工程研究所 | Automatic interpretation system and automatic interpretation method for telemetry data batch processing |
| CN105490777A (en) * | 2015-11-30 | 2016-04-13 | 上海卫星工程研究所 | Satellite telemetry data outlier elimination pre-processing method |
| CN106295197A (en) * | 2016-08-12 | 2017-01-04 | 上海卫星工程研究所 | High-precision high-frequency rate based on packet telemetry sampling programmable telemetry method |
| CN106330291A (en) * | 2016-08-12 | 2017-01-11 | 上海卫星工程研究所 | Data receiving and transmitting system and method for remote support of satellite tests |
| CN106506058A (en) * | 2016-11-03 | 2017-03-15 | 上海卫星工程研究所 | The remote-control simulated method and system of satellite telemetry |
| CN106991053A (en) * | 2017-04-06 | 2017-07-28 | 上海航天测控通信研究所 | Implementation method based on satellite borne equipment ground test general-purpose platform software |
| CN107222251A (en) * | 2017-05-18 | 2017-09-29 | 上海卫星工程研究所 | With proving ground telemetry exchange method and system in satellite field trial |
| CN107332604A (en) * | 2017-05-16 | 2017-11-07 | 上海卫星工程研究所 | The processing method and processing system of satellite complete period multi-source telemetry |
| CN107561559A (en) * | 2017-07-10 | 2018-01-09 | 上海卫星工程研究所 | Spinning satellite ground test program control device |
| CN107733515A (en) * | 2017-08-31 | 2018-02-23 | 北京空间飞行器总体设计部 | Satellite communication link analysis method under a kind of in-orbit complex environment |
| CN107766444A (en) * | 2017-09-22 | 2018-03-06 | 上海卫星工程研究所 | Cooperate with telemetry intelligence (TELINT) intelligent conversion system star |
| CN107797796A (en) * | 2017-09-25 | 2018-03-13 | 上海卫星工程研究所 | Satellite system state picture editor and display terminal |
| CN108957176A (en) * | 2018-06-20 | 2018-12-07 | 上海卫星工程研究所 | A kind of simulation battle array standard type automated testing method |
| CN109299104A (en) * | 2018-10-26 | 2019-02-01 | 成都国星宇航科技有限公司 | A kind of Telemetry Processing System flying control based on artificial intelligence secondary satellite |
| CN109416648A (en) * | 2016-07-22 | 2019-03-01 | 英特尔公司 | The technology coordinated using remotely-sensed data on-line analysis |
-
2019
- 2019-04-11 CN CN201910291099.8A patent/CN110175051B/en active Active
Patent Citations (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7274305B1 (en) * | 2002-10-16 | 2007-09-25 | Carina Technology, Inc. | Electrical utility communications and control system |
| CN101170345A (en) * | 2007-11-30 | 2008-04-30 | 航天东方红卫星有限公司 | An unpacking method for satellite packet remote sensing data |
| CN102520619A (en) * | 2011-11-15 | 2012-06-27 | 上海卫星工程研究所 | General-purpose satellite remote sensing simulator |
| CN103473056A (en) * | 2013-09-06 | 2013-12-25 | 北京控制工程研究所 | Automatic generation method for telemetering configuration files |
| CN104597854A (en) * | 2013-10-30 | 2015-05-06 | 北京临近空间飞行器系统工程研究所 | Automatic interpretation system and automatic interpretation method for telemetry data batch processing |
| CN104331035A (en) * | 2014-09-30 | 2015-02-04 | 航天东方红卫星有限公司 | Mini-satellite test remote measurement and remote control monitoring system based on service-oriented architecture and method thereof |
| CN105490777A (en) * | 2015-11-30 | 2016-04-13 | 上海卫星工程研究所 | Satellite telemetry data outlier elimination pre-processing method |
| CN109416648A (en) * | 2016-07-22 | 2019-03-01 | 英特尔公司 | The technology coordinated using remotely-sensed data on-line analysis |
| CN106295197A (en) * | 2016-08-12 | 2017-01-04 | 上海卫星工程研究所 | High-precision high-frequency rate based on packet telemetry sampling programmable telemetry method |
| CN106330291A (en) * | 2016-08-12 | 2017-01-11 | 上海卫星工程研究所 | Data receiving and transmitting system and method for remote support of satellite tests |
| CN106506058A (en) * | 2016-11-03 | 2017-03-15 | 上海卫星工程研究所 | The remote-control simulated method and system of satellite telemetry |
| CN106991053A (en) * | 2017-04-06 | 2017-07-28 | 上海航天测控通信研究所 | Implementation method based on satellite borne equipment ground test general-purpose platform software |
| CN107332604A (en) * | 2017-05-16 | 2017-11-07 | 上海卫星工程研究所 | The processing method and processing system of satellite complete period multi-source telemetry |
| CN107222251A (en) * | 2017-05-18 | 2017-09-29 | 上海卫星工程研究所 | With proving ground telemetry exchange method and system in satellite field trial |
| CN107561559A (en) * | 2017-07-10 | 2018-01-09 | 上海卫星工程研究所 | Spinning satellite ground test program control device |
| CN107733515A (en) * | 2017-08-31 | 2018-02-23 | 北京空间飞行器总体设计部 | Satellite communication link analysis method under a kind of in-orbit complex environment |
| CN107766444A (en) * | 2017-09-22 | 2018-03-06 | 上海卫星工程研究所 | Cooperate with telemetry intelligence (TELINT) intelligent conversion system star |
| CN107797796A (en) * | 2017-09-25 | 2018-03-13 | 上海卫星工程研究所 | Satellite system state picture editor and display terminal |
| CN108957176A (en) * | 2018-06-20 | 2018-12-07 | 上海卫星工程研究所 | A kind of simulation battle array standard type automated testing method |
| CN109299104A (en) * | 2018-10-26 | 2019-02-01 | 成都国星宇航科技有限公司 | A kind of Telemetry Processing System flying control based on artificial intelligence secondary satellite |
Non-Patent Citations (4)
| Title |
|---|
| 杨同智 等: ""卫星星地时差测量监控方法研究"", 《宇航计测技术》 * |
| 汪洋 等: ""基于函数解析的卫星测试数据自动判读"", 《遥测遥控》 * |
| 赵蒙等: "一种智能化卫星供配电测试系统设计", 《测控技术》 * |
| 魏冬冬等: "一种姿轨控软件仿真测试平台的遥测解析软件设计与实现", 《电子测试》 * |
Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110391840B (en) * | 2019-09-17 | 2019-12-17 | 中国人民解放军国防科技大学 | Method and system for judging abnormality of telemetry parameters of sun synchronous orbit satellite |
| CN110391840A (en) * | 2019-09-17 | 2019-10-29 | 中国人民解放军国防科技大学 | Method and system for judging abnormality of telemetry parameters of sun synchronous orbit satellite |
| CN110932929A (en) * | 2019-11-12 | 2020-03-27 | 上海卫星工程研究所 | Method, system and medium for classifying and extracting satellite telemetry packets in CCSDS system |
| CN110932929B (en) * | 2019-11-12 | 2021-08-24 | 上海卫星工程研究所 | Method, system and medium for classifying and extracting satellite telemetry packets in CCSDS system |
| CN111126020B (en) * | 2019-12-03 | 2023-09-29 | 航天东方红卫星有限公司 | Method and system for designing tabular autonomous security mode |
| CN111126020A (en) * | 2019-12-03 | 2020-05-08 | 航天东方红卫星有限公司 | Tabular autonomous security mode design method and system |
| CN111427685A (en) * | 2020-03-23 | 2020-07-17 | 中国人民解放军国防科技大学 | Space-based network intelligent satellite development system and method based on task requirements |
| CN111427685B (en) * | 2020-03-23 | 2022-08-23 | 中国人民解放军国防科技大学 | Space-based network intelligent satellite development system and method based on task requirements |
| CN113315567A (en) * | 2020-09-30 | 2021-08-27 | 中国科学院微小卫星创新研究院 | Telemetering scheduling method based on two-stage packet system |
| CN112910544A (en) * | 2021-02-05 | 2021-06-04 | 上海航天测控通信研究所 | On-orbit configurable satellite-borne L/S frequency band data broadcast distribution system |
| CN112910544B (en) * | 2021-02-05 | 2022-11-25 | 上海航天测控通信研究所 | On-orbit configurable satellite-borne L/S frequency band data broadcast distribution system |
| CN112988120A (en) * | 2021-03-12 | 2021-06-18 | 上海卫星工程研究所 | Satellite telemetering downlink scheduling parameter dynamic online binding method and system for Ada language |
| CN113364511A (en) * | 2021-05-11 | 2021-09-07 | 上海卫星工程研究所 | Equilibrium transfer computing method and system based on CCSDS packet telemetry |
| CN113364511B (en) * | 2021-05-11 | 2023-04-07 | 上海卫星工程研究所 | Equilibrium transfer computing method and system based on CCSDS packet telemetry |
| CN113535259A (en) * | 2021-06-28 | 2021-10-22 | 北京国科华路航天科技有限公司 | Configuration method and device for aerospace measurement and control station |
| CN113791433A (en) * | 2021-08-18 | 2021-12-14 | 上海卫星工程研究所 | Satellite remote bit error rate test system, test method and system |
| CN113791433B (en) * | 2021-08-18 | 2024-04-02 | 上海卫星工程研究所 | Satellite telemetry bit error rate test system and test method |
| CN113777928A (en) * | 2021-09-15 | 2021-12-10 | 上海卫星工程研究所 | Thermal control parameter analysis and closed-loop method and system based on burst remote measurement |
| CN115426026A (en) * | 2022-07-29 | 2022-12-02 | 上海卫星工程研究所 | Intensive ground measurement and control test system suitable for satellite constellation parallel test |
| CN115426026B (en) * | 2022-07-29 | 2024-03-12 | 上海卫星工程研究所 | Intensive ground measurement and control test system suitable for satellite constellation parallel test |
| CN116886179A (en) * | 2023-09-07 | 2023-10-13 | 长光卫星技术股份有限公司 | On-orbit satellite telemetry data management and downlink method |
| CN116886179B (en) * | 2023-09-07 | 2023-12-01 | 长光卫星技术股份有限公司 | On-orbit satellite telemetry data management and downlink method |
| CN116916192A (en) * | 2023-09-11 | 2023-10-20 | 长光卫星技术股份有限公司 | Satellite telemetry management method based on Beidou short message |
| CN116916192B (en) * | 2023-09-11 | 2023-12-01 | 长光卫星技术股份有限公司 | Satellite telemetry management method based on Beidou short message |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110175051B (en) | 2022-03-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110175051A (en) | The integrated telemetering configuring management method in star ground | |
| CN102750406B (en) | Multi-version management method for model set and difference model-based power grid model | |
| CN101272051B (en) | Information system integration method of electric network production control region and management information region | |
| CN107330056B (en) | Wind power plant SCADA system based on big data cloud computing platform and operation method thereof | |
| CN107292003A (en) | A kind of automatic generating method of electric network station wiring diagram | |
| CN105279144B (en) | A kind of composition method and device of wind tunnel test data text file | |
| CN106960103A (en) | The automatic generation method and device of a kind of grid graph | |
| CN103577926B (en) | A kind of method that realizes the calculating in real time of large scale electric network theory wire loss and high accuracy | |
| CN106445987B (en) | The building of CIR geographic information database and verification method | |
| CN110460076A (en) | The automatic checkout system and method for grid side energy storage Monitor Process control system | |
| CN107545085A (en) | A kind of transformer station process layer network Mating graph automatic generation method | |
| CN109992571A (en) | A kind of intelligent substation configuration file line closed loop check system and method for calibration | |
| CN108763399A (en) | It is a kind of to be suitable for the power distribution network multi-source data modeling method containing D-PMU | |
| CN102243676A (en) | Three-level modeling method of new energy comprehensive monitoring system | |
| CN116260720A (en) | Network resource deployment method and device, electronic equipment and storage medium | |
| CN116526667B (en) | Secondary fusion distribution network feeder terminal system based on current Internet of things feedback mechanism | |
| KR100987167B1 (en) | Multiple FACTS control system and method therefor | |
| CN108183869A (en) | A kind of electric quantity data acquisition system based on Distributed Message Queue | |
| CN106909529A (en) | A kind of Machine learning tools middleware and machine learning training method | |
| CN106126406A (en) | A kind of generation method and device applying daily paper | |
| CN110346661A (en) | A kind of method and system of user's electric voltage exception automatic detecting | |
| CN107273574A (en) | A kind of power transmission network automatic mapping technology that system is dispatched based on D5000 | |
| CN110011301B (en) | Provincial power grid online dynamic partitioning method | |
| CN103488726A (en) | Method for establishing unified grid data platform based on WEB-SERVICE | |
| CN107944005A (en) | A kind of method for exhibiting data and device |
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 |