CN101388709A - Satellite orientation operation interface intelligent system failure detection apparatus - Google Patents
Satellite orientation operation interface intelligent system failure detection apparatus Download PDFInfo
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- CN101388709A CN101388709A CNA2008101549078A CN200810154907A CN101388709A CN 101388709 A CN101388709 A CN 101388709A CN A2008101549078 A CNA2008101549078 A CN A2008101549078A CN 200810154907 A CN200810154907 A CN 200810154907A CN 101388709 A CN101388709 A CN 101388709A
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Abstract
A fault detecting device of a satellite pair-stair operation interface intelligent system and a detecting method thereof relate to the technical field of satellite fault detecting systems. The detecting device comprises a self-checking module, a working condition detecting module, a fault detecting module and a display module, wherein a signal input end of the self-checking module and a signal output end of the working condition detecting module are respectively connected with the signal input end of the fault detecting module, and the signal output end of the fault detecting module is connected with the signal input end of the display module. The device realizes the purposes of high assurance coefficient, convenient and rapid operations and actively leading the users to operate pair-stair systems accurately.
Description
Technical field
The present invention relates to the technical field of satellite failure detection system.
Background technology
Because in present stage China is to determine by artificial judgment whether operating system is working properly, and whether each equipment receives data, and fail safe is not high to the star system man-machine interface mostly, and easy error in judgement; Perhaps whether artificial judgment wireless connections mode connects, and allows operating personnel's misoperation cause damaging mechanical structure etc. to star system in addition, especially to star system is not understood or the unskilled personnel of operating personnel, can cause adverse effect.
Summary of the invention
The object of the invention provide a kind of coefficient of safety height, simple and efficient to handle, can the positive guide user correctly operate satellite to star system to star operation interface intelligent system failure detector and detection method thereof.
The present invention adopts following technical scheme for achieving the above object:
The present invention includes selftest module, operating state detection module, fault detection module, display module, the signal output part of selftest module, operating state detection module signal output part are connected with the signal input part of fault detection module respectively, and the signal output part of fault detection module is connected with the signal input part of display module.
Selftest module of the present invention comprises mainboard selftest module, communication selftest module, peripheral hardware selftest module, first signal output part of mainboard selftest module is connected with the signal input part of communication selftest module, first signal output part of communication selftest module is connected with the signal input part of peripheral hardware selftest module, the secondary signal output of mainboard selftest module is connected with the signal input part of display module, and communication selftest module secondary signal output is connected with the signal input part of display module, the signal output part of peripheral hardware selftest module is connected with the signal input part of fault detection module.
Operating state detection module of the present invention comprises electromechanical equipment detection module, satellite motion state detection module, communications status detection module, and the signal output part of electromechanical equipment detection module, satellite motion state detection module, communications status detection module is connected with the signal input part of fault detection module respectively.
The present invention is based on the detection method of satellite, comprise that startup self-detection and fault detect two parts automatically star operation interface intelligent system failure detector:
After the start, the opening operation interface, the mainboard selftest module sends self-test signal to communication selftest module, peripheral hardware selftest module respectively, operating state to operating system is carried out self check, at first begin to detect wired and communication, secondly various input all are by control system real-time tracking and real-time detection method, judge and reading of data, control system has any one data not send all can show corresponding fault automatically, display module all can initiatively eject the window that reports an error, and the reason that reports an error is described;
The electromechanical equipment detection module detects the electromechanical equipment operation conditions on the satellite, the satellite motion state detection module detects the motion state of satellite, the communications status detection module detects the communications status of satellite, above-mentioned testing result is if there is the fault display module all can initiatively eject the window that reports an error, and the explanation reason that reports an error.
Startup self-detection of the present invention comprises the steps:
The first step: opening operation interface;
Second step: the mainboard selftest module begins the master board self check, sends the self check order to communication selftest module, peripheral hardware selftest module simultaneously;
The 3rd step: the mainboard selftest module is finished chip self check, chip interconnect self check and signal output test respectively;
The 4th step: the communication selftest module is finished the communication self check respectively, network connects test, serial communication test;
The 5th step: the peripheral hardware selftest module is finished peripheral hardware test self check, GPS test, electronic compass test and carrier signal test respectively;
The 6th step: fault detection module is judged respectively the self-detection result in above-mentioned the 3rd step, the 4th step, the 5th step, if be judged as not, show on the display module " can operate " star, if be judged as be, then report fault, on display module, eject the window that reports an error simultaneously, show " can't continue operation please check ".
Fault of the present invention detects automatically and comprises the steps:
A): the operating state that reads various device;
B): the electromechanical equipment detection module changes over to from holding state the satellite communication state is kept and detection, and finishes GPS and compass detection;
C): the satellite motion state detection module detects the motion state of satellite, and finishes the detection to the satellite electromechanical equipment;
D): the communications status detection module detects in the carrier signal data hold mode of seeking under the starlike attitude tracking antenna;
E): fault detection module is to above-mentioned b), c), d) testing result judge respectively, if be not judged as not, show on the display module " can operate " star, if be judged as be, then report fault, on display module, eject the window that reports an error simultaneously, show " can't continue operation please check ".
The present invention adopts technique scheme, compared with prior art have the following advantages: be exactly in order not cause unfavorable factor to the user, make things convenient for the user more can correctly operate to star system, the user operates any interface button and can wrongly point out, and tells the user to operate wrong or some device data does not receive.Positive guide user correctly operates star system.Strengthened fail safe in use, simple and efficient to handle.
Description of drawings
Fig. 1 is a kind of structural representation of the present invention.
Fig. 2 is the flow chart of startup self-detection of the present invention.
Fig. 3 is the flow chart that fault of the present invention detects automatically.
Embodiment
Below in conjunction with accompanying drawing technical scheme of the present invention is elaborated:
As shown in Figure 1, the present invention includes selftest module 1, operating state detection module 2, fault detection module 3, display module 4, the signal output part of selftest module 1, operating state detection module 2 signal output parts are connected with the signal input part of fault detection module 3 respectively, and the signal output part of fault detection module 3 is connected with the signal input part of display module 4.
Selftest module 1 of the present invention comprises mainboard selftest module 11, communication selftest module 12, peripheral hardware selftest module 13, first signal output part of mainboard selftest module 11 is connected with the signal input part of communication selftest module 12, first signal output part of communication selftest module 12 is connected with the signal input part of peripheral hardware selftest module 13, the secondary signal output of mainboard selftest module 11 is connected with the signal input part of display module 3, and communication selftest module 12 secondary signal outputs are connected with the signal input part of display module 3, the signal output part of peripheral hardware selftest module 13 is connected with the signal input part of fault detection module 3.
Operating state detection module 2 of the present invention comprises electromechanical equipment detection module 21, satellite motion state detection module 22, communications status detection module 23, and the signal output part of electromechanical equipment detection module 21, satellite motion state detection module 22, communications status detection module 23 is connected with the signal input part of fault detection module 3 respectively.
The present invention is based on the detection method of satellite, comprise that startup self-detection and fault detect two parts automatically star operation interface intelligent system failure detector:
After the start, the opening operation interface, mainboard selftest module 11 sends self-test signal to communication selftest module 12, peripheral hardware selftest module 13 respectively, operating state to operating system is carried out self check, at first begin to detect wired and communication, secondly various input all are by control system real-time tracking and real-time detection method, judge and reading of data, control system has any one data not send all can show corresponding fault automatically, display module 4 all can initiatively eject the window that reports an error, and the reason that reports an error is described;
Electromechanical equipment operation conditions on 21 pairs of satellites of electromechanical equipment detection module detects, the motion state of 22 pairs of satellites of satellite motion state detection module detects, the communications status of 23 pairs of satellites of communications status detection module detects, above-mentioned testing result is if there is fault display module 4 all can initiatively eject the window that reports an error, and the explanation reason that reports an error.
As shown in Figure 2, startup self-detection of the present invention comprises the steps:
The first step: opening operation interface;
Second step: the 11 beginning master board self checks of mainboard selftest module send the self check order to communication selftest module 12, peripheral hardware selftest module 13 simultaneously;
The 3rd step: mainboard selftest module 11 is finished chip self check, chip interconnect self check and signal output test respectively,
The 4th step: communication selftest module 12 is finished the communication self check respectively, network connects test, serial communication test;
The 5th step: peripheral hardware selftest module 13 is finished peripheral hardware test self check, GPS test, electronic compass test and carrier signal test respectively;
The 6th step: fault detection module 3 pairs of above-mentioned the 3rd steps, the 4th step, the 5th self-detection results that go on foot are judged respectively, if be judged as not, show on the display module 4 " can operate " star, if be judged as be, then report fault, on display module, eject the window that reports an error simultaneously, show " can't continue operation please check ".
As shown in Figure 3, fault of the present invention detects automatically and comprises the steps:
A): read operating state;
B): electromechanical equipment detection module 21 changes over to from holding state the satellite communication state is kept and detection, and finishes GPS and compass detection;
C): the motion state of 22 pairs of satellites of satellite motion state detection module detects, and finishes the detection to the satellite electromechanical equipment;
D): 23 pairs of tracking antennas of communications status detection module detect in the carrier signal data hold mode of seeking under the starlike attitude;
E): 3 couples of above-mentioned b of fault detection module), c), d) testing result judge respectively, if be not judged as not, show on the display module 4 " can operate " star, if be judged as be, then report fault, on display module, eject the window that reports an error simultaneously, show " can't continue operation please check ".
The present invention still can use many functions as far as possible under failure condition, shielding can not be operated or operate and may fail, and also has automatic fault to judge and warning function.Just beginning the self check master board from the operation interface of opening detects to chip self check and the output of chip interconnect self-test signal, at first begin to detect wired and communication, secondly all be by control system real-time tracking and real-time detection method to various input, judge and reading of data, control system have any one data do not send operating personnel just begin the operation all can show corresponding fault automatically, operation interface initiatively pop-up window is notified the user, and this item number is according to not coming or reporting corresponding fault phase.
Fault detection module of the present invention will eject corresponding miscue window automatically under situation about detecting less than needed various signals.The wrong window of prompting has been arranged, sought the star operation and just can't carry out terminating operation personnel's instruction.
Claims (6)
1, a kind of satellite is to star operation interface intelligent system failure detector, it is characterized in that comprising selftest module (1), operating state detection module (2), fault detection module (3), display module (4), the signal output part of selftest module (1), operating state detection module (2) signal output part are connected with the signal input part of fault detection module (3) respectively, and the signal output part of fault detection module (3) is connected with the signal input part of display module (4).
2, satellite according to claim 1 is to star operation interface intelligent system failure detector, it is characterized in that selftest module (1) comprises mainboard selftest module (11), communication selftest module (12), peripheral hardware selftest module (13), first signal output part of mainboard selftest module (11) is connected with the signal input part of communication selftest module (12), first signal output part of communication selftest module (12) is connected with the signal input part of peripheral hardware selftest module (13), the secondary signal output of mainboard selftest module (11) is connected with the signal input part of display module (3), and communication selftest module (12) secondary signal output is connected with the signal input part of display module (3), the signal output part of peripheral hardware selftest module (13) is connected with the signal input part of fault detection module (3).
3, satellite according to claim 1 is to star operation interface intelligent system failure detector, it is characterized in that operating state detection module (2) comprises electromechanical equipment detection module (21), satellite motion state detection module (22), communications status detection module (23), the signal output part of electromechanical equipment detection module (21), satellite motion state detection module (22), communications status detection module (23) is connected with the signal input part of fault detection module (3) respectively.
4,, it is characterized in that comprising that startup self-detection and fault detect two parts automatically based on the detection method of the described satellite of claim 1 to star operation interface intelligent system failure detector:
After the start, the opening operation interface, mainboard selftest module (11) sends self-test signal to communication selftest module (12), peripheral hardware selftest module (13) respectively, operating state to operating system is carried out self check, at first begin to detect wired and communication, secondly various input all are by control system real-time tracking and real-time detection method, judge and reading of data, control system has any one data not send all can show corresponding fault automatically, display module (4) all can initiatively eject the window that reports an error, and the reason that reports an error is described;
Electromechanical equipment detection module (21) detects the electromechanical equipment operation conditions on the satellite, satellite motion state detection module (22) detects the motion state of satellite, communications status detection module (23) detects the communications status of satellite, above-mentioned testing result is if there is fault display module (4) all can initiatively eject the window that reports an error, and the explanation reason that reports an error.
5, satellite according to claim 4 is characterized in that to the detection method of star operation interface intelligent system failure detector above-mentioned startup self-detection comprises the steps:
The first step: opening operation interface;
Second step: mainboard selftest module (11) beginning master board self check sends the self check order to communication selftest module (12), peripheral hardware selftest module (13) simultaneously;
The 3rd step; Mainboard selftest module (11) is finished chip self check, chip interconnect self check and signal output test respectively;
The 4th step: communication selftest module (12) is finished the communication self check respectively, network connects test, serial communication test;
The 5th step: peripheral hardware selftest module (13) is finished peripheral hardware test self check, GPS test, electronic compass test and carrier signal test respectively;
The 6th step: fault detection module (3) is judged respectively the self-detection result in above-mentioned the 3rd step, the 4th step, the 5th step, if be judged as not, display module (4) is gone up and is shown " can operate star ", if be judged as be, then report fault, on display module, eject the window that reports an error simultaneously, show " can't continue operation please check ".
6, satellite according to claim 4 is characterized in that to the detection method of star operation interface intelligent system failure detector automatic detection of above-mentioned fault comprises the steps:
A): the operating state that reads various device;
B): electromechanical equipment detection module (21) changes over to from holding state the satellite communication state is kept and detection, and finishes GPS and compass detection;
C): satellite motion state detection module (22) detects the motion state of satellite, and finishes the detection to the satellite electromechanical equipment;
D): communications status detection module (23) detects in the carrier signal data hold mode of seeking under the starlike attitude tracking antenna;
E): fault detection module (3) is to above-mentioned b), c), d) testing result judge respectively, if be judged as not, display module (4) is gone up and is shown " can operate star ", if be judged as be, then report fault, on display module, eject the window that reports an error simultaneously, show " can't continue operation please check ".
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| Application Number | Priority Date | Filing Date | Title |
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| CNA2008101549078A CN101388709A (en) | 2008-10-24 | 2008-10-24 | Satellite orientation operation interface intelligent system failure detection apparatus |
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| Application Number | Priority Date | Filing Date | Title |
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| CNA2008101549078A CN101388709A (en) | 2008-10-24 | 2008-10-24 | Satellite orientation operation interface intelligent system failure detection apparatus |
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| CN101388709A true CN101388709A (en) | 2009-03-18 |
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| CNA2008101549078A Pending CN101388709A (en) | 2008-10-24 | 2008-10-24 | Satellite orientation operation interface intelligent system failure detection apparatus |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103076779A (en) * | 2012-12-28 | 2013-05-01 | 中国人民解放军国防科学技术大学 | Independent control method and device of satellite-borne equipment on microsatellite |
| CN109587473A (en) * | 2018-12-04 | 2019-04-05 | 安徽站乾科技有限公司 | A kind of self detection device of the failure of satellite TV system |
| CN109945930A (en) * | 2019-04-16 | 2019-06-28 | 山东理工职业学院 | A kind of electromechanical equipment fault detection approach based on electromagnetic technique |
-
2008
- 2008-10-24 CN CNA2008101549078A patent/CN101388709A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103076779A (en) * | 2012-12-28 | 2013-05-01 | 中国人民解放军国防科学技术大学 | Independent control method and device of satellite-borne equipment on microsatellite |
| CN109587473A (en) * | 2018-12-04 | 2019-04-05 | 安徽站乾科技有限公司 | A kind of self detection device of the failure of satellite TV system |
| CN109945930A (en) * | 2019-04-16 | 2019-06-28 | 山东理工职业学院 | A kind of electromechanical equipment fault detection approach based on electromagnetic technique |
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Application publication date: 20090318 |