CN112219633A - A control method and related device for artificially influencing weather - Google Patents
A control method and related device for artificially influencing weather Download PDFInfo
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- JKFYKCYQEWQPTM-UHFFFAOYSA-N 2-azaniumyl-2-(4-fluorophenyl)acetate Chemical compound OC(=O)C(N)C1=CC=C(F)C=C1 JKFYKCYQEWQPTM-UHFFFAOYSA-N 0.000 description 4
- 229910021612 Silver iodide Inorganic materials 0.000 description 4
- 229940045105 silver iodide Drugs 0.000 description 4
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- A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
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Abstract
The invention relates to a control method and a related device for artificially influencing weather, wherein the control method comprises the following steps: the method comprises the following steps that a weather radar acquires regional meteorological data and analyzes the meteorological data to obtain a regional meteorological result; the operation controller determines a rocket operation target position according to the regional meteorological result, and calculates rocket launching parameters according to the rocket operation target position and the relative position of a rocket launching point, wherein the rocket launching parameters comprise key launching parameters; and the rocket launching device adjusts the key launching parameters according to the rocket launching parameters and launches the rocket to the operation target position. According to the control method for the artificial influence weather, manual intervention is not needed in the whole operation process, the automation degree is greatly improved, the operation target position is accurate, and therefore the operation accuracy of the artificial influence weather is exponentially improved.
Description
Technical Field
The invention relates to the technical field of artificial influence weather, in particular to a control method and a related device for artificial influence weather.
Background
Artificially influencing weather refers to artificially changing weather phenomena towards a direction preset by people, such as artificial precipitation, artificial hail suppression and the like, and is a scientific and technological measure for influencing the physical process in the atmosphere in a local area to change the physical process in the atmosphere through technical means such as artificial catalysis and the like at a certain favorable time and under certain favorable conditions so as to achieve the purpose of lightening or avoiding meteorological disasters. In many areas of China, carriers such as antiaircraft guns, rockets and the like broadcast catalysts such as silver iodide, dry ice and the like to clouds for artificial rain enhancement and hail suppression.
The weather modification rocket launches the catalyst from the ground, explodes in the cloud, and burns the silver iodide in the bomb into smoke agent to be scattered in the cloud. After the rocket reaches a certain height in the cloud, the silver iodide agent starts to be ignited, and along with the flight of the rocket, the rocket is pulled to smoke and spread along the way. The rocket projectile spreads catalysts such as dry ice, silver iodide, salt powder and the like into the cloud to promote precipitation of cloud layers or increase precipitation.
At present, the launching angle of the rocket for artificially influencing weather mainly adopts a manual adjustment mode, an operator roughly judges the target position to be reached by the rocket according to the position of a cloud layer, and then the rocket is launched after adjusting key launching parameters. The prior art has higher requirements on operators and larger selection subjectivity of rocket target positions, so that the misoperation rate of artificially influencing weather is higher.
Based on this, it is necessary to provide a control method of artificially influencing weather with high degree of automation, a control system of artificially influencing weather, a data acquisition method, a weather radar, a data processing method, an operation controller, a rocket launching method, and a rocket launching device, which are used to greatly improve the operation accuracy of artificially influencing weather.
Disclosure of Invention
The embodiment of the application provides a control method and system for artificially influencing weather, which are beneficial to reducing the misoperation rate of artificially influencing weather.
In a first aspect, an embodiment of the present application provides a control method for artificially influencing weather, including the following steps:
the method comprises the following steps that a weather radar acquires regional meteorological data and analyzes the meteorological data to obtain a regional meteorological result;
the operation controller determines a rocket operation target position according to the regional meteorological result, and calculates rocket launching parameters according to the rocket operation target position and the relative position of a rocket launching point, wherein the rocket launching parameters comprise key launching parameters;
and the rocket launching device adjusts the key launching parameters according to the rocket launching parameters and launches the rocket to the operation target position.
In an alternative embodiment, the regional meteorological data is obtained by a combination of PPI and RHI scans.
In a second aspect, an embodiment of the present application provides a control system for artificially influencing weather, including:
the weather radar is used for acquiring regional meteorological data and analyzing the regional meteorological data to obtain a regional meteorological result;
the operation controller is electrically connected with the weather radar, the operation controller can calculate a rocket operation target position according to the regional weather result and calculate rocket launching parameters according to the relative positions of the rocket operation target position and a launching point, and the rocket launching parameters comprise key launching parameters; and
the rocket launching device is electrically connected with the operation controller, and can adjust the key launching parameters according to the launching parameters and launch the rocket to the operation target position.
In a third aspect, an embodiment of the present application provides a data acquisition method, which is applied to a control system for artificially influencing weather, and includes the following steps:
acquiring regional meteorological data;
analyzing the regional meteorological data to obtain a regional meteorological result;
and sending the regional weather result.
In a fourth aspect, an embodiment of the present application provides a weather radar, which is applied to a control system for artificially influencing weather, and includes:
the acquisition module is used for acquiring regional meteorological data;
the analysis module can analyze the regional meteorological data to obtain a regional meteorological result;
and the sending module is used for sending the regional meteorological result.
In a fifth aspect, an embodiment of the present application provides a data processing method, which is applied to a control system for artificially influencing weather, and includes the following steps:
receiving a regional weather result, wherein the regional weather result is obtained by analyzing the acquired regional weather data by a weather radar;
determining a rocket operation target position according to the regional meteorological result;
calculating rocket launching parameters according to the determined rocket operation target position and the relative position of the rocket launching point, wherein the rocket launching parameters comprise key launching parameters; and
and sending the rocket launching parameters.
In a sixth aspect, an embodiment of the present application provides an operation controller, which is applied to a control system for artificially influencing weather, and includes:
the receiving module is used for receiving a regional weather result, wherein the regional weather result is obtained by analyzing the acquired regional weather data by a weather radar;
a target determination module for determining a rocket operation target location;
the computation module can compute rocket launching parameters according to the rocket operation target position and the relative position of a rocket launching point, wherein the rocket launching parameters comprise key launching parameters; and
a sending module for sending the rocket launching parameters.
In an optional embodiment, the job controller further comprises:
the scanning control module is used for controlling a scanning area of the weather radar; and
an echo display module capable of displaying at least echo images of PPI and RHI radars.
In a seventh aspect, an embodiment of the present application provides a rocket launching method, which is applied to a control system for artificially influencing weather, and includes the following steps:
receiving rocket launching parameters, wherein the rocket launching parameters comprise key launching parameters, the rocket launching parameters are obtained by calculation of an operation controller according to the relative position of a rocket operation target position and a rocket launching point, the rocket operation target position is determined by the operation controller according to a regional meteorological result, and the regional meteorological result is obtained by analyzing acquired regional meteorological data through a weather radar;
adjusting the key launching parameters according to the rocket launching parameters;
and launching a rocket to the operation target position.
In an eighth aspect, an embodiment of the present application provides a rocket launching device, which is applied to a weather modification control system, and includes:
the receiving module is used for receiving rocket launching parameters, the rocket launching parameters comprise key launching parameters, the rocket launching parameters are obtained by calculation of the operation controller according to the rocket operation target position and the relative position of a rocket launching point, the rocket operation target position is determined by the operation controller according to the regional meteorological result, and the regional meteorological result is obtained by analyzing the acquired regional meteorological data through the weather radar;
an adjustment module that can adjust the key launch parameter according to the rocket launch parameter;
a launch module to launch a rocket to the operational target location.
In the embodiment of the application, firstly, a weather radar acquires regional meteorological data, and analyzes the meteorological data to obtain a regional meteorological result; secondly, the operation controller determines a rocket operation target position according to the regional meteorological result, and calculates rocket launching parameters according to the relative positions of the rocket operation target position and a rocket launching point, wherein the rocket launching parameters comprise key launching parameters; and finally, the rocket launching device adjusts the key launching parameters according to the rocket launching parameters and launches the rocket to the operation target position.
Therefore, in this embodiment, the control method for artificially influencing weather has the following beneficial effects: the weather radar is used for scanning and analyzing the area space to obtain area weather result data, the operation controller determines the rocket operation target position through the area weather result data and automatically calculates the rocket launching parameters by combining the rocket launching point position, the rocket launching device launches the rocket to the operation target position according to the rocket launching parameters, manual intervention is not needed in the whole operation process, the automation degree is greatly improved, the target position is accurate, and the operation accuracy of artificially influencing weather is improved exponentially.
Drawings
FIG. 1 is a flowchart of a method for controlling weather modification according to an embodiment;
FIG. 2 is a schematic diagram of an embodiment of a weather modification control system;
FIG. 3 is a flow diagram of a data acquisition method according to one embodiment;
FIG. 4 is a block diagram of functional blocks of a weather radar according to an embodiment;
FIG. 5 is a flow diagram of a data processing method according to an embodiment;
FIG. 6 is a block diagram of the functional block components of a job controller according to one embodiment;
FIG. 7 is a block diagram showing functional blocks of a job controller according to another embodiment;
FIG. 8 is a flow diagram of a rocket launch method according to one embodiment;
fig. 9 is a block diagram showing functional blocks of a rocket launching device according to an embodiment.
Detailed Description
In order to make the technical solutions better understood by those skilled in the art, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only partial embodiments of the present application, but not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
The following are detailed below.
The terms "first," "second," "third," and "fourth," etc. in the description and claims of this application and in the accompanying drawings are used for distinguishing between different objects and not for describing a particular order. Furthermore, the terms "include" and "have," as well as any variations thereof, are intended to cover non-exclusive inclusions. For example, a process, method, system, article, or apparatus that comprises a list of steps or elements is not limited to only those steps or elements listed, but may alternatively include other steps or elements not listed, or inherent to such process, method, article, or apparatus.
Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the application. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. It is explicitly and implicitly understood by one skilled in the art that the embodiments described herein can be combined with other embodiments.
The following describes embodiments of the present application in detail.
Referring to fig. 1 and 2, a control method for artificially influencing weather according to an embodiment includes the following steps:
step S010: the weather radar 10 acquires regional weather data and analyzes the weather data to obtain a regional weather result.
The weather radar 10 can emit a series of pulse wireless electromagnetic waves to cloud and rain targets such as clouds, rain, fog and snow in a working area, and obtains regional meteorological data by receiving scattering echoes by using scattering and absorption effects of precipitation particles such as clouds, rain, fog and snow on the electromagnetic waves. The obtained regional meteorological data can be analyzed to obtain regional meteorological result data such as spatial positions, intensity distribution, vertical structures and the like of precipitation particles such as clouds, rain, fog, snow and the like, and the weather radar 10 sends the regional meteorological result data to the operation controller 20.
In one embodiment, the weather radar 10 obtains regional weather data by combining PPI scanning and RHI scanning, where the PPI scanning can obtain plane data of precipitation particles such as cloud, rain, fog, and snow at a certain elevation angle, the RHI scanning can obtain distance and height data of the precipitation particles such as cloud, rain, fog, and snow, and the PPI scanning data and the RHI scanning data are combined to perform analysis, so as to obtain regional weather result data such as spatial positions, intensity distributions, vertical structures, and the like of the precipitation particles such as cloud, rain, fog, and snow.
Step S020: the operation controller 20 determines the rocket operation target position according to the regional meteorological result, and calculates rocket launching parameters according to the rocket operation target position and the relative position of the rocket launching point, wherein the rocket launching parameters comprise key launching parameters.
After receiving the regional weather result data sent by the weather radar 10, the operation controller 20 determines specific spatial coordinates as a rocket operation target position according to the regional weather result data such as the spatial position, the intensity distribution, the vertical structure and the like of precipitation particles such as cloud, rain, fog, snow and the like, and meanwhile, the operation controller 20 automatically calculates rocket launching parameters according to the relative positions of the rocket operation target position and a rocket launching point, wherein the rocket launching parameters comprise key launching parameters, and then the operation controller sends the rocket launching parameters to a rocket launching device.
In this embodiment, the key launch parameters include at least two parameters, azimuth and elevation, of rocket launch, and it should be understood that other parameters that may affect rocket launch may also be used as key launch parameters in the present invention.
Step S030: the rocket launching device 30 adjusts the key launching parameters according to the rocket launching parameters and launches the rocket to the operation target position.
After receiving the rocket launching parameters sent by the operation controller 20, the rocket launching device 30 adjusts the key launching parameters according to the received rocket launching parameters, and determines the parameters of the rocket launching, such as azimuth angle, elevation angle and the like. After the rocket is started to be launched, the rocket can reach a preset operation target position according to preset parameters of azimuth angle, elevation angle and the like of rocket launching.
The control method for artificially influencing the weather has the advantages that: the weather radar 10 is used for scanning and analyzing the area space to obtain area weather result data, the operation controller 20 determines the rocket operation target position through the area weather result data and automatically calculates rocket launching parameters by combining the rocket launching point position, the rocket launching device 30 launches the rocket to the operation target position according to the rocket launching parameters, manual intervention is not needed in the whole operation process, the automation degree is greatly improved, the target position is accurate, and the operation accuracy of artificially influencing weather is exponentially improved.
Referring to fig. 2, an embodiment of a weather modification control system includes: a weather radar 10, an operation controller 20 and a rocket launcher 30.
The weather radar 10 is electrically connected with the operation controller 20, and the weather radar 10 can transmit a series of pulse wireless electromagnetic waves to cloud and rain targets such as cloud, rain, fog and snow in an operation area, utilize scattering and absorption effects of precipitation particles such as the cloud, the rain, the fog and the snow on the electromagnetic waves, and obtain area meteorological data by receiving precipitation particle scattering echoes such as the cloud, the rain, the fog and the snow. The obtained regional weather data can be analyzed to obtain regional weather result data such as spatial position, intensity distribution, vertical structure and the like of the cloud and rain target, and the weather radar 10 sends the regional weather result data to the operation controller 20.
In one embodiment, the weather radar 10 obtains regional weather data by combining PPI scanning and RHI scanning, where the PPI scanning can obtain plane data of precipitation particles such as cloud, rain, fog, and snow at a certain elevation angle, the RHI scanning can obtain distance and height data of the precipitation particles such as cloud, rain, fog, and snow, and the PPI scanning data and the RHI scanning data are combined to perform analysis, so as to obtain regional weather result data such as spatial positions, intensity distributions, vertical structures, and the like of the precipitation particles such as cloud, rain, fog, and snow.
The operation controller 20 is electrically connected with the weather radar 10 and the rocket launching device 30 at the same time, after receiving regional weather result data sent by the weather radar 10, the operation controller 20 determines specific spatial coordinates as a rocket operation target position according to the regional weather result data such as the spatial position, the intensity distribution and the vertical structure of precipitation particles such as cloud, rain, fog and snow, meanwhile, the operation controller 20 automatically calculates rocket launching parameters according to the relative positions of the rocket operation target position and the rocket launching point, the rocket launching parameters comprise key launching parameters, and then the operation controller 20 sends the rocket launching parameters to the rocket launching device 30.
In this embodiment, the key launch parameters include at least two parameters, azimuth and elevation, of rocket launch, and it should be understood that other parameters that may affect rocket launch may also be used as key launch parameters in the present invention.
And the rocket launching device 30 is electrically connected with the operation controller 20, and after receiving the rocket launching parameters sent by the operation controller 20, the rocket launching device 30 adjusts launching parameters such as azimuth angle and elevation angle of rocket launching according to the received rocket launching parameters. After the rocket is started to be launched, the rocket can reach a preset operation target position according to preset rocket launching parameters.
The control system for artificially influencing weather has the beneficial effects that: the weather radar 10 is used for scanning and analyzing the area space to obtain area weather result data, the operation controller 20 determines the rocket operation target position through the area weather result data and automatically calculates rocket launching parameters by combining the rocket launching point position, the rocket launching device 30 launches the rocket to the operation target position according to the rocket launching parameters, manual intervention is not needed in the whole operation process, the automation degree is greatly improved, the target position is accurate, and the operation accuracy of artificially influencing weather is exponentially improved.
Referring to fig. 3 and 4, a data acquisition method according to an embodiment includes the following steps:
step S110: regional meteorological data are acquired.
The weather radar 10 can emit a series of pulse wireless electromagnetic waves to cloud and rain targets such as clouds, rain, fog and snow in a working area, and obtains regional meteorological data by receiving precipitation particles such as clouds, rain, fog and snow scattering echoes by using scattering and absorption effects of precipitation particles such as clouds, rain, fog and snow on the electromagnetic waves.
In one embodiment, the weather radar 10 obtains regional weather data by combining PPI scanning and RHI scanning, where the PPI scanning can obtain plane data of precipitation particles such as cloud, rain, fog, and snow at a certain elevation angle, the RHI scanning can obtain distance and height data of the precipitation particles such as cloud, rain, fog, and snow, and the PPI scanning data and the RHI scanning data are combined to perform analysis, so as to obtain regional weather result data such as spatial positions, intensity distributions, vertical structures, and the like of the precipitation particles such as cloud, rain, fog, and snow.
Step S120: and analyzing the regional meteorological data to obtain regional meteorological result data.
The weather radar 10 may analyze the obtained regional weather data to obtain regional weather result data such as spatial positions, intensity distributions, vertical structures, and the like of precipitation particles such as clouds, rain, fog, snow, and the like.
Step S130: and sending the regional meteorological result data.
The weather radar 10 transmits the weather result data to the task controller 20, thereby providing a basis for the task controller 20 to determine the rocket task target location.
The data acquisition method has the beneficial effects that: the weather radar 10 is used for scanning and analyzing the regional space to obtain regional weather result data, wherein the regional weather result data at least comprise the spatial position, the intensity distribution, the vertical structure and other data of precipitation particles such as cloud, rain, fog, snow and the like, so that a basis is provided for the operation controller 20 to accurately determine the rocket operation target position.
Referring to fig. 4, a weather radar according to an embodiment includes: an acquisition module 101, an analysis module 102 and a sending module 103.
The acquisition module 101 is configured to acquire regional meteorological data, and may transmit a series of pulse wireless electromagnetic waves to a cloud and rain target in a work region, and acquire the regional meteorological data by receiving scattering echoes of precipitation particles such as cloud, rain, fog, and snow by using scattering and absorption effects of the precipitation particles such as cloud, rain, fog, and snow on the electromagnetic waves.
In an embodiment, the obtaining module 101 obtains the regional meteorological data by using a combination of PPI scanning and RHI scanning, where the PPI scanning may obtain plane data of precipitation particles such as clouds, rain, fog, and snow at a certain elevation angle, and the RHI scanning may obtain distance and height data of the precipitation particles such as clouds, rain, fog, and snow.
The analysis module 102 may analyze the regional meteorological data to obtain regional meteorological result data, where the regional meteorological result data at least includes data of spatial positions, intensity distributions, vertical structures, and the like of precipitation particles such as clouds, rain, fog, snow, and the like.
The transmission module 103 may transmit the regional weather result data to the task controller 20, so as to provide a basis for the task controller 20 to determine the rocket task target location.
The weather radar has the beneficial effects that: the weather radar 10 can scan and analyze the regional space to obtain regional weather result data, wherein the regional weather result data at least comprises the spatial position, the intensity distribution, the vertical structure and other data of precipitation particles such as cloud, rain, fog, snow and the like, so that a basis is provided for the operation controller 20 to accurately determine the rocket operation target position.
Referring to fig. 5 and fig. 6, a data processing method according to an embodiment includes the following steps:
step S210: and receiving regional weather result data, wherein the regional weather result data is obtained by analyzing the obtained regional weather data by a weather radar.
The operation controller 20 receives regional weather result data sent by the weather radar 10, wherein the regional weather result data is obtained by analyzing plane data of precipitation particles such as cloud, rain, fog and snow at a certain elevation angle, which is obtained by the weather radar 10 through PPI scanning, and distance and height data of the precipitation particles such as cloud, rain, fog and snow, which is obtained through RHI scanning, and the regional weather result data includes regional weather result data such as spatial positions, intensity distribution and vertical structures of the precipitation particles such as cloud, rain, fog and snow. The weather radar 10 can emit a series of pulse wireless electromagnetic waves to cloud and rain targets such as clouds, rain, fog and snow in a working area, and can obtain area meteorological data by receiving precipitation particles such as clouds, rain, fog and snow and scattering echoes by utilizing scattering and absorption effects of the precipitation particles such as the clouds, the rain, the fog and the snow on the electromagnetic waves. And the acquired regional meteorological data can be analyzed to obtain regional meteorological result data such as the spatial position, the intensity distribution, the vertical structure and the like of the cloud and rain target.
Step S220: and determining the rocket operation target position according to the regional meteorological result.
The operation controller 20 selects a region in which precipitation particles such as clouds, rain, fog, and snow are concentrated as a rocket operation target position based on regional weather result data such as the spatial position, the intensity distribution, and the vertical structure of precipitation particles such as clouds, rain, fog, and snow in the regional weather result data.
Step S230: and calculating rocket launching parameters according to the rocket operation target position and the relative position of the rocket launching point, wherein the rocket launching parameters comprise key launching parameters.
The operation controller 20 automatically calculates rocket launching parameters according to the relative positions of the rocket operation target position and the rocket launching point, wherein the rocket launching parameters comprise key launching parameters.
In this embodiment, the key launch parameters include at least two parameters, azimuth and elevation, of rocket launch, and it should be understood that other parameters that may affect rocket launch may also be used as key launch parameters in the present invention.
Step S240: and sending the rocket launching parameter data.
The task controller 20 sends rocket launch parameters including key launch parameters to the rocket launch device 30.
The beneficial effects of the data processing method are as follows: and calculating rocket launching parameters through the rocket operation target position and the rocket launching relative position, thereby providing a basis for launching the rocket to the rocket operation target position.
Referring to fig. 6, an operation controller according to an embodiment includes: a receiving module 201, an object determining module 203, a calculating module 205 and a sending module 207.
The receiving module 201 is configured to receive a regional weather result, and the receiving module 201 may receive regional weather result data sent by the weather radar 10, where the regional weather result data is obtained by analyzing plane data of precipitation particles such as cloud, rain, fog, and snow at a certain elevation angle, which is obtained by the weather radar 10 through PPI scanning, and distance height data of the precipitation particles such as cloud, rain, fog, and snow, which is obtained through RHI scanning, and the regional weather result data includes regional weather result data such as spatial positions, intensity distributions, and vertical structures of the precipitation particles such as cloud, rain, fog, and snow. The weather radar 10 can emit a series of pulse wireless electromagnetic waves to cloud and rain targets such as clouds, rain, fog and snow in a working area, and can obtain area meteorological data by receiving precipitation particles such as clouds, rain, fog and snow and scattering echoes by utilizing scattering and absorption effects of the precipitation particles such as the clouds, the rain, the fog and the snow on the electromagnetic waves. And the acquired regional meteorological data can be analyzed to obtain regional meteorological result data such as the spatial position, the intensity distribution, the vertical structure and the like of the cloud and rain target.
The target determining module 203 is configured to determine a rocket operation target position, and may determine a specific spatial coordinate as the rocket operation target position according to regional weather result data, such as spatial positions, intensity distributions, vertical structures, and the like of precipitation particles such as clouds, rain, fog, snow, and the like in the regional weather result data.
The calculation module 205, the calculation module 205 may automatically calculate the rocket launching parameters according to the rocket operation target location and the relative location of the rocket launching point, and the rocket launching parameters include key launching parameters.
In this embodiment, the key launch parameters include at least two parameters, azimuth and elevation, of rocket launch, and it should be understood that other parameters that may affect rocket launch may also be used as key launch parameters in the present invention.
A sending module 207 for sending the rocket launching parameters so as to provide the basis for the rocket launching device 30.
The beneficial effect of above-mentioned operation controller is: the task controller 20 receives the precise regional weather result data from the weather radar 10 as a data source, selects a rocket task target location based on the data source, and further calculates rocket launching parameters through the rocket task target location and the rocket launching relative location, thereby providing a basis for launching the rocket to the rocket task target location.
In some embodiments, referring to fig. 7, the job controller further includes an echo display module 202 and a scan control module 211.
An echo display module 202 capable of displaying at least echo images of the PPI and RHI radar so that a user can directly observe regional weather data acquired by the weather radar through the echo display module 202.
Referring to fig. 8 and 9, a rocket launching method according to an embodiment includes the following steps:
step S310: receiving rocket launching parameters, wherein the rocket launching parameters comprise key launching parameters, the rocket launching parameters are obtained by calculation of an operation controller according to the relative position of a rocket operation target position and a rocket launching point, the rocket operation target position is determined by the operation controller according to a regional meteorological result, and the regional meteorological result is obtained by analyzing acquired regional meteorological data through a weather radar.
The rocket launching device 30 receives rocket launching parameters sent by the operation controller 20, and the rocket launching parameters comprise key launching parameters.
The rocket launching parameters are calculated by the operation controller 20, after receiving the regional weather result data sent by the weather radar 10, the operation controller 20 determines specific space coordinates as rocket operation target positions according to the regional weather result data such as the spatial positions, the intensity distribution and the vertical structure of precipitation particles such as cloud, rain, fog and snow, meanwhile, the operation controller 20 automatically calculates the rocket launching parameters according to the rocket operation target positions and the relative positions of rocket launching points, the rocket launching parameters comprise key launching parameters, and then the operation controller 20 sends the rocket launching parameters to the rocket launching device 30. In this embodiment, the key launch parameters include at least two parameters, azimuth and elevation, of rocket launch, and it should be understood that other parameters that may affect rocket launch may also be used as key launch parameters in the present invention.
The regional meteorological result is obtained and analyzed by the weather radar 10, the weather radar 10 can emit a series of pulse wireless electromagnetic waves to cloud and rain targets such as cloud, rain, fog and snow in the operation region, and the regional meteorological data can be obtained by receiving scattering echoes by using scattering and absorption effects of precipitation particles such as cloud, rain, fog and snow on the electromagnetic waves. The obtained regional meteorological data can be analyzed to obtain regional meteorological result data such as spatial positions, intensity distribution, vertical structures and the like of precipitation particles such as clouds, rain, fog, snow and the like, and the weather radar 10 sends the regional meteorological result data to the operation controller 20.
In one embodiment, the weather radar 10 obtains regional weather data by combining PPI scanning and RHI scanning, where the PPI scanning can obtain plane data of precipitation particles such as cloud, rain, fog, and snow at a certain elevation angle, the RHI scanning can obtain distance and height data of the precipitation particles such as cloud, rain, fog, and snow, and the PPI scanning data and the RHI scanning data are combined to perform analysis, so as to obtain regional weather result data such as spatial positions, intensity distributions, vertical structures, and the like of the precipitation particles such as cloud, rain, fog, and snow.
Step S320: and adjusting key launching parameters according to the rocket launching parameters.
After receiving the rocket launching parameters sent by the operation controller 20, the rocket launching device 30 adjusts the key launching parameters according to the received rocket launching parameters, and determines the parameters of the rocket launching, such as azimuth angle, elevation angle and the like.
Step S310: and launching the rocket to the operation target position.
And starting rocket launching, wherein the rocket launching device 30 can launch the rocket to a preset operation target position according to the received rocket launching parameters.
The rocket launching method has the beneficial effects that: by receiving the rocket launching parameters sent by the operation controller 20, the key launching parameters are adjusted, and the rocket is launched to the operation target position according to the key launching parameters. Since the rocket launching parameters are calculated by the operation controller 20 through the selected rocket operation target position and the rocket launching position, and the rocket operation target position is obtained through acquiring meteorological data and accurately analyzing by the weather radar, the rocket launching method can accurately launch the rocket to the operation target position.
Referring to fig. 9, one embodiment of a rocket launch device 30 includes: a receiving module 301, an adjusting module 302 and a transmitting module 303.
The receiving module 301, the receiving module 301 is configured to receive rocket launching parameters, where the rocket launching parameters include key launching parameters, the rocket launching parameters are calculated by the operation controller 20 according to the rocket operation target location and the relative location of the rocket launching point, the rocket operation target location is determined by the operation controller according to the regional weather result, and the regional weather result is obtained by analyzing the acquired regional weather data by the weather radar.
The receiving module 301 receives the rocket launching parameters sent by the operation controller 20, and the rocket launching parameters include key launching parameters.
The rocket launching parameters are calculated by the operation controller 20, after the operation controller 20 receives regional meteorological result data sent by a weather radar, specific spatial coordinates are determined as rocket operation target positions according to the regional meteorological result data such as the spatial positions, the intensity distribution and the vertical structure of precipitation particles such as cloud, rain, fog and snow, meanwhile, the operation controller 20 automatically calculates the rocket launching parameters according to the rocket operation target positions and the relative positions of rocket launching points, the rocket launching parameters comprise key launching parameters, and then the operation controller sends the rocket launching parameters to a rocket launching device. In this embodiment, the key launch parameters include at least two parameters, azimuth and elevation, of rocket launch, and it should be understood that other parameters that may affect rocket launch may also be used as key launch parameters in the present invention.
The regional meteorological result is obtained and analyzed by the weather radar 10, the weather radar 10 can emit a series of pulse wireless electromagnetic waves to cloud and rain targets such as cloud, rain, fog and snow in the operation region, and the regional meteorological data can be obtained by receiving scattering echoes by using scattering and absorption effects of precipitation particles such as cloud, rain, fog and snow on the electromagnetic waves. The obtained regional meteorological data can be analyzed to obtain regional meteorological result data such as spatial positions, intensity distribution, vertical structures and the like of precipitation particles such as clouds, rain, fog, snow and the like, and the weather radar 10 sends the regional meteorological result data to the operation controller 20.
In one embodiment, the weather radar acquires regional weather data by combining PPI scanning and RHI scanning, the PPI scanning can acquire plane data of precipitation particles such as cloud, rain, fog and snow at a certain elevation angle, the RHI scanning can acquire distance and height data of the precipitation particles such as cloud, rain, fog and snow, and the regional weather result data such as the spatial position, the intensity distribution and the vertical structure of the precipitation particles such as cloud, rain, fog and snow can be acquired by combining the PPI scanning data and the RHI scanning data for analysis.
And an adjusting module 302, wherein after receiving the rocket launching parameters sent by the operation controller 20, the adjusting module 302 adjusts the key launching parameters according to the received rocket launching parameters, and determines parameters such as azimuth angle and elevation angle of rocket launching.
And the launching module 303, after the rocket is launched, the launching module 303 can reach a preset operation target position according to preset parameters of azimuth angle, elevation angle and the like of rocket launching.
The rocket launcher has the advantages that: the receiving module 301 receives rocket launching parameters sent by the operation controller, the adjusting module 302 adjusts key launching parameters, and the launching module 303 launches the rocket to an operation target position according to the key launching parameters. Since the rocket launching parameters are calculated by the operation controller 20 through the selected rocket operation target position and the rocket launching position, and the rocket operation target position is obtained through acquiring meteorological data and accurately analyzing by the weather radar, the rocket launching device can accurately launch the rocket to the operation target position.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (10)
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