CN107911157A - Utility Satellite command automation technical data processing system and method - Google Patents
Utility Satellite command automation technical data processing system and method Download PDFInfo
- Publication number
- CN107911157A CN107911157A CN201710876497.7A CN201710876497A CN107911157A CN 107911157 A CN107911157 A CN 107911157A CN 201710876497 A CN201710876497 A CN 201710876497A CN 107911157 A CN107911157 A CN 107911157A
- Authority
- CN
- China
- Prior art keywords
- satellite
- telemetry
- command automation
- data processing
- module
- 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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18519—Operations control, administration or maintenance
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Radio Relay Systems (AREA)
- Selective Calling Equipment (AREA)
Abstract
The invention discloses a kind of Utility Satellite command automation technical data processing system and method, which includes：For the data conversion module for receiving cosmodrome TT＆C Management center telemetry and changing, the satellite telemetry demodulated equipment analog module of telemetering channel, remote measurement processing module for receiving, handling satellite test system multicast telemetry etc. are established for analog satellite telemetry demodulation equipment and satellite test system.The present invention can solve the versatility of Satellite Command automatic technology data handling system, the present invention has re-started combing for the command automation technical protocol of current all cosmodromes, function according to system carries out Module Division to it, corresponding submodule is built to the discrepant part of three firing bases, main processing block calls the processing submodule in specified base according to the configuration of user, and the versatility of system is realized with this.
Description
Technical field
The present invention relates to a kind of satellite data process field, more particularly to a kind of Utility Satellite command automation technology number
According to processing system and method.
Background technology
With the fast development of China's S＆T tax, space flight, the development of national defense system and launch mission are more and more, task
Cycle is more and more tighter, and satellite is gone to after the test phase of launching site to be needed also to get over to the rapid deployment ability of satellite ground test system
Come more urgent, generalization is currently that developing direction is carried forward vigorously in satellite test field, for complicated in satellite ground test system
Position carry out generalization and be transformed into for a hot spot of ground testing system upgrading, at Satellite Command automatic technology data
Reason system is the unique interface of firing base command automation technological system and satellite test system, carries Data Collection, place
Reason and the effect sent, are information transferring systems necessary to satellite is tested and launched at launching site, for different model
Satellite, due to the difference of firing base command automation technological system, the difference of satellite test system and satellite test system
The difference of information protocol between the information system of launching site, result in for each satellite to be launched, will spend a large amount of
Manpower and materials build again, debug the supporting command automation technical data processing system of this model satellite, the present invention is just
It is a kind of Utility Satellite command automation technical data processing system and method to solve the above-mentioned problems, currently without discovery
The explanation or report of similar correlation technique, are also not yet collected into data similar both at home and abroad.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of Utility Satellite command automation technical data processing system
And method, it can solve the versatility of Satellite Command automatic technology data handling system, and the present invention is defended for all at present
The command automation technical protocol of star firing base has re-started combing, and the function according to system carries out Module Division to it,
Corresponding submodule is built to the discrepant part of three firing bases, main processing block calls specified base according to the configuration of user
The processing submodule on ground, the versatility of system is realized with this.
The present invention is to solve above-mentioned technical problem by following technical proposals：A kind of Utility Satellite command automation skill
Art data handling system, the Utility Satellite command automation technical data processing system include：
Data conversion module：For receiving cosmodrome TT＆C Management center telemetry and changing；
Satellite telemetry demodulated equipment analog module：Telemetry frame data processing after data conversion module is handled is distant for satellite
The telemetry format that demodulated equipment is arranged with reflecting software in satellite test system is surveyed, and the company of reflecting software is waited as server-side
Connecing, telemetry is sent after successful connection, telemetry is no different all the way with satellite telemetry demodulated equipment for reflecting software,
Telemetering channel is established for analog satellite telemetry demodulation equipment and satellite test system；
Remote measurement processing module：The comprehensive multicast packet surveyed server and sent in satellite test system is received, and is matched somebody with somebody according to user
The remote measurement code name put, extracts the handling result and state of corresponding code name, for receiving, handling satellite test system from multicast packet
System multicast telemetry；
Base framing module：The module includes the framing mode of three firing bases, and primary module is called according to user configuration
Corresponding base processing submodule, each submodule are handled according to the remote measurement that command automation technical protocol extracts remote measurement processing module
As a result repack framing and send, for concern remote measurement code name again framing；
Link monitoring module：Link monitoring passage is established between the module and firing base command automation technological system,
And every 0.5 second sends heartbeat data, for monitoring and firing base command automation technology link stability；
Module is locally stored：The telemetry and framing module that storage Satellite TT administrative center sends are sent to transmitting base
Telemetry after the framing of ground command automation technological system, for real-time storage telemetry.
The another aspect of the object of the invention, there is provided a kind of Utility Satellite command automation technical data processing method is general
Satellite Command automatic technology data processing method comprises the following steps：
Step 1, command automation technical data processing system carry out Initialize installation according to configuration file；
Step 2, the remote measurement number of Satellite TT administrative center transmission is received from firing base command automation technological system
According to being converted into satellite system standard telemetry format；
Step 3, the form by the telemetry after conversion according to observing and controlling modulation /demodulation baseband equipment in satellite test system
Packing, and send to the reflecting software in satellite test system；
Step 4, receives the comprehensive remote measurement handling result data surveyed server multicast and sent, foundation in satellite test system and matches somebody with somebody
Put and require therefrom to extract the telemetry intelligence (TELINT) of concern, and press firing base command automation technological system protocol conventions, to remote measurement into
Row framing again, sends to firing base command automation technological system after the completion of framing；
Step 5, in command automation technical data processing system operational process with firing base command automation technology system
Link monitoring passage is established between system, the system timing sends heartbeat data, confirms that intercommunication keeps normal；
Step 6, can preserve in command automation technical data processing system operational process from Satellite TT management in real time
The received telemetry of the heart and telemetry after the framing of base command automation technological system is sent to, gives later stage malfunction elimination
Data ma-terial support is provided.
Preferably, deployment of the command automation technical data processing system for the working environment of obstructed satellite model
Mainly to the modification of configuration text file, by changing the information in configuration file, to reach modification command automation technology
The purpose of configuration.
Preferably, the interface of the command automation technical data processing system and standard satellite test system realizes system
One, command automation technical data processing system is adapted to current standard satellite test system；During satellite launch site is tested,
Great tune will not be caused to original test system by introducing command automation technical data processing system in satellite ground test system
It is whole, it ensure that the robustness and stability of whole ground testing system.
Preferably, difference has been respectively created for different firing bases in the command automation technical data processing system
Base framing submodule, primary module can call the processing submodule in corresponding base according to the configuration of user, whole to realize with this
The versatility of a system, command automation technical data processing system are suitable for current all cosmodromes.
The positive effect of the present invention is：The use of the present invention while compatible all cosmodromes at present, solution
The generalization process problem for each base command automation technical data of having determined, it is allowed to which user is by changing configuration file to each model
Matching setting is carried out in each base, substantially increases testing efficiency, has saved system research and development cost.
Brief description of the drawings
Fig. 1 is the structure diagram of Utility Satellite command automation technical data processing system of the present invention.
Fig. 2 is Utility Satellite command automation technical data process flow figure of the present invention.
Embodiment
Present pre-ferred embodiments are provided below in conjunction with the accompanying drawings, with the technical solution that the present invention will be described in detail.
As shown in Figure 1, Utility Satellite command automation technical data processing system of the present invention includes：
Data conversion module：For receiving cosmodrome TT＆C Management center telemetry and changing；
Satellite telemetry demodulated equipment analog module：Telemetry frame data processing after data conversion module is handled is distant for satellite
The telemetry format that demodulated equipment is arranged with reflecting software in satellite test system is surveyed, and the company of reflecting software is waited as server-side
Connecing, telemetry is sent after successful connection, telemetry is no different all the way with satellite telemetry demodulated equipment for reflecting software,
Telemetering channel is established for analog satellite telemetry demodulation equipment and satellite test system；
Remote measurement processing module：The comprehensive multicast packet surveyed server and sent in satellite test system is received, and is matched somebody with somebody according to user
The remote measurement code name put, extracts the handling result and state of corresponding code name, for receiving, handling satellite test system from multicast packet
System multicast telemetry；
Base framing module：The module includes the framing mode of three firing bases, and primary module is called according to user configuration
Corresponding base processing submodule, each submodule are handled according to the remote measurement that command automation technical protocol extracts remote measurement processing module
As a result repack framing and send, for concern remote measurement code name again framing；
Link monitoring module：Link monitoring passage is established between the module and firing base command automation technological system,
And every 0.5 second sends heartbeat data, for monitoring and firing base command automation technology link stability；
Module is locally stored：The telemetry and framing module that storage Satellite TT administrative center sends are sent to transmitting base
Telemetry after the framing of ground command automation technological system, for real-time storage telemetry.
As shown in Fig. 2, Utility Satellite command automation technical data processing method of the present invention comprises the following steps：
Step 1, command automation technical data processing system carry out Initialize installation according to configuration file；
Step 2, the remote measurement number of Satellite TT administrative center transmission is received from firing base command automation technological system
According to being converted into satellite system standard telemetry format；
Step 3, the form by the telemetry after conversion according to observing and controlling modulation /demodulation baseband equipment in satellite test system
Packing, and send to the reflecting software in satellite test system；
Step 4, receives the comprehensive remote measurement handling result data surveyed server multicast and sent, foundation in satellite test system and matches somebody with somebody
Put and require therefrom to extract the telemetry intelligence (TELINT) of concern, and press firing base command automation technological system protocol conventions, to remote measurement into
Row framing again, sends to firing base command automation technological system after the completion of framing；
Step 5, in command automation technical data processing system operational process with firing base command automation technology system
Link monitoring passage is established between system, the system timing sends heartbeat data, confirms that intercommunication keeps normal；
Step 6, can preserve in command automation technical data processing system operational process from Satellite TT management in real time
The received telemetry of the heart and telemetry after the framing of base command automation technological system is sent to, gives later stage malfunction elimination
Data ma-terial support is provided.
The command automation technical data processing system is mainly for the deployment of working environment of obstructed satellite model
Modification to configuration text file, by changing the information in configuration file, to reach modification command automation technical configuration
Purpose.
The interface of the command automation technical data processing system and standard satellite test system realizes unification, commander
Automatic technology data handling system is adapted to current standard satellite test system；During satellite launch site is tested, in satellite
Ground testing system, which introduces command automation technical data processing system, to cause Important Adjustment to original test system, ensure
The robustness and stability of whole ground testing system.
Different bases has been respectively created for different firing bases in the command automation technical data processing system
Framing submodule, primary module can call the processing submodule in corresponding base according to the configuration of user, and whole system is realized with this
Versatility, command automation technical data processing system is suitable for current all cosmodromes.
In conclusion the present invention can solve the versatility of Satellite Command automatic technology data handling system, the present invention
Combing is re-started for the command automation technical protocol of current all cosmodromes, the function according to system is to it
Module Division is carried out, corresponding submodule is built to the discrepant part of three firing bases, main processing block is matched somebody with somebody according to user's
Put to call the processing submodule in specified base, the versatility of system is realized with this.
Particular embodiments described above, technical problem, technical solution and the beneficial effect of the solution to the present invention carry out
It is further described, it should be understood that the foregoing is merely the specific embodiment of the present invention, is not limited to
The present invention, within the spirit and principles of the invention, any modification, equivalent substitution, improvement and etc. done, should be included in this
Within the protection domain of invention.
Claims (5)
1. a kind of Utility Satellite command automation technical data processing system, it is characterised in that the Utility Satellite commander is automatic
Changing technical data processing system includes：
Data conversion module：For receiving cosmodrome TT＆C Management center telemetry and changing；
Satellite telemetry demodulated equipment analog module：Telemetry frame data processing after data conversion module is handled is satellite telemetry solution
The telemetry format of equipment and reflecting software agreement in satellite test system is adjusted, and the connection of reflecting software is waited as server-side,
Telemetry is sent after successful connection, telemetry is no different all the way with satellite telemetry demodulated equipment for reflecting software, is used
Telemetering channel is established in analog satellite telemetry demodulation equipment and satellite test system；
Remote measurement processing module：The comprehensive multicast packet surveyed server and sent in satellite test system is received, and according to user configuration
Remote measurement code name, extracts the handling result and state of corresponding code name from multicast packet, for receiving, handling satellite test system group
Broadcast telemetry；
Base framing module：The module includes the framing mode of three firing bases, and primary module calls corresponding according to user configuration
Base handles submodule, the remote measurement handling result that each submodule extracts remote measurement processing module according to command automation technical protocol
Repack framing and send, for concern remote measurement code name again framing；
Link monitoring module：Link monitoring passage is established between the module and firing base command automation technological system, and often
Heartbeat data is sent within 0.5 second, for monitoring and firing base command automation technology link stability；
Module is locally stored：The telemetry and framing module that storage Satellite TT administrative center sends are sent to firing base and refer to
The telemetry after the framing of automatic technology system is waved, for real-time storage telemetry.
A kind of 2. Utility Satellite command automation technical data processing method, it is characterised in that Utility Satellite command automation skill
Art data processing method comprises the following steps：
Step 1, command automation technical data processing system carry out Initialize installation according to configuration file；
Step 2, the telemetry of Satellite TT administrative center transmission is received from firing base command automation technological system, will
It is converted to satellite system standard telemetry format；
Step 3, the telemetry after conversion is beaten according to the form of observing and controlling modulation /demodulation baseband equipment in satellite test system
Bag, and send to the reflecting software in satellite test system；
Step 4, receives the comprehensive remote measurement handling result data surveyed server multicast and sent in satellite test system, will according to configuration
The telemetry intelligence (TELINT) for therefrom extracting concern is sought, and presses firing base command automation technological system protocol conventions, weight is carried out to remote measurement
New framing, sends to firing base command automation technological system after the completion of framing；
Step 5, in command automation technical data processing system operational process with firing base command automation technological system it
Between establish link monitoring passage, the system timing sends heartbeat data, confirms that intercommunication keeps normal；
Step 6, can in real time preserve in command automation technical data processing system operational process and be received from Satellite TT administrative center
To telemetry and be sent to telemetry after the framing of base command automation technological system, give later stage malfunction elimination to provide
Data ma-terial supports.
3. Utility Satellite command automation technical data processing method as claimed in claim 2, it is characterised in that the commander
Automatic technology data handling system is mainly to configuration text file for the deployment of the working environment of obstructed satellite model
Modification, by changing the information in configuration file, to achieve the purpose that to change command automation technical configuration.
4. Utility Satellite command automation technical data processing method as claimed in claim 2, it is characterised in that the commander
The interface that automatic technology data handling system tests system with a standard satellite realizes unification, command automation technology number
Current standard satellite test system is adapted to according to processing system；During satellite launch site is tested, system is tested in satellite ground
Important Adjustment will not be caused to original test system by introducing command automation technical data processing system, ensure that whole ground is surveyed
The robustness and stability of test system.
5. Utility Satellite command automation technical data processing method as claimed in claim 2, it is characterised in that the commander
Different base framing submodules, primary module has been respectively created for different firing bases in automatic technology data handling system
The processing submodule in corresponding base can be called according to the configuration of user, the versatility of whole system is realized with this, commander is automatic
Change technical data processing system and be suitable for current all cosmodromes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710876497.7A CN107911157B (en) | 2017-09-25 | 2017-09-25 | Universal satellite command automation technology data processing system and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710876497.7A CN107911157B (en) | 2017-09-25 | 2017-09-25 | Universal satellite command automation technology data processing system and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107911157A true CN107911157A (en) | 2018-04-13 |
| CN107911157B CN107911157B (en) | 2020-07-14 |
Family
ID=61840245
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710876497.7A Active CN107911157B (en) | 2017-09-25 | 2017-09-25 | Universal satellite command automation technology data processing system and method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107911157B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112994784A (en) * | 2021-04-26 | 2021-06-18 | 北京航天驭星科技有限公司 | Method for receiving satellite telemetering data and method for sending instruction to satellite |
| CN113993003A (en) * | 2021-09-18 | 2022-01-28 | 深圳航天东方红卫星有限公司 | Multi-satellite parallel data forwarding system and method |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102520619A (en) * | 2011-11-15 | 2012-06-27 | 上海卫星工程研究所 | General-purpose satellite remote sensing simulator |
| CN103412540A (en) * | 2013-08-09 | 2013-11-27 | 中国空间技术研究院 | Communication satellite simulator and general telemetry and telecontrol stream data transmission method |
| CN103957134A (en) * | 2014-04-22 | 2014-07-30 | 航天恒星科技有限公司 | Modular configurable telemetry parameter analyzing and processing system |
| KR101505139B1 (en) * | 2013-12-30 | 2015-03-24 | 한국항공우주연구원 | Telemetry frame generating method and satelite monitoring method by the same |
| CN104618311A (en) * | 2013-11-05 | 2015-05-13 | 中国空间技术研究院 | Telecommand data conversion method |
| CN104618171A (en) * | 2013-11-05 | 2015-05-13 | 中国空间技术研究院 | Telemetry data conversion method |
| CN105897504A (en) * | 2016-03-30 | 2016-08-24 | 上海卫星工程研究所 | Satellite universal testing system data interaction method and system |
| 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 |
| CN107168282A (en) * | 2017-05-19 | 2017-09-15 | 上海卫星工程研究所 | Utility Satellite observing and controlling test system and method |
-
2017
- 2017-09-25 CN CN201710876497.7A patent/CN107911157B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102520619A (en) * | 2011-11-15 | 2012-06-27 | 上海卫星工程研究所 | General-purpose satellite remote sensing simulator |
| CN103412540A (en) * | 2013-08-09 | 2013-11-27 | 中国空间技术研究院 | Communication satellite simulator and general telemetry and telecontrol stream data transmission method |
| CN104618311A (en) * | 2013-11-05 | 2015-05-13 | 中国空间技术研究院 | Telecommand data conversion method |
| CN104618171A (en) * | 2013-11-05 | 2015-05-13 | 中国空间技术研究院 | Telemetry data conversion method |
| KR101505139B1 (en) * | 2013-12-30 | 2015-03-24 | 한국항공우주연구원 | Telemetry frame generating method and satelite monitoring method by the same |
| CN103957134A (en) * | 2014-04-22 | 2014-07-30 | 航天恒星科技有限公司 | Modular configurable telemetry parameter analyzing and processing system |
| CN105897504A (en) * | 2016-03-30 | 2016-08-24 | 上海卫星工程研究所 | Satellite universal testing system data interaction method and system |
| 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 |
| CN107168282A (en) * | 2017-05-19 | 2017-09-15 | 上海卫星工程研究所 | Utility Satellite observing and controlling test system and method |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112994784A (en) * | 2021-04-26 | 2021-06-18 | 北京航天驭星科技有限公司 | Method for receiving satellite telemetering data and method for sending instruction to satellite |
| CN112994784B (en) * | 2021-04-26 | 2021-09-17 | 北京航天驭星科技有限公司 | Method for receiving satellite telemetering data and method for sending instruction to satellite |
| CN113993003A (en) * | 2021-09-18 | 2022-01-28 | 深圳航天东方红卫星有限公司 | Multi-satellite parallel data forwarding system and method |
| CN113993003B (en) * | 2021-09-18 | 2023-12-26 | 深圳航天东方红卫星有限公司 | Multi-satellite parallel data forwarding system and method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107911157B (en) | 2020-07-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106538037A (en) | Wireless bearer configuration method, device and system | |
| CN107967801A (en) | A kind of energy measurement data online acquisition and monitoring method and system | |
| CN107911157A (en) | Utility Satellite command automation technical data processing system and method | |
| CN101978720A (en) | Method of network management by assistance from terminal using control-plane signaling between terminal and network | |
| CN103825761A (en) | On-board router simulation method of delay-tolerant network | |
| CN102014464B (en) | Method for synchronously processing networks in wireless MESH network | |
| CN106487575A (en) | A kind of communication module batch upgrading method based on power line communication | |
| CN101909010B (en) | Port configuration method and device as well as switcher equipment | |
| CN106160852B (en) | A kind of network system and its remote upgrade method of transmission device | |
| CN105897504B (en) | Satellite General test macro data interactive method and system | |
| CN113722013A (en) | Data exchange method suitable for Beidou third-satellite measurement, operation and control system | |
| CN106936658A (en) | The method of testing and test platform of test case, simulation test equipment | |
| CN101227335A (en) | Method for upgrading software version of network cell device | |
| CN107222251A (en) | With proving ground telemetry exchange method and system in satellite field trial | |
| CN107329738A (en) | Component update method and device | |
| CN102857890A (en) | Monitoring method for self-adaptation between electric power tunnel text messages and wireless network communication | |
| CN102843156A (en) | Digital microwave distributed type transmitting system and digital microwave distributed type transmitting method | |
| CN102710447A (en) | Cloud repairing method and system of terminal device | |
| CN106849349A (en) | A kind of sun square formation simulator developing Of Remote Control Power frame system | |
| CN116708475A (en) | Multi-station multi-seat software remote synchronization method and system | |
| CN102801435B (en) | A kind of C being applicable to moonlet launching site and using 3i system | |
| CN101150545B (en) | A data distribution method multi-module data configuration of media gateway | |
| CN106210107A (en) | Animal heat acquisition method and system | |
| CN113993003A (en) | Multi-satellite parallel data forwarding system and method | |
| CN103746887A (en) | Method for activating locomotive access network |
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 |