CN108923840A - The in-orbit monitoring information alarm information pushing system of satellite - Google Patents
The in-orbit monitoring information alarm information pushing system of satellite Download PDFInfo
- Publication number
- CN108923840A CN108923840A CN201810670982.3A CN201810670982A CN108923840A CN 108923840 A CN108923840 A CN 108923840A CN 201810670982 A CN201810670982 A CN 201810670982A CN 108923840 A CN108923840 A CN 108923840A
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- China
- Prior art keywords
- satellite
- alarm
- information
- orbit
- orbit monitoring
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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
-
- 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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L41/00—Arrangements for maintenance, administration or management of data switching networks, e.g. of packet switching networks
- H04L41/06—Management of faults, events, alarms or notifications
- H04L41/0631—Management of faults, events, alarms or notifications using root cause analysis; using analysis of correlation between notifications, alarms or events based on decision criteria, e.g. hierarchy, tree or time analysis
Abstract
The invention discloses a kind of in-orbit monitoring information alarm information pushing systems of satellite, its alarm for including multiple types and cue module, open interface module, warning message check module, the alarm of multiple types and cue module are for sound, text, short message and DESKTOP INFORMATION push, the data communication interface of open interface module is realized using dynamic link library, warning message checks that module includes that text mode is checked, provides the inquiry of historical data, supports more satellite modes and single satellite mode.The in-orbit monitoring information alarm information pushing system of satellite of the present invention, which solves in-orbit monitoring personnel in existing in-orbit monitoring technology, to notify design of satellites teacher for satellite warning message and fault message in time, satellite surveillance system more than one is provided by in-orbit monitoring information alert monitoring system for satellite monitoring personnel, relative alarm information can be issued simultaneously in time, improve exception and the timeliness and accuracy of alert notice in the in-orbit monitoring of satellite.
Description
Technical field
The present invention relates to a kind of alarm information pushing systems, more particularly to a kind of in-orbit monitoring information warning message of satellite
Supplying system.
Background technique
Satellite model task is increasing, to in-orbit monitoring the judging automatically of satellite telemetry information, automatic alarm, automatic
More stringent requirements are proposed for notice.Unmanned carry out satellitosis notice on duty, automatic has become the in-orbit monitoring of satellite
Development trend.Automatic satellite interpretation, alarm and notice device have become an important composition of the in-orbit system Construction of satellite
Part.
After satellite in orbit completes failure and condition diagnosing, need to remind satellite monitoring people in time after satellite is alarmed
Member notifies satellite relevant design personnel as early as possible.The prior art can not in time be accused satellite warning message by way of acousto-optic-electric
Know satellite monitoring personnel, lacks and call automatic short message notice device notice relevant design teacher, by being mounted in designer's computer
Desktop pushing software by alarm information pushing to the technological means of relevant design teacher, cause waste of human resource, satellite exists
The problem of rail fault discovery time increases.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of in-orbit monitoring information alarm information pushing system of satellite,
Solving in-orbit monitoring personnel in existing in-orbit monitoring technology can not notify to defend in time by satellite warning message and fault message in time
Star designer provides satellite surveillance system more than one by in-orbit monitoring information alert monitoring system for satellite monitoring personnel, together
When relative alarm information can be issued in time, improve in the in-orbit monitoring of satellite exception and the timeliness of alert notice and accurate
Property.
The present invention is to solve above-mentioned technical problem by following technical proposals：A kind of in-orbit monitoring information alarm of satellite
Information transmission system comprising the alarm of multiple types and cue module, open interface module, warning message check module, more
The alarm of type and cue module are for sound, text, short message and DESKTOP INFORMATION push, the data communication of open interface module
Interface realizes that warning message checks that module includes that text mode is checked, provides the inquiry of historical data using dynamic link library, supports
More satellite modes and single satellite mode.
Preferably, the alarm of the multiple types and cue module are using four kinds of sound, text, short message and DESKTOP INFORMATION push
Mode carries out alarm and failure push, and the combination prompt of diversified forms warning message improves prompt effect.
Preferably, sound push is to use apparent sound to be prompted after alarm and failure occurs, and right
Warning message carries out text casting；Text push is prompted using text flashing and conspicuous color notation methods；Short message push
It is after being confirmed as failure, by calling automatic short message to send platform according to the short message for carrying out different personnel with fault type of alarming
It sends；DESKTOP INFORMATION push is to send pushed information to the computer of designer by unilateral network Transmission system, passes through desktop bullet
The form of window prompts designer.
Preferably, the dynamic link library avoids redesigning alarm information pushing system after newly increasing alarm source,
It only needs to be designed dynamic link library, the data protocol requirements of alarm information pushing system can be met, alarming
Corresponding dynamic link library is configured in information transmission system, when reducing new diagnostic center access system caused by exploitation
Amount, it is characterised in that the uniformity and reliability for increasing alarm information pushing system using dynamic link library, when external alert source
When upgrading, without redesigning alarm information pushing system, system reliability is provided.
Preferably, single satellite operation mode is concerned about some satellite suitable for designer, is divided for some satellite
Analysis；More satellite operation modes are directed to the in-orbit monitoring personnel of satellite, to solve the demand of more stars while monitoring, while being more satellites point
Analysis provides a kind of possibility.
Preferably, more satellite modes and single satellite mode realize cutting for two kinds of operating modes by the way of configuration
It changes.
The positive effect of the present invention is that：The in-orbit monitoring information alarm information pushing system of satellite of the present invention solves existing
There is in-orbit monitoring personnel in in-orbit monitoring technology satellite warning message and fault message not notified design of satellites in time in time
Teacher provides satellite surveillance system more than one by in-orbit monitoring information alert monitoring system for satellite monitoring personnel, while can
Relative alarm information is issued in time, improves exception and the timeliness and accuracy of alert notice in the in-orbit monitoring of satellite.
Detailed description of the invention
Fig. 1 is the embodiment composition schematic diagram of the in-orbit monitoring information alarm information pushing system of satellite of the present invention.
Fig. 2 is the information flow chart of the embodiment of the in-orbit monitoring information alarm information pushing system of satellite of the present invention.
Specific embodiment
Present pre-ferred embodiments are provided with reference to the accompanying drawing, in order to explain the technical scheme of the invention in detail.
As depicted in figs. 1 and 2, the in-orbit monitoring information alarm information pushing system of satellite of the present invention includes the alarm of multiple types
Check that module, the alarm of multiple types and cue module are used for sound, text with cue module, open interface module, warning message
Word, short message and DESKTOP INFORMATION push, open interface module is by data communication interface using dynamic link library realization, warning message
It checks that module includes that text mode is checked, provides the inquiry of historical data, supports more satellite modes and single satellite mode.
More satellite modes and single satellite mode realize the switching of two kinds of operating modes so that it is convenient to make by the way of configuration
With.
The alarm of multiple types and cue module push four kinds of modes using sound, text, short message and DESKTOP INFORMATION and are reported
Alert and failure push, diversified forms warning message combination prompt, improves prompt effect.
Sound push is to be prompted after alarm and failure occurs using apparent sound, and carry out to warning message
Text casting；Text push is prompted using text flashing and conspicuous color notation methods；Short message push is to work as to be confirmed as event
After barrier, sent by calling automatic short message to send platform according to the short message that alarm and fault type carry out different personnel；Desktop letter
Breath push is to send pushed information to the computer of designer by unilateral network Transmission system, is prompted by way of desktop pop-up
Designer.
Dynamic link library avoids redesigning alarm information pushing system after newly increasing alarm source, it is only necessary to dynamic
Chained library is designed, and can meet the data protocol requirements of alarm information pushing system, in alarm information pushing system
The corresponding dynamic link library of middle configuration, when reducing new diagnostic center access system caused by exploitation amount, feature exists
It is not necessarily in the uniformity and reliability that increase alarm information pushing system using dynamic link library when the upgrading of external alert source
Alarm information pushing system is redesigned, system reliability is provided.
Single satellite operation mode is suitable for designer and is concerned about some satellite, is analyzed for some satellite；More satellite works
Operation mode is directed to the in-orbit monitoring personnel of satellite, to solve the demand of more stars while monitoring, while providing one kind for the analysis of more satellites
It may.
The particularity of the characteristics of present invention is monitored according to satellite in orbit and in-orbit monitoring data alarm information pushing system,
Other than having in-orbit data real-time monitoring ability, additionally it is possible to carry out on-orbit fault alarm by sound and image mode, improve
The timeliness of the in-orbit monitoring fault discovery of satellite；The present invention can receive satellite telemetry information and fault diagnosis as a result, root
According to type of alarm to the warning note of different designs Shi Jinhang short message and desktop message mode, the discovery energy of satellite failure is improved
Power.The opening of interface is good in design simultaneously, can receive different types of alarm and fault message；The present invention is suitable for defending more
Star monitoring can realize that unit/terminal monitors and check simultaneously the warning message of different satellites, can also adopt by way of configuring
With unit/terminal, only emphasis monitors and checks the warning message of a certain particular satellite.
In specific embodiment as depicted in figs. 1 and 2, the in-orbit monitoring information alarm information pushing system of satellite of the present invention
It is main to check module comprising alarm and cue module, open interface module, warning message.Wherein alarm and cue module include
Failure message release terminal, failure push desktop terminal；Open interface module is collected eventually using the failure of open interface
End；Warning message checks that module includes data storage terminal and malfunction coefficient inquiry terminal.
Data storage terminal is the storage center of whole system, is the interface layer of database and upper layer application service, mainly
For storing the warning message and fault message that receive.It is that failure collects terminal to the main external interface of application layer, is used
It is accessed in warning message, the interface to database is mainly read-write and the query interface to database, and upper layer request is converted into
The operation of sql like language progress database.
Failure collects the data center that terminal is whole system, receives on-orbit fault diagnostic center and telemetering analytical center
Telemetry is extracted warning message and fault message therein, is stored that data in data storage terminal, while in real time
Information tissue is sent to malfunction coefficient terminal progress information to show, while according to different passing of satelline message release terminals and table
Face pushes terminal and carries out information publication, while inquiring terminal for malfunction coefficient and providing subsequent query interface.
Malfunction coefficient inquiry terminal is that the in-orbit management operator on duty of satellite carries out on-orbit fault and the monitoring of warning message is whole
The real-time and ex-post analysis and inquiry terminal of end and whole system, are the man-machine interfaces of whole system.By the terminal to whole
The state of a data alarm system is monitored that the alarm and exception to all satellite in orbit monitor, after alarming
It is prompted using modes such as sound, image and texts.It simultaneously can be in the failure and alarm progress satellite occurred afterwards
Inquiry and analysis.The terminal as failure collect terminal client, receive corresponding warning message and shown, and according to
Family request carries out the extraction of post-flight data.
Failure message release terminal is that one of the terminal of information publication is externally carried out in system.It receives failure and collects terminal hair
The information come, by calling automatic short message sending device to carry out the publication of automatic alarm information.
Failure desktop push terminal is mounted in the desktop software in designer's computer, when data collection terminal receives report
DESKTOP INFORMATION is sent information to by Unilateral Data Transferring System after alert or fault message and pushes terminal, using desktop pop-up
Mode carry out the push of warning message.
Information flow chart as shown in Figure 2 after the reception and fault diagnosis of completing satellite telemetering data, carries out alarming first true
Reality inspection rejects single frames error code, due to calculating the false alarm introduced.Its main judging means is that multiframe is carried out continuously alarm i.e.
It regards as really alarming.Classification notice is carried out to the alarm of different stage according to different satellites after completion warning message inspection,
General alarm is only prompted by the mode that DESKTOP INFORMATION pushes, for seriously alarming, short message report is added using desktop pop-up
Alert mode will also prompt operator on duty for fatal alarm at once, carry out Advise By Wire, avoid the further expansion of failure.
After completing the push of alarm and fault message, then the operation of deposit data library is carried out to related data.After frame processing to be done, then
Into checking next time.Particularly, if large area alarm continuously occur or alarming more, alarm is merged and is pushed away
It send.
Particular embodiments described above, the technical issues of to solution of the invention, technical scheme and beneficial effects carry out
It is further described, it should be understood that the above is only a specific embodiment of the present invention, is not limited to
The present invention, all within the spirits and principles of the present invention, any modification, equivalent substitution, improvement and etc. done should be included in this
Within the protection scope of invention.
Claims (6)
1. a kind of in-orbit monitoring information alarm information pushing system of satellite, which is characterized in that it includes the alarm of multiple types and mentions
Show that module, open interface module, warning message check module, the alarm of multiple types and cue module for sound, text, short
Letter and DESKTOP INFORMATION push, the data communication interface of open interface module realize that warning message is checked using dynamic link library
Module includes that text mode is checked, provides the inquiry of historical data, supports more satellite modes and single satellite mode.
2. the in-orbit monitoring information alarm information pushing system of satellite as described in claim 1, which is characterized in that the multiple types
Alarm and cue module four kinds of modes are pushed using sound, text, short message and DESKTOP INFORMATION and carry out alarm and failure push, it is more
Kind form warning message combination prompt, improves prompt effect.
3. the in-orbit monitoring information alarm information pushing system of satellite as claimed in claim 2, which is characterized in that the sound pushes away
Send is to be prompted after alarm and failure occurs using apparent sound, and carry out text casting to warning message；Text
Push is prompted using text flashing and conspicuous color notation methods；Short message push is to pass through calling after being confirmed as failure
Automatic short message sends platform and is sent according to the short message that alarm and fault type carry out different personnel；DESKTOP INFORMATION push is to pass through list
Pushed information is sent to network transmission system to the computer of designer, designer is prompted by way of desktop pop-up.
4. the in-orbit monitoring information alarm information pushing system of satellite as described in claim 1, which is characterized in that the dynamic chain
It connects library to avoid redesigning alarm information pushing system after newly increasing alarm source, it is only necessary to set dynamic link library
Meter, can meet the data protocol requirements of alarm information pushing system, configure in alarm information pushing system corresponding
Dynamic link library, when reducing new diagnostic center access system caused by exploitation amount, it is characterised in that utilize dynamic chain
Uniformity and reliability that library increases alarm information pushing system are connect, when the upgrading of external alert source, without redesigning alarm
Information transmission system provides system reliability.
5. the in-orbit monitoring information alarm information pushing system of satellite as described in claim 1, which is characterized in that the list satellite
Operating mode is suitable for designer and is concerned about some satellite, is analyzed for some satellite；More satellite operation modes are directed to satellite
In-orbit monitoring personnel to solve the demand of more stars while monitoring, while providing a kind of possibility for the analysis of more satellites.
6. the in-orbit monitoring information alarm information pushing system of satellite as described in claim 1, which is characterized in that more satellites
Mode and single satellite mode realize the switching of two kinds of operating modes by the way of configuration.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810670982.3A CN108923840A (en) | 2018-06-26 | 2018-06-26 | The in-orbit monitoring information alarm information pushing system of satellite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810670982.3A CN108923840A (en) | 2018-06-26 | 2018-06-26 | The in-orbit monitoring information alarm information pushing system of satellite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108923840A true CN108923840A (en) | 2018-11-30 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810670982.3A Pending CN108923840A (en) | 2018-06-26 | 2018-06-26 | The in-orbit monitoring information alarm information pushing system of satellite |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110658803A (en) * | 2019-09-09 | 2020-01-07 | 天津国电津能滨海热电有限公司 | On-line fault alarm device of thermal control equipment |
| CN111258305A (en) * | 2020-03-06 | 2020-06-09 | 哈工大机器人（岳阳）军民融合研究院 | Satellite operation control center system, equipment management method, equipment and storage medium |
| CN113162680A (en) * | 2021-04-23 | 2021-07-23 | 上海卫星工程研究所 | Pile-inserting type on-orbit satellite state monitoring method |
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| CN113162680B (en) * | 2021-04-23 | 2023-02-28 | 上海卫星工程研究所 | Pile-inserting type on-orbit satellite state monitoring method |
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Application publication date: 20181130 |