CN115762025A - Intelligent early warning method and system for communication optical cable - Google Patents
Intelligent early warning method and system for communication optical cable Download PDFInfo
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Abstract
The invention discloses an intelligent early warning method for a communication optical cable, which relates to the field of communication and comprises the steps of obtaining basic information of the communication optical cable and constructing an optical cable distribution diagram; the optical cable basic information comprises an information acquisition terminal in communication connection with an optical cable, a detection host and optical cable laying; determining each identification position based on the optical cable distribution diagram, and acquiring aircraft base station information pre-constructed at the identification position; acquiring sudden vibration data information, acquiring aircraft flight execution information, base station aircraft information and aircraft scheduling information, creating a priority, performing step-by-step matching and forming a flight task; obtaining the uploading view information of the aircraft, secondarily evaluating the sudden vibration type and generating an early warning type; and executing the alarm. Also discloses an intelligent early warning system for the communication optical cable. The method can realize the quick positioning of the optical cable abnormity, realize quick response based on the constructed aircraft base station, judge the sudden vibration type for the second time, accurately capture the invasion information type and reduce the judgment error.
Description
Technical Field
The invention relates to the technical field of optical cable communication, in particular to an intelligent early warning method and system for a communication optical cable.
Background
With the rapid development of optical fiber communication technology and the need of economic market development, the construction of optical cables for communication information transmission is also extending the strengthening bus and continuously expanding the laying range. However, as the optical cable laying range is enlarged, the optical cable is negatively affected by communication interruption and the like caused by more and more external force damages, wherein the external factors causing the communication optical cable damages mainly include: rough engineering construction work, intentional and unintentional human factors (such as optical cable theft, malicious damage and the like), natural disasters (such as earthquakes, typhoons and the like) and the like. Therefore, the communication optical cable is prevented from being damaged by external force through a related early warning method, and the safety and the reliability of monitoring and protecting the normal operation of the communication optical cable line are very necessary.
At present, to the early warning monitoring of communication optical cable external force destruction, mainly DVS (distributed optical fiber vibration sensing system) uses optic fibre as the optical instrument that the sensor carries out the vibration perception or increases collection terminal on treating the detection optical cable, through utilizing single optic fibre and collection terminal to realize the monitoring of vibration and the transmission of signal, the specific position of external disturbance is judged to the backscatter signal of analytic optic fibre transmission return. However, the monitoring method has the problems of high false alarm and leakage alarm rate, incapability of identifying the distance between the vibration source and the optical cable and the specific hazard level and the like. The existing mode of utilizing the acquisition terminal is poor in monitoring precision of the external force damage degree of the communication optical cable, blocking processing cannot be performed in a short time, and when the communication optical cable needs to be in the field or alarm is implemented or driven away, multiple departments or personnel need to be linked, the response speed is slow, the intrusion blocking is extremely unfavorable, and the loss higher than the estimated loss is caused under the condition that the damage can be reduced.
Disclosure of Invention
The invention aims to solve the technical problem of providing an intelligent early warning method for a communication optical cable, which can quickly respond to the abnormity of the optical cable and can accurately capture the type of invasion information. In addition, still provide a communication optical cable intelligence early warning system.
The technical scheme adopted by the invention for solving the technical problems is as follows: the intelligent early warning method for the communication optical cable comprises the following steps
S1, acquiring basic information of a communication optical cable, and constructing an optical cable distribution diagram; the optical cable basic information comprises an information acquisition terminal in communication connection with an optical cable, a detection host and optical cable laying;
s2, determining each identification position based on the optical cable distribution diagram, and acquiring aircraft base station information pre-constructed at the identification position;
s3, acquiring sudden vibration data information, acquiring aircraft flight execution information, base station aircraft information and aircraft scheduling information, creating a priority, performing step-by-step matching and forming a flight task;
s4, obtaining the view information uploaded by the aircraft, secondarily evaluating the sudden vibration type and generating an early warning type;
and S5, executing alarm based on the received early warning type information.
Further, the step S4 also comprises the steps of obtaining the view information uploaded by the aircraft, secondarily evaluating the sudden vibration type,
and judging the grade based on the sudden vibration type, and dispatching the inspection vehicle or pushing information to an inspection functional department within a preset range of the sudden vibration position after the grade reaches the set grade.
Further, S3, acquiring sudden vibration data information, acquiring flight execution information, base station information and flight scheduling information of the aircraft, creating priority and performing step-by-step matching to form flight tasks, wherein the steps comprise
S301, judging whether a flying execution aircraft exists at the sudden vibration generation position, if so, acquiring the utilization time and the current position information of the aircraft, judging whether the state of the aircraft is matched with a flight task, and if not, executing the step S302;
s302, calculating the number of aircraft base stations in a preset range based on the sudden vibration data information, acquiring aircraft state information in the base stations and judging whether the aircraft is airworthy, and if not, executing the step S303;
s303, acquiring scheduling information, judging whether the current scheduling aircraft passes through the sudden vibration generation position, and if not, executing the step S304;
and S304, dispatching the inspection vehicle to inspect and early warn the sudden vibration position.
Further, step S302 of obtaining status information of the aircraft in the base station and determining whether the aircraft is airworthy includes
Calculating the endurance distance of the aircraft, and executing a flight task if the aircraft meets the requirement of single flight;
and judging whether the task is executed completely, if so, landing at a preset position and executing electric quantity reservation to wait for searching and carrying of the inspection vehicle.
Further, whether the task is executed is judged, if yes, the vehicle lands at a preset position and electric quantity reservation is executed to wait for the polling vehicle to search for carrying, and the method comprises the following steps,
obtaining return distance information or supply point information or routing information of the inspection vehicle to obtain a calibration position;
calculating self electric quantity and endurance distance and flying to any calibration position;
and landing and sending a connection signal at regular time so as to be used for polling vehicle connection and searching.
Further, the early warning type comprises one or more of voice drive-off, tracking shooting and warning lamps.
Based on the same idea, still provide a communication optical cable intelligence early warning system, include
The optical cable information acquisition module is used for acquiring basic information of the communication optical cable and constructing an optical cable distribution diagram; the optical cable basic information comprises an information acquisition terminal in communication connection with an optical cable, a detection host and optical cable laying;
the base station information acquisition module is used for determining each identification position based on the optical cable distribution diagram and acquiring aircraft base station information pre-constructed at the identification position;
the flight calculation module is used for acquiring sudden vibration data information, acquiring flight execution information of the aircraft, information of the base station aircraft and scheduling information of the aircraft, creating priorities, performing step-by-step matching and forming a flight task;
the assessment early warning module is used for acquiring the view information uploaded by the aircraft, secondarily assessing the sudden vibration type and generating an early warning type;
the warning module is used for executing warning based on the received warning type information; the early warning type comprises one or more of voice drive, tracking shooting and warning lamps.
Furthermore, the assessment early warning module is also used for judging the grade based on the sudden vibration type, and after the grade reaches the set grade, dispatching the inspection vehicle or pushing information to the preset range of the sudden vibration position to inspect the functional department.
Further, the flight calculation module is also used for
Judging whether a flying-execution aircraft exists at the sudden vibration generation position, if so, acquiring the utilization time and the current position information of the aircraft, and judging whether the state of the aircraft is matched with a flight task;
when the base stations are not matched, the number of the aircraft base stations in a preset range is calculated based on the sudden vibration data information, the aircraft state information in the base stations is obtained, and whether the base stations are airworthy is judged;
when the aircraft is not suitable for navigation, obtaining scheduling information, and judging whether the current scheduling aircraft passes through the sudden vibration generation position;
and when the vehicle is not passing, dispatching the inspection vehicle to inspect and early warn the sudden vibration position.
Further, the flight calculation module is also used for calculating the endurance distance of the aircraft, and if the aircraft meets the requirement of single flight, the flight task is executed;
judging whether the task is finished, if so, landing at a preset position and performing electric quantity reservation to wait for the search and carrying of the inspection vehicle,
the system is used for acquiring return distance information or supply point information or routing information of the inspection vehicle to acquire a calibration position;
calculating self electric quantity and endurance distance and flying to any calibration position;
and landing and sending a connection signal at regular time so as to be used for polling vehicle connection and searching.
The intelligent early warning method for the communication optical cable comprises the steps of confirming a sudden vibration position by the optical cable, an acquisition terminal and a detection host, then determining a base station condition in a preset range of the sudden vibration position by the aid of constructed aircraft base station information, creating a site confirmation task of the sudden vibration position by the aid of aircraft flying information, base station aircraft information and aircraft scheduling information, returning view information after the aircraft enters the site of the sudden vibration position and judging the type of the sudden vibration, and if the type of the vibration is illegal, generating early warning and broadcasting by the aircraft. According to the intelligent early warning method for the communication optical cable, the acquisition terminal, the detection host and other equipment are used for quickly positioning the abnormity of the optical cable by Rayleigh scattering, quick response is realized based on the constructed aircraft base station, the captured view information is returned after the aircraft flies to the site, the sudden vibration type is judged secondarily, the invasion information type is accurately captured, the judgment error is reduced, and in addition, the early warning type is generated based on the sudden vibration type, so that accurate early warning is realized.
The intelligent early warning system for the communication optical cable is based on the same idea as the method, and utilizes the optical cable information acquisition module, the base station information acquisition module, the flight calculation module, the evaluation early warning module and the warning module to realize the quick positioning of the optical cable abnormity, and realizes quick response based on the constructed aircraft base station, and returns the captured view information after the aircraft flies to the site, and secondarily judges the sudden vibration type, accurately captures the invasion information type, reduces the judgment error, and generates an early warning type based on the sudden vibration type to realize accurate early warning.
Drawings
The invention will be further described with reference to the accompanying drawings and examples, in which:
FIG. 1 is a flow chart of an intelligent early warning method for a communication cable according to an embodiment of the present invention;
FIG. 2 is a block flow diagram of the formation of a flight mission according to an embodiment of the present invention;
fig. 3 is a block diagram of a flow of reserving electric quantity and waiting for embarkation according to an embodiment of the present invention;
fig. 4 is a block diagram of a communication cable intelligent early warning system according to an embodiment of the present invention.
Detailed Description
For a more clear understanding of the technical features, objects and effects of the present invention, embodiments of the present invention will now be described in detail with reference to the accompanying drawings.
The intelligent early warning method for the communication optical cable shown in the figures 1-3 comprises the following steps
S1, acquiring basic information of a communication optical cable, and constructing an optical cable distribution diagram; the optical cable basic information comprises an information acquisition terminal, a detection host and optical cable laying, wherein the information acquisition terminal is in communication connection with the optical cable.
Based on optical cable, collection terminal and detection host computer can calculate the distribution condition of optical cable to can calculate the positional information when the disturbance appears based on the rayleigh scattering principle, this embodiment, information acquisition terminal includes vibration sensing matrix module, and vibration sensing matrix module includes a plurality of vibration sensor that set up relatively on spatial position, and vibration sensor is arranged in gathering the vibration wave that produces and the acquisition time that corresponds in the environment respectively, and information acquisition terminal locates the tip of optical cable is located to the monitoring host computer on the surface of optical cable. (ii) a The information acquisition terminal is used for controlling the vibration sensing matrix module to collect vibration source signals generated in the environment, the monitoring host is used for converting the backscattered light signals into corresponding digital electric signals, and frequency characteristic analysis and vibration characteristic matching are carried out on the digital electric signals, so that the position of sudden vibration is determined.
S2, determining each identification position based on the optical cable distribution diagram, and acquiring aircraft base station information pre-constructed at the identification position. The positions of the aircraft base stations are determined and constructed based on the optical cable distribution diagram, identification position determination can be achieved by using an AI algorithm in city construction, and optimization of paths and cost can be achieved by using the algorithm. In the embodiment, the main functions of the constructed aircraft base station are to realize the parking and charging of the unmanned aerial vehicle, so that the purpose can be realized by depending on a power grid system in a city or town, for example, a street lamp is improved to be used for temporary parking of the unmanned aerial vehicle; the electric power can be conveniently taken and the cost can be effectively saved by depending on the construction along the highway or the railway in a wide area.
And S3, acquiring the sudden vibration data information, acquiring the flight execution information of the aircraft, the aircraft information of the base station and the aircraft scheduling information, creating the priority, performing step-by-step matching and forming a flight task. The data information of the sudden vibration is the first judgment basis, the type of the vibration can be preliminarily judged by analyzing the data information of the sudden vibration, and the approximate reason generated by analyzing the data information of the sudden vibration can be analyzed, although errors exist, the situation except critical situations can be eliminated to a certain extent, such as temporary stop of a large vehicle, passing or stopping of a tracked vehicle, and the invasion possibility can be eliminated through the preliminary judgment.
After the probability of the intrusion possibility is increased, the aircraft is called to perform a flight task, a specific task assignment and scheduling of the aircraft, which will be described in detail in the following section.
And S4, obtaining the view information uploaded by the aircraft, secondarily evaluating the sudden vibration type and generating an early warning type. In this embodiment, obtaining the view information uploaded by the aircraft, and performing secondary evaluation on the sudden vibration type further includes determining a level based on the sudden vibration type, and after the level reaches a set level, scheduling the inspection vehicle or pushing the information to an inspection function department within a preset range of the sudden vibration position.
And S5, executing alarm based on the received early warning type information. The early warning category comprises one or more of voice driving, tracking shooting and warning lamps.
The intelligent early warning method for the communication optical cable comprises the steps of confirming a sudden vibration position by the optical cable, an acquisition terminal and a detection host, then determining a base station condition in a preset range of the sudden vibration position by the aid of constructed aircraft base station information, creating a site confirmation task of the sudden vibration position by the aid of aircraft flying information, base station aircraft information and aircraft scheduling information, returning view information after the aircraft enters the site of the sudden vibration position and judging the type of the sudden vibration, and if the type of the vibration is illegal, generating early warning and broadcasting by the aircraft. According to the intelligent early warning method for the communication optical cable, the acquisition terminal, the detection host and other equipment are used for quickly positioning the optical cable abnormity by Rayleigh scattering, quick response is realized based on the constructed aircraft base station, the captured view information is returned after the aircraft flies to the site, the sudden vibration type is secondarily judged, the invasion information type is accurately captured, the judgment error is reduced, and in addition, the early warning type is generated based on the sudden vibration type, so that accurate early warning is realized.
As shown in fig. 2, step S3 obtains the information of the sudden vibration data, obtains the flight execution information of the aircraft, the information of the base station and the scheduling information of the aircraft, creates the priority and performs the step-by-step matching to form the flight mission, including
S301, judging whether a flying execution aircraft exists at the sudden vibration generation position, if so, acquiring the utilization time and the current position information of the aircraft, judging whether the state of the aircraft is matched with a flight task, and if not, executing the step S302;
s302, calculating the number of aircraft base stations in a preset range based on the information of the sudden vibration data, acquiring the state information of the aircraft in the base stations and judging whether the aircraft is airworthy, wherein the method comprises the steps of
Calculating the endurance distance of the aircraft, and executing a flight task if the aircraft meets the requirement of single flight;
and judging whether the task is finished, if so, landing at a preset position and performing electric quantity reservation to wait for searching and carrying of the inspection vehicle. As shown in fig. 3, it specifically includes the following steps,
obtaining return distance information or supply point information or routing information of the inspection vehicle to obtain a calibration position;
calculating self electric quantity and endurance distance and flying to any calibration position;
and landing and sending a connection signal at regular time so as to be used for polling vehicle connection and searching.
If not, go to step S303. S303, acquiring scheduling information, judging whether the current scheduling aircraft passes through the sudden vibration generation position, and if not, executing the step S304;
and S304, dispatching the inspection vehicle to inspect and early warn the sudden vibration position.
This aircraft removes to carry out the flight task, and specific task dept and the dispatch of aircraft are as above, to unmanned aerial vehicle dispatch priority, can realize quick response to can solve continuation of the journey and flight cost problem, compare in the point-to-point flight of aircraft, avoid the later stage to patrol and examine the vehicle span scope too big, and can effectively avoid the construction system to cause too big burden.
As shown in fig. 4, the intelligent early warning system for communication optical cable comprises an optical cable information acquisition module, a base station information acquisition module, a flight calculation module, an evaluation early warning module and an alarm module. Wherein the content of the first and second substances,
the optical cable information acquisition module is used for acquiring basic information of the communication optical cable and constructing an optical cable distribution diagram; the optical cable basic information comprises an information acquisition terminal in communication connection with the optical cable, a detection host and optical cable laying.
Based on optical cable, collection terminal and detection host computer can calculate the distribution condition of optical cable to can calculate the positional information when the disturbance appears based on the rayleigh scattering principle, this embodiment, information acquisition terminal includes vibration sensing matrix module, and vibration sensing matrix module includes a plurality of vibration sensor that set up relatively on spatial position, and vibration sensor is arranged in gathering the vibration wave that produces and the acquisition time that corresponds in the environment respectively, and information acquisition terminal locates the tip of optical cable is located to the monitoring host computer on the surface of optical cable. (ii) a The information acquisition terminal is used for controlling the vibration sensing matrix module to collect vibration source signals generated in the environment, the monitoring host is used for converting the backscattered light signals into corresponding digital electric signals, and frequency characteristic analysis and vibration characteristic matching are carried out on the digital electric signals, so that the position of sudden vibration is determined.
And the base station information acquisition module is used for determining each identification position based on the optical cable distribution diagram and acquiring the aircraft base station information pre-constructed at the identification position. The positions of the aircraft base stations are determined and constructed based on the optical cable distribution diagram, identification position determination can be achieved by using an AI algorithm in city construction, and optimization of paths and cost can be achieved by using the algorithm. In this embodiment, the main function of the constructed aircraft base station is to realize the parking and charging of the unmanned aerial vehicle, so that the purpose can be realized by depending on a power grid system in a city or a town, for example, a street lamp is improved for temporary parking of the unmanned aerial vehicle; the electric power can be conveniently taken and the cost can be effectively saved by depending on the construction along the highway or the railway in a wide area.
And the flight calculation module is used for acquiring the sudden vibration data information, acquiring the flight execution information of the aircraft, the aircraft information of the base station and the aircraft scheduling information, creating the priority, performing step-by-step matching and forming a flight task. The data information of the sudden vibration is the first judgment basis, the type of the vibration can be preliminarily judged by analyzing the data information of the sudden vibration, and the approximate reason generated by analyzing the data information of the sudden vibration can be analyzed, although errors exist, the situation except critical situations can be eliminated to a certain extent, such as temporary stop of a large vehicle, passing or stopping of a tracked vehicle, and the invasion possibility can be eliminated through the preliminary judgment.
The flight calculation module is also used for
Judging whether a flying-execution aircraft exists at the sudden vibration generation position, if so, acquiring the utilization time and the current position information of the aircraft, and judging whether the state of the aircraft is matched with a flight task;
when the base stations are not matched, the number of the aircraft base stations in a preset range is calculated based on the sudden vibration data information, the aircraft state information in the base stations is obtained, and whether the base stations are airworthy is judged;
when the aircraft is not suitable for navigation, obtaining scheduling information and judging whether the current scheduling aircraft passes through the sudden vibration generating position;
and when the vehicle is not passing, dispatching the inspection vehicle to inspect and early warn the sudden vibration position.
The flight calculation module is also used for calculating the endurance distance of the aircraft, and if the aircraft meets the requirement of single flight, the flight task is executed;
judging whether the task is finished, if so, landing at a preset position and performing electric quantity reservation to wait for the search and carrying of the inspection vehicle,
the system is used for acquiring return distance information or supply point information or routing information of the inspection vehicle to acquire a calibration position;
calculating the self-electricity quantity and the endurance distance and flying to any calibration position;
and landing and sending a connection signal at regular time so as to be used for polling vehicle connection and searching.
This aircraft removes to carry out the flight task, and specific task dept and the dispatch of aircraft are as above, to unmanned aerial vehicle dispatch priority, can realize quick response to can solve continuation of the journey and flight cost problem, compare in the point-to-point flight of aircraft, avoid the later stage to patrol and examine the vehicle span scope too big, and can effectively avoid the construction system to cause too big burden.
And the assessment early warning module is used for acquiring the view information uploaded by the aircraft, secondarily assessing the sudden vibration type and generating an early warning type. In this embodiment, the method includes obtaining view information uploaded by the aircraft, and performing secondary evaluation on the sudden vibration type, and then determining the level based on the sudden vibration type, and after reaching a set level, scheduling the inspection vehicle or pushing the information to an inspection functional department within a preset range of the sudden vibration position.
The warning module is used for executing warning based on the received warning type information; the early warning category comprises one or more of voice driving, tracking shooting and warning lamps.
The intelligent early warning system for the communication optical cable is based on the same idea as the method, and utilizes the optical cable information acquisition module, the base station information acquisition module, the flight calculation module, the evaluation early warning module and the warning module to realize the quick positioning of the optical cable abnormity, and realizes quick response based on the constructed aircraft base station, and returns the captured view information after the aircraft flies to the site, and secondarily judges the sudden vibration type, accurately captures the invasion information type, reduces the judgment error, and generates an early warning type based on the sudden vibration type to realize accurate early warning.
It should be understood that the above examples are only for clarity of illustration and are not intended to limit the embodiments. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. And obvious variations or modifications therefrom are within the scope of the invention.
Claims (10)
1. An intelligent early warning method for communication optical cables is characterized by comprising the following steps
S1, acquiring basic information of a communication optical cable, and constructing an optical cable distribution diagram; the optical cable basic information comprises an information acquisition terminal, a detection host and optical cable laying, wherein the information acquisition terminal is in communication connection with the optical cable;
s2, determining each identification position based on the optical cable distribution diagram, and acquiring aircraft base station information pre-constructed at the identification position;
s3, acquiring sudden vibration data information, acquiring aircraft flight execution information, base station aircraft information and aircraft scheduling information, creating a priority, performing step-by-step matching and forming a flight task;
s4, obtaining the view information uploaded by the aircraft, secondarily evaluating the sudden vibration type and generating an early warning type;
and S5, executing alarm based on the received early warning type information.
2. The intelligent early warning method for the communication optical cable according to claim 1, wherein the step S4 further comprises obtaining information of an uploading view of the aircraft, and after secondarily evaluating the sudden vibration type, further comprises,
and judging the grade based on the sudden vibration type, and dispatching the inspection vehicle or pushing information to an inspection functional department within a preset range of the sudden vibration position after the grade reaches the set grade.
3. The intelligent early warning method for the communication optical cable according to claim 2, wherein the step S3 of obtaining the information of the sudden vibration data, obtaining the flight execution information of the aircraft, the information of the base station and the scheduling information of the aircraft, creating the priority and performing the step-by-step matching to form the flight mission comprises
S301, judging whether a flying execution aircraft exists at the sudden vibration generation position, if so, acquiring the utilization time and the current position information of the aircraft, judging whether the state of the aircraft is matched with a flight mission, and if not, executing a step S302;
s302, calculating the number of aircraft base stations in a preset range based on the sudden vibration data information, acquiring aircraft state information in the base stations and judging whether the aircraft is airworthy, and if not, executing the step S303;
s303, acquiring scheduling information, judging whether the current scheduling aircraft passes through the sudden vibration generation position, and if not, executing the step S304;
s304, dispatching the inspection vehicle to inspect and early warn the sudden vibration position.
4. The intelligent early warning method for communication optical cable according to claim 3, wherein the step S302 of obtaining the status information of the aircraft in the base station and determining whether the aircraft is airworthy comprises
Calculating the endurance distance of the aircraft, and executing a flight task if the aircraft meets the requirement of single flight;
and judging whether the task is executed completely, if so, landing at a preset position and executing electric quantity reservation to wait for searching and carrying of the inspection vehicle.
5. The intelligent communication cable early warning method according to claim 4, wherein the method comprises the steps of judging whether the task is completed, if so, descending at a preset position and reserving electric quantity to wait for the inspection vehicle to search for carrying, and comprises the following steps,
obtaining return distance information or supply point information or routing information of the inspection vehicle to obtain a calibration position;
calculating self electric quantity and endurance distance and flying to any calibration position;
and landing and sending a connection signal at regular time so as to be used for polling vehicle connection and searching.
6. An intelligent early warning method for communication optical cables as claimed in any one of claims 1 to 5, wherein the early warning types comprise one or more of voice drive-off, tracking shooting and warning light.
7. An intelligent early warning system for communication optical cables is characterized by comprising
The optical cable information acquisition module is used for acquiring basic information of the communication optical cable and constructing an optical cable distribution diagram; the optical cable basic information comprises an information acquisition terminal, a detection host and optical cable laying, wherein the information acquisition terminal is in communication connection with the optical cable;
the base station information acquisition module is used for determining each identification position based on the optical cable distribution diagram and acquiring aircraft base station information pre-constructed at the identification position;
the flight calculation module is used for acquiring sudden vibration data information, acquiring flight execution information of the aircraft, information of the base station aircraft and scheduling information of the aircraft, creating priorities, performing step-by-step matching and forming a flight task;
the assessment early warning module is used for acquiring the view information uploaded by the aircraft, secondarily assessing the sudden vibration type and generating an early warning type;
the warning module is used for executing warning based on the received warning type information; the early warning type comprises one or more of voice drive-off, tracking shooting and warning lamps.
8. The intelligent communication optical cable early warning system of claim 7, wherein the assessment early warning module is further configured to determine a level based on the sudden vibration type, and schedule the inspection vehicle or push information to an inspection functional department within a preset range of the sudden vibration position after the level reaches the set level.
9. The intelligent warning system for communication cables of claim 8, wherein the flight calculation module is further configured to calculate the flight parameters of the aircraft
Judging whether a flying-execution aircraft exists at the sudden vibration generation position, if so, acquiring the utilization time and the current position information of the aircraft, and judging whether the state of the aircraft is matched with a flight task;
when the base stations are not matched, the number of the aircraft base stations in a preset range is calculated based on the sudden vibration data information, the aircraft state information in the base stations is obtained, and whether the base stations are airworthy is judged;
when the aircraft is not suitable for navigation, obtaining scheduling information, and judging whether the current scheduling aircraft passes through the sudden vibration generation position;
and when the vehicle is not passing, dispatching the inspection vehicle to inspect and early warn the sudden vibration position.
10. The intelligent early warning system for communication cables as claimed in claim 9, wherein the flight calculation module further comprises a processor for calculating a cruising distance of the aircraft, and executing a flight task if the aircraft meets a single flight requirement;
judging whether the task is finished, if so, landing at a preset position and performing electric quantity reservation to wait for the search and carrying of the inspection vehicle,
the system is used for acquiring return distance information or supply point information or routing information of the inspection vehicle to acquire a calibration position;
calculating the self-electricity quantity and the endurance distance and flying to any calibration position;
and landing and sending a connection signal at regular time so as to be used for polling vehicle connection and searching.
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| CN202211590754.8A CN115762025B (en) | 2022-12-12 | Intelligent early warning method and system for communication optical cable |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN116593811B (en) * | 2023-07-17 | 2023-09-15 | 南京欧陆电气股份有限公司 | Integrated frequency converter running state monitoring system and monitoring method |
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