CN111854526B - Intelligent artificial precipitation hail suppression rocket operation system and method - Google Patents
Intelligent artificial precipitation hail suppression rocket operation system and method Download PDFInfo
- Publication number
- CN111854526B CN111854526B CN202010161820.4A CN202010161820A CN111854526B CN 111854526 B CN111854526 B CN 111854526B CN 202010161820 A CN202010161820 A CN 202010161820A CN 111854526 B CN111854526 B CN 111854526B
- Authority
- CN
- China
- Prior art keywords
- launching
- controller
- servo controller
- transmitting
- rainfall
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000001556 precipitation Methods 0.000 title claims abstract description 18
- 230000001629 suppression Effects 0.000 title claims abstract description 16
- 238000000034 method Methods 0.000 title claims description 14
- 238000004891 communication Methods 0.000 claims abstract description 24
- 238000001514 detection method Methods 0.000 claims description 20
- 230000005540 biological transmission Effects 0.000 claims description 13
- 238000006073 displacement reaction Methods 0.000 claims description 9
- 238000003860 storage Methods 0.000 claims description 3
- 238000012545 processing Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 230000004888 barrier function Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
- A01G15/00—Devices or methods for influencing weather conditions
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0421—Multiprocessor system
Abstract
The invention discloses an intelligent artificial precipitation hail suppression rocket operation system, which comprises a launching controller, a launching turntable and a launching frame, wherein the launching frame is arranged on the launching turntable, and a launching control terminal is also in communication connection with a command center; the turntable comprises a servo controller; the emission control terminal is in communication connection with the servo controller; the servo controller bus is connected with an azimuth driver for adjusting left and right rotation of the turntable and a pitching driver for adjusting pitching angle of the launching frame; the servo controller is connected with a position feedback unit in a signal mode, and the position feedback unit is arranged on the transmitting frame. The wireless transmitter is connected with the command center and the transmitting turntable in a wireless communication way, and the transmitting turntable is used as an intermediate information receiving feedback point, so that closed-loop control of information is realized, and intelligent automatic artificial rainfall is realized.
Description
Technical Field
The invention belongs to the field of artificial rainfall, and particularly relates to an intelligent artificial precipitation hail suppression rocket operation system and method.
Background
At present, artificial weather (hereinafter referred to as 'figure') operation rocket bullets and launching frames are various in variety, different in form, more and more complex and time-lapse, and form industry barriers and local monopoly of figure equipment gradually, so that the further development of the whole figure industry is not facilitated. In order to break the situation, the whole human shadow industry has long been discussed for realizing standardization and generalization of rocket launchers and realizing separation of the rocket launchers, and the universal rocket launchers cannot be popularized in the ground all the time for various reasons. In order to break the monopoly situation and the industry barrier of the bullet rack of the personal image equipment, the goals of separating the bullet rack and promoting the faster development of the personal image industry are needed.
Aiming at solving the problems of various rocket projectiles and launching frames, different standards, huge volume, heavy weight, large potential safety hazard, low operation efficiency and the like in the prior figure operation, the standardized general rocket launching frame is developed to serve the figure industry.
Disclosure of Invention
The invention provides an intelligent artificial precipitation hail-suppression rocket operation system and method, which solve the problem of artificial precipitation.
The technical scheme adopted by the invention is as follows:
an intelligent artificial precipitation hail suppression rocket operation system comprises an emission controller, an emission turntable and an emission frame, wherein the emission frame is arranged on the emission turntable, and the emission control terminal is also in communication connection with a command center; the turntable comprises a servo controller; the emission control terminal is in communication connection with the servo controller; the servo controller bus is connected with an azimuth driver for adjusting left and right rotation of the turntable and a pitching driver for adjusting pitching angle of the launching frame; the servo controller is connected with a position feedback unit in a signal mode, and the position feedback unit is arranged on the transmitting frame. The wireless transmitter is connected with the command center and the transmitting turntable in a wireless communication way, and the transmitting turntable is used as an intermediate information receiving feedback point, so that closed-loop control of information is realized, and intelligent automatic artificial rainfall is realized.
Further, the position feedback unit comprises a direction feedback unit and a geographic information feedback unit, wherein the direction feedback unit is an electronic compass, and the geographic information feedback unit is a Beidou module or a GPS positioning module.
Further, the servo controller is electrically connected with a displacement sensor for detecting deformation of the track of the launching cradle, the displacement sensor is positioned on the upper side and the lower side of the track of the launching cradle, and detection points are arranged at the top, the middle and the tail of the track. The displacement sensors are arranged at the top, the middle and the tail of the track to detect deformation of the track, when the deformation exceeds a predicted range value, the emission of the rainfall bomb is affected, the rainfall bomb is considered as a cartridge, the automatic detection of the track is realized, and information is collected through the servo controller and transmitted to the emission controller, so that intelligent fault detection is realized.
Further, the launching cradle comprises a plurality of rainfall bullet tracks, and each rainfall bullet track is provided with an independent igniter; each independent igniter is electrically connected with a relay, and the relay is electrically connected with a servo controller; the relay connected with each igniter is electrically connected with an ignition control circuit, and the ignition control circuit comprises an adjustable voltage circuit, a booster circuit, a second relay, a high-voltage switch and a power supply which are electrically connected in sequence; the adjustable voltage circuit is electrically connected with a relay connected with the igniter; the second relay is electrically connected with the servo controller.
Further, the output end of the boost circuit is electrically connected with a voltage detection sensor, and the voltage detection sensor is electrically connected with the servo controller.
Further, the emission controller comprises an industrial flat plate, and the industrial flat plate is electrically connected with a key acquisition plate; the industrial panel comprises a wireless module, a signal interface module, a 4G module, a processor, a screen and a camera module for scanning codes; the servo controller is electrically connected with a wireless module and a signal interface module; the industrial flat plate is in communication connection with the command center through the 4G module; the processor is electrically connected with the signal interface module, the 4G module and the camera module respectively. The two-dimensional code on the rainfall bomb can be scanned through the camera so as to read the basic information of the rainfall bomb, identify whether the rainfall bomb is qualified or not, and realize the automatic detection function of the rainfall bomb.
Further, the transmitting turntable is powered by the storage battery.
Further, the launching cradle adopts a self-adaptive ballistic launching cradle. The launching cradle adopting the self-adaptive trajectory can be compatible to launch rocket projectiles of various types, realize one-cradle multi-projectile launching, and different projectile types can be rapidly loaded through one-time operation by scanning the two-dimension code. The launching frame is designed with a self-adaptive seed-flicking director, an automatic control turntable and an intelligent launching controller, and the operation is convenient and quick.
An intelligent artificial precipitation hail suppression rocket operation method adopts the intelligent artificial precipitation hail suppression rocket operation system, and comprises the following steps that the emission controller is adopted to scan two-dimensional codes of the rainfall bullets to judge rainfall bullet information, if the information accords with preset standards which can be emitted by the rainfall bullets, loading is carried out, otherwise, the rainfall bullets are replaced; when the information of the rainfall bullets accords with the preset standard that the rainfall bullets can be launched, the launching controller sends a rainfall bullet specification signal to the servo controller, and the servo controller adjusts the ballistic size of the launching frame according to the rainfall bullet specification and then carries out loading; after loading, the personnel are evacuated to a safe area, and the position information, the direction and the pitching angle of the launching frame transmitted by the launching turntable are received through the launching controller; turning the launching cradle to a target pointing position; the boost information is sent to the servo controller through the transmitting controller; after the boosting is finished, transmitting information to the servo controller through the transmitting controller to finish transmitting; and after the transmission is successful, the transmission controller generates a transmission log and sends the transmission log to the command center.
The invention has the following advantages and beneficial effects:
1. according to the invention, the wireless transmitter is in wireless communication connection with the command center and the transmitting turntable, and the transmitting turntable is used as an intermediate information receiving feedback point, so that closed-loop control of information is realized, and intelligent automatic artificial rainfall is realized;
2. the launching frame adopts a self-adaptive ballistic launching frame, and the design of the director, the automatic control turntable and the launching controller is convenient and quick to operate;
3. the operation system of the launching frame can rapidly, efficiently, accurately and safely perform artificial precipitation hail suppression operation.
Drawings
The accompanying drawings, which are included to provide a further understanding of embodiments of the invention and are incorporated in and constitute a part of this application, illustrate embodiments of the invention. In the drawings:
FIG. 1 is a block diagram of the system for operating a rack in accordance with the present invention.
FIG. 2 is a schematic block diagram of a servo control system of the present invention.
Fig. 3 is a schematic diagram of the ignition control circuit of the present invention.
Fig. 4 is a schematic diagram of a power distribution network of the present invention.
Fig. 5 is a functional block diagram of a transmit controller of the present invention.
FIG. 6 is a key arrangement diagram of a launch controller in accordance with an embodiment of the present invention.
Detailed Description
For the purpose of making apparent the objects, technical solutions and advantages of the present invention, the present invention will be further described in detail with reference to the following examples and the accompanying drawings, wherein the exemplary embodiments of the present invention and the descriptions thereof are for illustrating the present invention only and are not to be construed as limiting the present invention.
It should be appreciated that the terms first, second, etc. are used merely to distinguish between descriptions and should not be construed as indicating or implying relative importance. Although the terms first, second, etc. may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another element. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of example embodiments of the present invention.
It should be understood that the term "and/or" is merely an association relationship describing the associated object, and means that three relationships may exist, for example, a and/or B may mean: the terms "/and" herein describe another associative object relationship, indicating that there may be two relationships, e.g., a/and B, may indicate that: the character "/" herein generally indicates that the associated object is an "or" relationship.
It should be understood that in the description of the present invention, the terms "upper", "vertical", "inner", "outer", etc. indicate an azimuth or a positional relationship in which the inventive product is conventionally put in use, or an azimuth or a positional relationship that are conventionally understood by those skilled in the art, are merely for convenience of describing the present invention and simplifying the description, and do not indicate or imply that the apparatus or elements referred to must have a specific azimuth, be configured and operated in a specific azimuth, and thus should not be construed as limiting the present invention.
It will be understood that when an element is referred to as being "connected," "connected," or "coupled" to another element, it can be connected or coupled to the other element or intervening elements may be present. In contrast, when an element is referred to as being "directly connected" or "directly coupled" to another element, there are no intervening elements present. Other words used to describe relationships between elements (e.g., "between … …" pair "directly between … …", "adjacent" pair "directly adjacent", etc.) should be interpreted in a similar manner.
In the description of the present invention, it should also be noted that, unless explicitly specified and limited otherwise, the terms "disposed," "mounted," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments of the invention. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, unless the context clearly indicates to the contrary. It will be further understood that the terms "comprises," "comprising," "includes," "including" and/or "including," when used herein, specify the presence of stated features, integers, steps, operations, elements, and/or components, and do not preclude the presence or addition of one or more other features, numbers, steps, operations, elements, components, and/or groups thereof.
Example 1:
as shown in fig. 1, the embodiment provides an intelligent artificial precipitation hail suppression rocket work system, which comprises a launching controller, a launching turntable, a launching frame and a servo control system, wherein the servo control system comprises a control operation processing unit, a signal input unit, a state indicating unit, a motor driving unit and a position feedback unit, the control operation processing unit adopts a servo controller, and the motor driving unit comprises an azimuth driver and a pitching driver; the transmitting frame is arranged on the transmitting turntable, and the transmitting control terminal is also in communication connection with the command center; the servo controller is arranged in the transmitting turntable; the emission control terminal is in communication connection with the servo controller; the servo controller bus is connected with an azimuth driver for adjusting left and right rotation of the turntable and a pitching driver for adjusting pitching angle of the launching frame; the pitching motor selects a UI2486-98-5004A stepping motor of Shanghai you ai Bao intelligent robot science and technology company, and the maximum moment reaches 4.9Nm; the azimuth motor is a stepping motor of UI2457-56-2804A of Shanghai you ai Bao intelligent robot science and technology company, and the maximum moment reaches 1.26Nm; the servo controller is connected with a position feedback unit in a signal mode, and the position feedback unit is arranged on the transmitting frame. The wireless transmitter is connected with the command center and the transmitting turntable in a wireless communication way, and the transmitting turntable is used as an intermediate information receiving feedback point, so that closed-loop control of information is realized, and intelligent automatic artificial rainfall is realized.
In specific implementation, as shown in fig. 2, the position feedback unit includes a direction feedback unit and a geographic information feedback unit, where the direction feedback unit is an electronic compass, and the geographic information feedback unit is a beidou module or a GPS positioning module. The position of the transmitting turntable is positioned through the Beidou module or the GPS positioning module, when the transmitting turntable is positioned in the injection forbidden region, the injection forbidden region is set through a display control interface of the transmitting controller, and the servo system does not respond to the rotation of the injection forbidden region. The servo speed control adopts stepping motor open loop control, the electronic compass outputs the current angle pointing information of the director, and the servo controller completes the control of the motor, the input and output communication of external data and the like according to the system working requirement. The wireless display control is realized through GPS/Beidou positioning and wireless network communication, and the wireless display control is compatible with a wired communication connection mode in specific implementation. In the specific implementation, the pitching rotation of the launching frame can be realized by using a stepping motor through a speed reducer and through worm and gear transmission, and the azimuth rotation of the launching frame is realized by using the stepping motor and a straight tooth gear pair with a large reduction ratio; the hand handles are respectively arranged on the azimuth driving shaft and the pitching driving shaft, so that manual rotation can be realized. And the GPSGPS/Beidou dual-mode positioning module of the positive point atoms is selected to realize the detection of the longitude and latitude and the altitude of the rocket projectile launching frame. The electronic compass is used for measuring the azimuth and the pitching angle of the transmitting bracket and has an angle calibration compensation function. The electronic compass mounting position and the transmitting frame transmitting tube form an angle of 55 degrees, so that the working angle of the electronic compass is always within 60 degrees within the working angle range of the transmitting frame, and the precision of the electronic compass is guaranteed. A Shenzhen remifene science and technology company HCM375B type electronic compass is selected.
During implementation, the servo controller is electrically connected with a displacement sensor for detecting deformation of the track of the launching frame, and Shen Milang technology Co., ltd., KTC2-mm-SL displacement sensors are selected during implementation, the displacement sensors are located on the upper side and the lower side of the track of the launching frame, and detection points are arranged on the top, the middle and the tail of the track. The displacement sensors are arranged at the top, the middle and the tail of the track to detect deformation of the track, when the deformation exceeds a predicted range value, the emission of the rainfall bomb is affected, the rainfall bomb is considered as a cartridge, the automatic detection of the track is realized, and information is collected through the servo controller and transmitted to the emission controller, so that intelligent fault detection is realized. When in specific implementation, the servo controller comprises a CPU processing module, an interface control module, an I/O control module, a power conversion module, a bottom plate and the like. The CPU processing module mainly comprises a DSP processor TMS320F28335 and an FPGA logic unit EP2C8T144I 8N. The DSP processor TMS320F28335 mainly realizes processing of control commands of the handheld terminal and realizes the task of transferring the turntable. The DSP realizes load rotation speed control through CAN communication. The FPGA logic unit realizes the data input/output interface processing and related logic control signal processing functions.
In specific implementation, the launching frame comprises a plurality of rainfall bullet tracks, and each rainfall bullet track is provided with an independent igniter; each independent igniter is electrically connected with a relay, and the relay is electrically connected with a servo controller; the relay connected with each igniter is electrically connected with the booster circuit, and the booster circuit comprises an adjustable voltage circuit, a booster circuit, a second relay, a high-voltage switch and a power supply which are electrically connected in sequence; as shown in fig. 3, the adjustable voltage circuit is electrically connected to a relay to which the igniter is connected; the second relay is electrically connected with the servo controller. The servo controller receives the boosting instruction through wired communication or wireless communication, controls the second relay and starts the boosting circuit to boost; after boosting, the transmitting controller transmits a transmitting signal corresponding to the trajectory, and the servo controller receives the signal and then controls the relay corresponding to the trajectory so as to enable the igniter to ignite, so that independent ignition control of the trajectory is realized, and the practicability is high. In specific implementation, after the launching controller scans the two-dimensional code of the rocket projectile, the servo system automatically acquires technical parameters of the rocket projectile and configures corresponding ignition conditions (ignition voltage, ignition current, ignition pulse duration and the like) for the rocket projectile according to the self-adaptive projectile type ignition control circuit. The output voltage of the booster circuit is the highest emission voltage required by all rocket projectiles, and the adjustable voltage circuit can output the emission voltage required by other projectile species, so that the self-adaptive projectile species ignition condition configuration is realized. After the boost button is pressed down, the boost relay is conducted, the voltage detection sensor detects whether the ignition voltage is normal and feeds back to the controller, and after all the ignition voltages are normal, the corresponding relays are controlled to be conducted by pressing the emission keys of the four channels respectively, so that ignition can be realized.
In specific implementation, the output end of the boost circuit is electrically connected with a voltage detection sensor, and the voltage detection sensor is electrically connected with the servo controller. The voltage condition of the boost circuit is detected by the voltage detection sensor, the voltage condition is fed back to the servo controller, and the servo controller transmits signals to the emission controller, so that whether the boost is ready is remotely checked.
In specific implementation, as shown in fig. 5, the emission controller includes an industrial flat board, and the industrial flat board is electrically connected with a key acquisition board; the industrial panel comprises a wireless module, a signal interface module, a 4G module, a processor, a screen and a camera module for scanning codes; the servo controller is electrically connected with a wireless module and a signal interface module; the industrial flat plate is in communication connection with the command center through the 4G module; the processor is electrically connected with the signal interface module, the 4G module and the camera module respectively. The two-dimensional code on the rainfall bomb can be scanned through the camera so as to read the basic information of the rainfall bomb, identify whether the rainfall bomb is qualified or not, realize the automatic detection function of the rainfall bomb, and judge whether the rainfall bomb is an overdue bomb or a problem bomb by detecting the content including the rainfall date when the automatic detection function is implemented. In practice, the keyboard design is performed as shown in fig. 6. Key indicator light interpretation:
channel 1-4 indicator lights: the rocket projectile resistance value normally displays green, and if the rocket projectile resistance value exceeds the range, the rocket projectile resistance value displays red;
underpower indicator lamp: the key collection board indicates the power supply, is green and normal, and extinguishes or flashes to indicate the power supply is abnormal;
boost indicator light: the servo voltage is green when the servo voltage is increased successfully, and red when the servo voltage is increased successfully;
emission pilot lamp: when the light is emitted normally, green is displayed, and when the light is emitted abnormally, red is displayed;
azimuth key: four mutually exclusive keys are adopted, and when one key is pressed down, the other three keys are automatically sprung up; the high, medium and low represent that the three speeds can be respectively changed at a high speed of 40 DEG/s, a medium speed of 20 DEG/s and a low speed of 5 DEG/s on the azimuth plane.
Pitch key: three mutually exclusive keys are adopted, and the high and low states are rotated at the two speeds of 10 degrees/s at a high speed and 2.5 degrees/s at a low speed on the nodding surface;
emergency key: two mutually exclusive keys are adopted for cutting off or opening a system power supply in emergency;
detecting keys: the resistance values of the 4-channel rocket shell are detected by a servo system when the self-reset key is pressed;
boost key: adopting a self-reset key to boost the pressure of the igniter by one key;
emission key: and a self-reset key is adopted to execute the rocket projectile launching operation, and four launching channels are independently controlled.
In specific implementation, the transmitting turntable is powered by a 24V storage battery. The implementation is shown in fig. 4.
In specific implementation, the launching cradle adopts a self-adaptive ballistic launching cradle. The launching cradle is provided with a contact igniter and a wiring type igniter, and is suitable for rainfall bullets with various ignition modes.
In specific implementation, the automatic control function includes:
1) Automatically controlling the space between the transmitting tracks to adapt to different bullet types;
2) Automatically controlling the azimuth/elevation angle of the launching frame;
3) And (3) self-adaptive bullet ignition control, wherein a servo system automatically acquires rocket bullet technical parameters and configures corresponding ignition conditions, such as ignition voltage, ignition current, ignition pulse duration and the like.
Example 2:
an intelligent artificial precipitation hail suppression rocket operation method adopts the intelligent artificial precipitation hail suppression rocket operation system, and comprises the following steps that the emission controller is adopted to scan two-dimensional codes of the rainfall bullets to judge rainfall bullet information, if the information accords with preset standards which can be emitted by the rainfall bullets, loading is carried out, otherwise, the rainfall bullets are replaced; when the information of the rainfall bullets accords with the preset standard that the rainfall bullets can be launched, the launching controller sends a rainfall bullet specification signal to the servo controller, and the servo controller adjusts the ballistic size of the launching frame according to the rainfall bullet specification and then carries out loading; after loading, the personnel are evacuated to a safe area, and the position information, the direction and the pitching angle of the launching frame transmitted by the launching turntable are received through the launching controller; turning the launching cradle to a target pointing position; the boost information is sent to the servo controller through the transmitting controller; after the boosting is finished, transmitting information to the servo controller through the transmitting controller to finish transmitting; and after the transmission is successful, the transmission controller generates a transmission log and sends the transmission log to the command center.
In specific implementation, the code scanning function is as follows: and (5) scanning the two-dimensional code of the bullet body to automatically acquire information such as rocket bullet model, bullet length, bullet diameter, overdue/problem bullet and the like.
The foregoing description of the embodiments has been provided for the purpose of illustrating the general principles of the invention, and is not meant to limit the scope of the invention, but to limit the invention to the particular embodiments, and any modifications, equivalents, improvements, etc. that fall within the spirit and principles of the invention are intended to be included within the scope of the invention.
Claims (4)
1. An intelligent artificial precipitation hail suppression rocket operation method is characterized in that: an intelligent artificial precipitation hail suppression rocket operation system is adopted, the system comprises a launching controller, a launching turntable and a launching frame, the launching frame is arranged on the launching turntable, and the launching controller is also in communication connection with a command center; the transmitting turntable comprises a servo controller; the emission controller is in communication connection with the servo controller; the servo controller bus is connected with an azimuth driver for adjusting left and right rotation of the transmitting turntable and a pitching driver for adjusting pitching angle of the transmitting frame; the servo controller is in signal connection with a position feedback unit which is arranged on the transmitting frame; the launching frame adopts a self-adaptive ballistic launching frame; the emission controller comprises an industrial flat plate, and the industrial flat plate is electrically connected with a key acquisition plate; the industrial panel comprises a wireless module, a signal interface module, a 4G module, a processor, a screen and a camera module for scanning codes; the servo controller is electrically connected with a wireless module and a signal interface module; the industrial flat plate is in communication connection with the command center through the 4G module; the processor is electrically connected with the signal interface module, the 4G module and the camera module respectively;
the method comprises the following steps that the emission controller is adopted to scan the two-dimensional code of the rainfall bomb to judge the information of the rainfall bomb, if the information accords with the preset standard that the rainfall bomb can emit, loading is carried out, otherwise, the rainfall bomb is replaced; when the information of the rainfall bullets accords with the preset standard that the rainfall bullets can be launched, the launching controller sends a rainfall bullet specification signal to the servo controller, and the servo controller adjusts the ballistic size of the launching frame according to the rainfall bullet specification and then carries out loading; after loading, the personnel are evacuated to a safe area, and the position information, the azimuth and the pitching angle of the launching frame transmitted by the launching turntable are received through the launching controller; turning the launching cradle to a target pointing position; the boost information is sent to the servo controller through the transmitting controller; after the boosting is finished, transmitting information to the servo controller through the transmitting controller to finish transmitting; after the transmission is successful, the transmission controller generates a transmission log and sends the transmission log to the command center;
the launching frame comprises a plurality of rainfall bullet tracks, and each rainfall bullet track is provided with an independent igniter; each independent igniter is electrically connected with a relay, and the relay is electrically connected with a servo controller; the relay connected with each igniter is electrically connected with an ignition control circuit, and the ignition control circuit comprises an adjustable voltage circuit, a booster circuit, a second relay, a high-voltage switch and a power supply which are electrically connected in sequence; the adjustable voltage circuit is electrically connected with a relay connected with the igniter; the second relay is electrically connected with the servo controller; the transmitting controller remotely transmits a boosting command, the servo controller receives the boosting command through wired communication or wireless communication, controls the second relay, and starts the boosting circuit to boost voltage; after the boosting is finished, the emission controller sends emission signals corresponding to the trajectory, and the servo controller receives the signals and controls relays corresponding to the trajectory so that the igniter ignites, and therefore independent ignition control of the trajectory is achieved;
the output end of the ignition control circuit is electrically connected with a voltage detection sensor, and the voltage detection sensor is electrically connected with a servo controller; the voltage detection sensor detects the voltage condition of the ignition control circuit and feeds the voltage condition back to the servo controller, and the servo controller transmits a signal to the emission controller so as to remotely check whether the boosting is ready;
after the emission controller scans the two-dimension codes of the raindrops, the servo controller automatically acquires technical parameters of the raindrops and configures corresponding ignition voltage, ignition current and ignition pulse duration for the raindrops through the ignition control circuit, the output voltage of the booster circuit is the highest emission voltage required by all the raindrops, and then the emission voltage required by other raindrops in specification is output through the adjustable voltage circuit, so that the self-adaptive configuration of the ignition conditions of the raindrops is realized.
2. The intelligent artificial precipitation hail suppression rocket work method according to claim 1, wherein the method comprises the following steps: the position feedback unit comprises a position feedback unit and a geographic information feedback unit, wherein the position feedback unit is an electronic compass, and the geographic information feedback unit is a Beidou module or a GPS positioning module.
3. The intelligent artificial precipitation hail suppression rocket work method according to claim 1, wherein the method comprises the following steps: the servo controller is electrically connected with a displacement sensor for detecting deformation of the track of the launching cradle, the displacement sensor is positioned on the upper side and the lower side of the track of the launching cradle, and detection points are arranged at the top, the middle and the tail of the track.
4. The intelligent artificial precipitation hail suppression rocket work method according to claim 1, wherein the method comprises the following steps: the transmitting turntable is powered by a storage battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010161820.4A CN111854526B (en) | 2020-03-10 | 2020-03-10 | Intelligent artificial precipitation hail suppression rocket operation system and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010161820.4A CN111854526B (en) | 2020-03-10 | 2020-03-10 | Intelligent artificial precipitation hail suppression rocket operation system and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111854526A CN111854526A (en) | 2020-10-30 |
| CN111854526B true CN111854526B (en) | 2024-01-26 |
Family
ID=72985524
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010161820.4A Active CN111854526B (en) | 2020-03-10 | 2020-03-10 | Intelligent artificial precipitation hail suppression rocket operation system and method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111854526B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114427803A (en) * | 2021-12-24 | 2022-05-03 | 湖南金翎箭信息技术有限公司 | Anti-frog grenade positioning control system and control method |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201016649Y (en) * | 2006-10-23 | 2008-02-06 | 新疆维吾尔自治区人工影响天气办公室 | Multifunctional artificial hail-proof rain-increasing rocket pod and emission controller thereof |
| CN101441065A (en) * | 2008-08-21 | 2009-05-27 | 中国科学院长春光学精密机械与物理研究所 | Tiny displacement deforming high precision and non-contact type measuring system and method |
| CN202442650U (en) * | 2012-02-17 | 2012-09-19 | 江苏众普智能物联科技有限公司 | Integrated control device for vehicle-mounted police equipment |
| CN103031787A (en) * | 2013-01-10 | 2013-04-10 | 中铁七局集团第一工程有限公司 | Method and device for fully automatically and accurately monitoring changes of geometric parameters of track |
| CN203490491U (en) * | 2013-09-03 | 2014-03-19 | 中国兵器科学研究院 | Weather-modification precipitation-increasing remote-control operation system through rocket |
| CN103644786A (en) * | 2013-12-03 | 2014-03-19 | 桂林航天电子有限公司 | High-voltage ignition relay and operating method thereof |
| CN104315921A (en) * | 2014-10-17 | 2015-01-28 | 太原融盛科技有限公司 | Rain-increasing antihail rocket projectile launching device |
| CN205228284U (en) * | 2015-12-30 | 2016-05-11 | 陕西中天火箭技术股份有限公司 | Full -automatic precipitation of hail of rockets launcher control system |
| CN106127445A (en) * | 2016-08-30 | 2016-11-16 | 成都润联科技开发有限公司 | The monitoring system of a kind of weather modification ammunition based on Internet of Things and method thereof |
| CN205808244U (en) * | 2016-06-07 | 2016-12-14 | 陕西中天火箭技术股份有限公司 | A kind of rocket-firing system based on radio frequency reading technology |
| CN212512704U (en) * | 2020-03-10 | 2021-02-09 | 成都润联科技开发有限公司 | Intelligent artificial precipitation-increasing hail-suppression rocket operation system |
-
2020
- 2020-03-10 CN CN202010161820.4A patent/CN111854526B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201016649Y (en) * | 2006-10-23 | 2008-02-06 | 新疆维吾尔自治区人工影响天气办公室 | Multifunctional artificial hail-proof rain-increasing rocket pod and emission controller thereof |
| CN101441065A (en) * | 2008-08-21 | 2009-05-27 | 中国科学院长春光学精密机械与物理研究所 | Tiny displacement deforming high precision and non-contact type measuring system and method |
| CN202442650U (en) * | 2012-02-17 | 2012-09-19 | 江苏众普智能物联科技有限公司 | Integrated control device for vehicle-mounted police equipment |
| CN103031787A (en) * | 2013-01-10 | 2013-04-10 | 中铁七局集团第一工程有限公司 | Method and device for fully automatically and accurately monitoring changes of geometric parameters of track |
| CN203490491U (en) * | 2013-09-03 | 2014-03-19 | 中国兵器科学研究院 | Weather-modification precipitation-increasing remote-control operation system through rocket |
| CN103644786A (en) * | 2013-12-03 | 2014-03-19 | 桂林航天电子有限公司 | High-voltage ignition relay and operating method thereof |
| CN104315921A (en) * | 2014-10-17 | 2015-01-28 | 太原融盛科技有限公司 | Rain-increasing antihail rocket projectile launching device |
| CN205228284U (en) * | 2015-12-30 | 2016-05-11 | 陕西中天火箭技术股份有限公司 | Full -automatic precipitation of hail of rockets launcher control system |
| CN205808244U (en) * | 2016-06-07 | 2016-12-14 | 陕西中天火箭技术股份有限公司 | A kind of rocket-firing system based on radio frequency reading technology |
| CN106127445A (en) * | 2016-08-30 | 2016-11-16 | 成都润联科技开发有限公司 | The monitoring system of a kind of weather modification ammunition based on Internet of Things and method thereof |
| CN212512704U (en) * | 2020-03-10 | 2021-02-09 | 成都润联科技开发有限公司 | Intelligent artificial precipitation-increasing hail-suppression rocket operation system |
Non-Patent Citations (1)
| Title |
|---|
| 物联网技术在广东人工影响天气安全管理中的应用;赵博等;广东气象;第40卷(第02期);第48-50页 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111854526A (en) | 2020-10-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111854526B (en) | Intelligent artificial precipitation hail suppression rocket operation system and method | |
| CN112556491B (en) | Automatic missile horizontal filling system based on visual alignment and operation method thereof | |
| KR20140060543A (en) | Remote weapon station, in particular for aircraft, such as fixed-wing aircraft | |
| CN110624189B (en) | Unmanned aerial vehicle-mounted fire extinguishing bomb device, fire-fighting unmanned aerial vehicle and emission control method | |
| CN212512704U (en) | Intelligent artificial precipitation-increasing hail-suppression rocket operation system | |
| CN110058580B (en) | Novel wheel type self-propelled gun electrical system comprehensive diagnosis platform | |
| CN106628142A (en) | Unmanned aerial vehicle for air sampling detection and combustible and explosive gas pre-warning and monitoring | |
| CN108100187A (en) | A kind of automatic lifesaving circle | |
| CN201334116Y (en) | Hovering police reconnaissance flight vehicle with infra-red range measuring function | |
| CN107942348B (en) | Road law enforcement system based on unmanned aerial vehicle and robot technique | |
| CN106742015A (en) | The flight system and its control method of a kind of automobile control unmanned plane | |
| CN207095389U (en) | A kind of laser beam emitting device of adjustable firing direction | |
| CN116343438A (en) | Leakage alarm device for environment-friendly gas insulation equipment | |
| CN110618358A (en) | Flying on-line and off-line insulator string detection robot system, platform and method | |
| KR100460522B1 (en) | Analysis Method of Target Impact Point for Heavy firearms And System for Use in Such Method | |
| KR20230121479A (en) | Remote Monitoring System using Tethered Drone Station using the same | |
| CN212515479U (en) | Unmanned aerial vehicle cluster system | |
| CN211417591U (en) | Unmanned aerial vehicle of propaganda directed to communicate and propaganda directed to communicate carrying device thereof | |
| CN110645834A (en) | Intelligent wushu ware station control system | |
| CN207181680U (en) | Police radar detects car and police low latitude detecting system | |
| CN112611280B (en) | Intelligent cooperative explosion initiating system in movie and television shooting and control method | |
| CN115200415A (en) | High-precision automatic target-reporting control system and method for conductive target plate | |
| CN206695684U (en) | A kind of robot weapon emitter of portable missile | |
| CN114310936A (en) | Circuit control system for intelligent inspection robot | |
| CN117685824A (en) | Portable air defense missile automatic launching system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |