CN112579423B - Equipment monitoring method and device - Google Patents
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Abstract
The disclosure provides a device monitoring method and device, relates to the technical field of electronic information, and can solve the problem of low management efficiency caused by non-uniform device interfaces when managing ground measurement and control devices. The specific technical scheme is as follows: after the target file is acquired, determining a target task corresponding to the ground measurement and control equipment according to the flight task of the spacecraft in the target file, wherein the target task comprises a test task, a calibration task, a capturing task and other tasks, and issuing the task to the ground measurement and control equipment corresponding to the target spacecraft, so that the integrated management of the ground measurement and control equipment is realized. The present disclosure is for device monitoring.
Description
Technical Field
The disclosure relates to the technical field of electronic information, and in particular relates to a device monitoring method and device.
Background
With the rapid development of aerospace technology, monitoring and management on a spacecraft are becoming a problem to be solved urgently. In the prior art, in order to realize the management and operation and maintenance of the spacecraft, ground measurement and control equipment of satellite orbit measurement and control service is configured, but the equipment needs to manually acquire a measurement and control work plan in the operation process and then send the measurement and control work plan to the corresponding ground measurement and control equipment according to the work plan, so that the labor cost is increased, and especially when the number of the ground measurement and control equipment is large and the number of the ground measurement and control equipment is large, the requirement of measurement and control tasks cannot be met by adopting a manual mode, and the measurement and control efficiency is low.
Disclosure of Invention
The embodiment of the disclosure provides a device monitoring method and device, which can solve the problem of low management efficiency of ground measurement and control devices. The technical scheme is as follows:
According to a first aspect of an embodiment of the present disclosure, there is provided an apparatus monitoring method, applied to a monitoring device, the method including:
Acquiring a target file, wherein the target file is used for indicating a task file corresponding to target equipment when a spacecraft executes a flight task, the target file comprises an equipment operation planning file, an equipment operation flow file and an equipment operation parameter file, and the target equipment is ground measurement and control equipment for controlling the spacecraft;
Analyzing the target file, and generating a target task according to an analysis result, wherein the target task is used for indicating target equipment to operate according to the target file and setting parameters according to the target file;
And sending the target task to the target equipment.
In one embodiment, the method generates a target task comprising:
Acquiring a target interval time and target equipment corresponding to the spacecraft according to an analysis result of the target file, wherein the target time is the interval time between the current target task and the last target task corresponding to the target equipment, and the target equipment is measurement and control equipment corresponding to the target spacecraft;
Determining a calibration type of the target device according to the target time information and a preset correction strategy, wherein the calibration type comprises: at least one of the distance-measuring distance leave school zero, the automatic phase correction of angle tracking, the calibration of photoelectric mismatch of angle measurement and the calibration of chassis level of movable equipment;
And generating a calibration task according to the correction strategy and the correction type, wherein the calibration task is used for indicating the execution of the calibration type in the target interval time.
In one embodiment, the method generates a target task comprising:
Determining a test item of the target equipment according to the analysis result of the target file, wherein the test item comprises test ephemeris data, test theoretical trajectory or comparison data of data downloaded by the on-board positioning equipment, test telemetry data transmission simulation data and monitoring frame synchronization bit error data;
and generating a test task according to the test item, and acquiring a test result.
In one embodiment, the method wherein the spacecraft comprises a satellite, the generating the target mission comprises:
according to the analysis result of the target file, determining a target antenna corresponding to the spacecraft and navigation data corresponding to the spacecraft, wherein the navigation data comprises: station entering instantaneous root data, orbit root data and ephemeris data;
according to the target antenna, acquiring parameter information corresponding to the target antenna, wherein the parameter information comprises: antenna shielding data and positive and negative loop operation limit data;
and generating a capturing task according to the navigation data and the parameter information, wherein the capturing task is used for indicating the target antenna to capture the signal of the target spacecraft.
In one embodiment, generating the capture task in the method further comprises:
Acquiring switching information corresponding to the spacecraft, wherein the switching information comprises: frequency switching information and telemetry code rate switching information;
And generating the capturing information according to the switching information.
In one embodiment, the method further comprises:
Acquiring environmental data of a target place corresponding to the target equipment, wherein the environmental data comprises weather data, voltage and current data and security data, and the weather data comprises: indoor and outdoor humiture and disaster weather early warning of the target place;
and generating warning information according to the comparison result of the environment data and the preset threshold value.
According to the monitoring method provided by the embodiment of the disclosure, after the target file is acquired, the target task corresponding to the ground measurement and control equipment is determined according to the flight task of the spacecraft in the target file, wherein the target task comprises a test task, a calibration task, a capturing task and other tasks, and the task is issued to the ground measurement and control equipment corresponding to the target spacecraft, so that the integrated management of the ground measurement and control equipment is realized. When the ground measurement and control equipment is managed according to the target file, the device parameters of a plurality of different ground measurement and control equipment are compatible, corresponding device parameters and operation tasks are set according to the flight task of the spacecraft, the requirements of various task scenes in reality can be met, meanwhile, manual operation is greatly reduced, and the device management efficiency is improved.
According to a second aspect of embodiments of the present disclosure, there is provided a monitoring apparatus, comprising:
A receiver, a transmitter and a processor,
The processor is respectively connected with the receiver and the transmitter;
The receiver is used for acquiring a target file, wherein the target file is used for indicating a file corresponding to target equipment when the spacecraft executes a flight task, the target file comprises an equipment operation planning file, an equipment operation flow file and an equipment operation parameter file, and the target equipment is ground measurement and control equipment for controlling the spacecraft;
the processor is used for analyzing the target file, generating a target task according to the analysis result, and the target task is used for indicating target equipment to operate according to the target file and setting parameters according to the target file;
the transmitter is configured to transmit the target task to the target device, the target device including a spacecraft.
In one embodiment, the processor in the device is further configured to,
Acquiring a target interval time and target equipment corresponding to the spacecraft according to an analysis result of the target file, wherein the target time is the interval time between the current target task and the last target task corresponding to the target equipment, and the target equipment is measurement and control equipment corresponding to the target spacecraft;
Determining a calibration type of the target device according to the target time information and a preset correction strategy, wherein the calibration type comprises: at least one of the distance-measuring distance leave school zero, the automatic phase correction of angle tracking, the calibration of photoelectric mismatch of angle measurement and the calibration of chassis level of movable equipment;
And generating a calibration task according to the correction strategy and the correction type, wherein the calibration task is used for indicating the execution of the calibration type in the target interval time.
In one embodiment, the processor in the device is further configured to,
Determining a test item of the target equipment according to the analysis result of the target file, wherein the test item comprises test ephemeris data, test theoretical trajectory or comparison data of data downloaded by the on-board positioning equipment, test telemetry data transmission simulation data and monitoring frame synchronization bit error data;
and generating a test task according to the test item, and acquiring a test result.
In one embodiment, the processor in the device is further configured to,
According to the analysis result of the target file, determining a target antenna corresponding to the spacecraft and navigation data corresponding to the spacecraft, wherein the navigation data comprises: station entering instantaneous root data, orbit root data and ephemeris data;
according to the target antenna, acquiring parameter information corresponding to the target antenna, wherein the parameter information comprises: antenna shielding data and positive and negative loop operation limit data;
and generating a capturing task according to the navigation data and the parameter information, wherein the capturing task is used for indicating the target antenna to capture the signal of the target spacecraft.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the disclosure.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the disclosure and together with the description, serve to explain the principles of the disclosure.
FIG. 1 is a flow chart of a device monitoring method provided by an embodiment of the present disclosure;
fig. 2 is a schematic diagram of a monitoring device according to an embodiment of the disclosure.
Detailed Description
Reference will now be made in detail to exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numbers in different drawings refer to the same or similar elements, unless otherwise indicated. The implementations described in the following exemplary examples are not representative of all implementations consistent with the present disclosure. Rather, they are merely examples of apparatus and methods consistent with some aspects of the present disclosure as detailed in the accompanying claims.
An embodiment of the present disclosure provides an apparatus monitoring method, as shown in fig. 1, including the following steps:
101. and obtaining the target file.
The target file is used for indicating task information of each circle of the target equipment; the target files comprise a device operation planning file, a device operation flow file and a device operation parameter file, wherein the device operation planning file is used for determining target devices corresponding to target tasks, the device operation flow file is used for indicating the flow files corresponding to the target devices when the target devices execute the target tasks, and the device operation parameter file is used for indicating the parameter files of the target devices when the target tasks are completed. The target device is a ground measurement and control device for controlling the spacecraft, which comprises satellites.
The target file may be generated by the device monitoring device or may be sent by another device, such as a server, which is used to manage multiple device monitoring devices.
The device monitoring device may be a hardware device, a network server, or the like.
The equipment monitoring equipment is used for managing the ground measurement and control equipment and the spacecraft so as to ensure that the spacecraft can execute navigation commands according to a plan. Furthermore, the equipment monitoring equipment can perform control management such as monitoring management, operation management, calibration processing, capturing tracking, testing and the like on ground measurement and control equipment and a spacecraft; and monitoring and controlling communication equipment, power supply and distribution and security equipment of a preset test place to which the ground measurement and control equipment belongs.
102. And analyzing the target file, and generating a target task according to the analysis result.
According to the method provided by the disclosure, the target task is generated according to the target file, so that the workflow of each device can be generated, each plan and each flow are executed by the organization device according to the time coincidence and the condition coincidence, and the target task is ensured to be used for management.
Wherein running management related tasks may include: at least one of the detection task, calibration task, capture task, etc. are set forth herein by way of three examples and are not representative of the present disclosure.
Example one: and generating a test task.
Determining a test item of the target equipment according to the analysis result of the target file, wherein the test item comprises test ephemeris data, test theoretical trajectory or comparison data of data downloaded by the on-board positioning equipment, test telemetry data transmission simulation data and monitoring frame synchronization bit error data;
and generating a test task according to the test item, and acquiring a test result. And generating alarm information according to the comparison condition of the test result and the test index.
Meanwhile, the monitoring method provided by the disclosure further comprises determining test items and maintenance items of the target equipment according to the target file, wherein the test content comprises all indexes of the equipment; the maintenance content comprises all online maintenance content, software upgrading, computer restarting, log record data cleaning and virus killing.
Example two: generating a calibration task of the ground measurement and control equipment, wherein the calibration task refers to a cooperative work implementation process of the measurement equipment, calibration facilities and geodetic measurement, which are organized by determining that error model parameters of the measurement equipment are aligned with a coordinate system according to a target file.
Acquiring target interval time and target equipment corresponding to the spacecraft according to an analysis result of the target file, wherein the target time is interval time between a current target task corresponding to the target equipment and a last target task, and the target equipment is measurement and control equipment corresponding to the target spacecraft; namely, calibration of the ground measurement and control equipment is completed in an intermittent time period of single navigation of two spacecrafts, so that normal navigation of the spacecrafts can be ensured, and the test control accuracy of the ground measurement and control equipment can be improved
Determining a calibration type of the target device according to the target time information and a preset correction strategy, wherein the calibration type comprises: at least one of the distance-measuring distance leave school zero, the automatic phase correction of angle tracking, the calibration of photoelectric mismatch of angle measurement and the calibration of chassis level of movable equipment;
And generating a calibration task according to the correction strategy and the correction type, wherein the calibration task is used for indicating the execution of the calibration type in the target interval time.
Example three: generating a capturing task of ground measurement and control equipment, wherein the capturing task is used for completing radio tracking measurement of measurement and control and communication of a spacecraft and can also realize the functions of tracking measurement, remote control, remote measurement, communication, image transmission and the like of the spacecraft, and the specific method comprises the following steps of:
according to the analysis result of the target file, determining a target antenna corresponding to the spacecraft and navigation data corresponding to the spacecraft, wherein the navigation data comprises: station entering instantaneous root data, orbit root data and ephemeris data;
according to the target antenna, acquiring parameter information corresponding to the target antenna, wherein the parameter information comprises: antenna shielding data and positive and negative circle operation limiting data, wherein the antenna shielding data are used for determining shielding position information of a target antenna when a target spacecraft signal is captured, and the positive and negative circle operation limiting data refer to the rotating angle range of the target antenna, so that the target antenna can be ensured to timely move in the opposite direction when reaching the limit of the operating angle range, and the target antenna is prevented from being unable to normally use;
and generating a capturing task according to the navigation data and the parameter information, wherein the capturing task is used for instructing the target antenna to capture the signal of the target spacecraft, and the capturing in the capturing task can be frequency capturing, antenna angle tracking, bidirectional carrier capturing, distance capturing and the like.
Further, the generating the capturing task in the above step further includes:
Acquiring switching information corresponding to the spacecraft, wherein the switching information comprises: frequency switching information and telemetry code rate switching information;
And generating the capturing information according to the switching information. The switching information contained in the target file can enable the antenna to switch the capturing strategy according to the switching information, so that data loss caused by the fact that the antenna does not switch the capturing strategy in time when capturing spacecraft signals in the prior art is effectively avoided.
The method provided by the disclosure further comprises the steps of generating a monitoring command according to the target file requirement, sending state data of each device to the server, and uniformly controlling the operation modes by the server. The system monitoring software provides a remote monitoring interface to the outside, and the server can send a command to the remote monitoring interface and receive a command response so as to realize the remote control of the server on the equipment.
103. And sending the target task to the corresponding target equipment in the target task.
The method provided by the disclosure further comprises the step of carrying out confirmation processing according to the task information and the parameter information of the device after the target device acquires the task, and only after the target device passes the confirmation processing, the target task is executed.
The method provided by the disclosure further comprises the steps of collecting environment data, transmitting the environment data to a service or displaying the environment data, generating warning information when the comparison result of the environment data and a preset threshold value does not meet the preset requirement, and generating a corresponding control task according to the warning information.
Acquiring environmental data of a target place corresponding to the target equipment, wherein the environmental data comprises weather data, voltage and current data and security data, and the weather data comprises: indoor and outdoor humiture and disaster weather early warning of the target place;
and generating warning information according to the comparison result of the environment data and the preset threshold value. Collecting reporting, displaying, alarming and local and remote treatment capability.
The weather data can be combined with a station meteorological system to obtain indoor and outdoor humiture of a target place, and the weather data can be used for forecasting local weather and early warning local disasters.
The voltage and current data can be obtained according to the intelligent power subsystem, and the operating conditions of the voltage and current, the commercial power, the UPS and the oil engine are obtained.
The security data can be obtained according to the station security system, and security early warning data can be obtained.
According to the monitoring method provided by the embodiment of the disclosure, after the target file is acquired, the target task corresponding to the ground measurement and control equipment is determined according to the flight task of the spacecraft in the target file, wherein the target task comprises a test task, a calibration task, a capturing task and other tasks, and the task is issued to the ground measurement and control equipment corresponding to the target spacecraft, so that the integrated management of the ground measurement and control equipment is realized. According to the method and the device, when the ground measurement and control equipment is managed according to the target file, equipment parameters of a plurality of different ground measurement and control equipment are acquired, corresponding equipment parameters and operation tasks are set according to the flight task of the spacecraft, the requirements of various task scenes in reality can be met, meanwhile, manual operation is greatly reduced, and equipment management efficiency is improved.
Example two
Based on the device monitoring method described in the foregoing corresponding embodiment of fig. 1, the following is an embodiment of the apparatus of the present disclosure, which may be used to execute an embodiment of the method of the present disclosure.
The embodiment of the present disclosure provides a monitoring device, as shown in fig. 2, the monitoring device 20 includes: a receiver 201, a transmitter 203 and a processor 202,
The processor 202 is connected to the receiver 201 and the transmitter 203, respectively;
the receiver 201 is configured to obtain a target file, where the target file is used to instruct a file corresponding to a target device when the spacecraft performs a flight task, the target file includes a device operation planning file, a device operation flow file, and a device operation parameter file, and the target device is a ground measurement and control device for controlling the spacecraft.
In an alternative implementation, the receiver 201 is also configured to collect satellite telemetry data and device parameter values and transmit them to a database device; database device for storing satellite telemetry data and device parameter values
The processor 202 is configured to parse the target file, generate a target task according to the parsing result, and instruct a target device to operate according to the target file, and set parameters according to the target file.
In an alternative implementation, the processor 202 is further configured to,
Acquiring target interval time and target equipment corresponding to the spacecraft according to an analysis result of the target file, wherein the target time is interval time between a current target task corresponding to the target equipment and a last target task, and the target equipment is measurement and control equipment corresponding to the target spacecraft;
Determining a calibration type of the target device according to the target time information and a preset correction strategy, wherein the calibration type comprises: at least one of the distance-measuring distance leave school zero, the automatic phase correction of angle tracking, the calibration of photoelectric mismatch of angle measurement and the calibration of chassis level of movable equipment;
And generating a calibration task according to the correction strategy and the correction type, wherein the calibration task is used for indicating the execution of the calibration type in the target interval time.
In an alternative implementation, the processor 202 is further configured to,
Determining a test item of the target equipment according to the analysis result of the target file, wherein the test item comprises test ephemeris data, test theoretical trajectory or comparison data of data downloaded by the on-board positioning equipment and test telemetry data transmission monitoring frame synchronization bit error data;
and generating a test task according to the test item, and acquiring a test result.
In an alternative implementation, the processor 202 is further configured to,
According to the analysis result of the target file, determining a target antenna corresponding to the spacecraft and navigation data corresponding to the spacecraft, wherein the navigation data comprises: station entering instantaneous root data, orbit root data and ephemeris data;
according to the target antenna, acquiring parameter information corresponding to the target antenna, wherein the parameter information comprises: antenna shielding data and positive and negative loop operation limit data;
And generating a capturing task according to the navigation data and the parameter information, wherein the capturing task is used for indicating the target antenna to capture the signal of the target spacecraft. The receiver can be used for acquiring the target file
The method can also be used for acquiring acquisition satellite telemetry data, equipment parameter information and monitoring data;
The transmitter 203 is configured to transmit the target task to the target device, where the target device includes a spacecraft.
In an alternative implementation, the transmitter 203 is further configured to transmit satellite telemetry data and device parameter values to a display device, so as to facilitate a human operator in determining the operation of the device monitoring case.
According to the monitoring device provided by the embodiment of the disclosure, after the target file is acquired, the target task corresponding to the ground measurement and control equipment is determined according to the flight task of the spacecraft in the target file, wherein the target task comprises a test task, a calibration task, a capturing task and other tasks, and the task is issued to the ground measurement and control equipment corresponding to the target spacecraft, so that the integrated management of the ground measurement and control equipment is realized. When the ground measurement and control equipment is managed according to the target file, the device parameters of a plurality of different ground measurement and control equipment are compatible, corresponding device parameters and operation tasks are set according to the flight task of the spacecraft, the requirements of various task scenes in reality can be met, meanwhile, manual operation is greatly reduced, and the device management efficiency is improved.
Based on the device monitoring method described in the above embodiment corresponding to fig. 1, the embodiment of the present disclosure further provides a computer readable storage medium, for example, a non-transitory computer readable storage medium may be a Read Only Memory (ROM), a random access Memory (Random Access Memory, RAM), a CD-ROM, a magnetic tape, a floppy disk, an optical data storage device, and the like. The storage medium stores computer instructions for executing the device monitoring method described in the embodiment corresponding to fig. 1, which is not described herein.
Other embodiments of the disclosure will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure disclosed herein. This application is intended to cover any adaptations, uses, or adaptations of the disclosure following, in general, the principles of the disclosure and including such departures from the present disclosure as come within known or customary practice within the art to which the disclosure pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the disclosure being indicated by the following claims.
Claims (8)
1. A device monitoring method, applied to a monitoring apparatus, the method comprising:
Acquiring a target file, wherein the target file is used for indicating a task file corresponding to target equipment when a spacecraft executes a flight task, the target file comprises an equipment operation planning file, an equipment operation flow file and an equipment operation parameter file, and the target equipment is ground measurement and control equipment for controlling the spacecraft;
Analyzing the target file, and generating a target task according to an analysis result, wherein the target task is used for indicating target equipment to operate according to the target file and setting parameters according to the target file;
Sending the target task to the target device;
The generating the target task includes:
Acquiring target interval time and target equipment corresponding to the spacecraft according to the analysis result of the target file, wherein the target interval time is the interval time between a current target task corresponding to the target equipment and a last target task;
Determining a calibration type of the target equipment according to the target interval time and a preset correction strategy, wherein the calibration type comprises: at least one of the distance-measuring distance leave school zero, the automatic phase correction of angle tracking, the calibration of photoelectric mismatch of angle measurement and the calibration of chassis level of movable equipment;
and generating a calibration task according to a correction strategy and the calibration type, wherein the calibration task is used for indicating the calibration type to be executed within the target interval time.
2. The method of claim 1, wherein generating the target task comprises:
Determining test items of the target equipment according to the analysis result of the target file, wherein the test items comprise test ephemeris data, test theoretical trajectory or comparison data of data downloaded by the on-board positioning equipment, test telemetry data transmission simulation data and monitoring frame synchronization bit error data;
and generating a test task according to the test item, and acquiring a test result.
3. The method of claim 1, wherein generating the target task comprises:
determining a target antenna corresponding to the spacecraft and navigation data corresponding to the spacecraft according to the analysis result of the target file, wherein the navigation data comprises: station entering instantaneous root data, orbit root data and ephemeris data;
according to the target antenna, acquiring parameter information corresponding to the target antenna, wherein the parameter information comprises: antenna shielding data and positive and negative loop operation limit data;
and generating a capturing task according to the navigation data and the parameter information, wherein the capturing task is used for indicating the target antenna to capture the signal of the spacecraft.
4. The method of claim 3, wherein generating a capture task further comprises:
Acquiring switching information corresponding to the spacecraft, wherein the switching information comprises: frequency switching information and telemetry code rate switching information;
and generating the capture task according to the switching information.
5. The method according to any one of claims 1-4, further comprising:
acquiring environmental data of a target place corresponding to the target equipment, wherein the environmental data comprises weather data, voltage and current data and security data, and the weather data comprises: indoor and outdoor humiture and disaster weather early warning of the target place;
And generating warning information according to a comparison result of the environment data and a preset threshold value.
6. A monitoring device, comprising: a receiver, a transmitter and a processor,
The processor is respectively connected with the receiver and the transmitter;
The receiver is used for acquiring a target file, wherein the target file is used for indicating a file corresponding to target equipment when a spacecraft executes a flight task, the target file comprises an equipment operation planning file, an equipment operation flow file and an equipment operation parameter file, and the target equipment is ground measurement and control equipment for controlling the spacecraft;
the processor is used for analyzing the target file, generating a target task according to the analysis result, and the target task is used for indicating target equipment to operate according to the target file and setting parameters according to the target file;
the transmitter is used for transmitting the target task to the target equipment;
the processor is further configured to, in response to the processor,
Acquiring target interval time and target equipment corresponding to the spacecraft according to an analysis result of the target file, wherein the target interval time is the interval time between the current target task and the last target task corresponding to the target equipment;
Determining a calibration type of the target equipment according to the target interval time and a preset correction strategy, wherein the calibration type comprises: at least one of the distance-measuring distance leave school zero, the automatic phase correction of angle tracking, the calibration of photoelectric mismatch of angle measurement and the calibration of chassis level of movable equipment;
and generating a calibration task according to a correction strategy and the calibration type, wherein the calibration task is used for indicating the calibration type to be executed within the target interval time.
7. The apparatus of claim 6, wherein the processor is further configured to,
Determining test items of the target equipment according to the analysis result of the target file, wherein the test items comprise test ephemeris data, test theoretical trajectory or comparison data of data downloaded by the on-board positioning equipment, test telemetry data transmission simulation data and monitoring frame synchronization bit error data;
and generating a test task according to the test item, and acquiring a test result.
8. The apparatus of claim 6, wherein the processor is further configured to,
Determining a target antenna corresponding to the spacecraft and navigation data corresponding to the spacecraft according to the analysis result of the target file, wherein the navigation data comprises: station entering instantaneous root data, orbit root data and ephemeris data;
according to the target antenna, acquiring parameter information corresponding to the target antenna, wherein the parameter information comprises: antenna shielding data and positive and negative loop operation limit data;
and generating a capturing task according to the navigation data and the parameter information, wherein the capturing task is used for indicating the target antenna to capture the signal of the spacecraft.
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