CN203687785U - Shadow rocket and shadow antiaircraft cooperative control system based on radar information - Google Patents
Shadow rocket and shadow antiaircraft cooperative control system based on radar information Download PDFInfo
- Publication number
- CN203687785U CN203687785U CN201320835740.8U CN201320835740U CN203687785U CN 203687785 U CN203687785 U CN 203687785U CN 201320835740 U CN201320835740 U CN 201320835740U CN 203687785 U CN203687785 U CN 203687785U
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- rocket
- antiaircraft gun
- signal transceiver
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- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
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- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Life Sciences & Earth Sciences (AREA)
- Atmospheric Sciences (AREA)
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Abstract
The utility model discloses a shadow rocket and a shadow antiaircraft cooperative control system based on radar information. A rocket projectile launching system and an antiaircraft gun launching system are controlled and increased by utilizing a command and control industrial personal computer in a rainfall catalyzing system in the prior art, and a weather radar is introduced to provide trajectory calculating basis for the rocket projectile launching system and the antiaircraft gun launching system, so that automatic control for the rocket projectile launching system and the antiaircraft gun launching system is realized, and the problem that more manpower resources need to be consumed since the launching of rocket projectiles and antiaircraft guns are manually controlled by workers in the prior art is solved.
Description
Technical field
The utility model relates to Weather modification operation technical field, relates in particular to a kind of shadow rocket and figure antiaircraft gun cooperative control system based on radar information.
Background technology
At present, the means of weather modification are diversified.Taking Precipitation simulation as example, at present common Catalysis work mode is: 1, adopt the mode of manually the lighting silver iodide that burn on ground, and utilize atmosphere ascending air to carry out catalysis; 2, utilize that to have people to increase rain aircraft be that manned aircraft is implemented the burning of silver iodide flame bar and sowed the mode etc. of carrying out catalysis.
Above-mentioned the 2nd kind of defect that Catalysis work mode exists of the prior art is: someone increases rain aircraft and often flies aerial at height, as bad weather, what the high mixed and disorderly electromagnetic wave producing due to bad weather in the air may cause that someone increases that aircraft control signal transceiver on rain aircraft is difficult to successfully that satellite receiver subsystem sends urges rain notification message, urges rain opportunity thereby probably cause missing the best.
For fear of above-mentioned defect, there is technology to propose to adopt antiaircraft gun or rocket projectile to carry and increase rain catalyst.By increasing the rocket projectile of rain catalyst or antiaircraft gun and be transmitted into appointed area and carry out catalysis rainfall from ground by carrying, can utilize the catalysis rainfall equipment arranging on ground effectively to supplement above-mentioned the 2nd kind of Catalysis work mode, fill up that aircraft control signal transceiver is difficult to successfully that satellite receiver subsystem sends urge rain notification message and cause missed the best and urged rain this leak on opportunity, thereby improve the success rate of catalysis rainfall operation, avoid missing the best and urge rain opportunity.
But the emission control for rocket projectile and antiaircraft gun of the prior art all realizes manually by staff, automaticity is lower, and need to expend more human resources.
Utility model content
The utility model embodiment provides a kind of shadow rocket and figure antiaircraft gun cooperative control system based on radar information, in order to solve the problem that need to expend more human resources in prior art by the transmitting of staff's Artificial Control rocket projectile and antiaircraft gun.
The utility model embodiment is by the following technical solutions:
Shadow rocket based on radar information and a figure antiaircraft gun cooperative control system, comprising:
Send search coverage positional information and urge the commander of rain instruction to control industrial computer;
Treat the target cloud layer of catalysis according to search coverage positional information and follow the tracks of the also weather radar of output tracking result;
Rocket bomb transmitting system and antiaircraft gun emission system; In the antiaircraft gun of the rocket projectile of described rocket bomb transmitting system transmitting and the transmitting of described antiaircraft gun emission system, be all filled with and increase rain catalyst;
Wherein, described weather radar comprises:
Described commander is controlled to described search coverage positional information that industrial computer sends receives and to the target cloud layer in treating catalysis described in search coverage being followed the tracks of to the radar signal transceiver that the tracking results that obtains sends according to described search coverage positional information;
According to described search coverage positional information, the target cloud layer in treating catalysis described in search coverage is followed the tracks of, and tracking results is outputed to the target-sighting apparatus of radar signal transceiver;
Described rocket bomb transmitting system comprises:
Rocket bomb transmitting equipment, the rocket projectile operation control signal transceiver of urging the tracking results that rain instruction and described radar signal transceiver send that receives that described commander controls that industrial computer sends, and the processor launching a rocket shell according to described tracking results control rocket bomb transmitting equipment;
Described antiaircraft gun emission system comprises:
Antiaircraft gun transmitter, the antiaircraft gun operation control signal transceiver of urging the tracking results that rain instruction and described radar signal transceiver send that receives that described commander controls that industrial computer sends, and according to the processor of described tracking results control antiaircraft gun transmitter transmitting antiaircraft gun.
The beneficial effect of the utility model embodiment is as follows:
The utility model embodiment provides above-mentioned shadow rocket projectile based on radar information and antiaircraft gun cooperative control system controlled and increased rocket bomb transmitting system and antiaircraft gun emission system by utilizing commander in catalysis rainfall system of the prior art to control industrial computer, and introduce weather radar and provide ballistic solution foundation for rocket bomb transmitting system and antiaircraft gun emission system, realize the automatic control to rocket bomb transmitting system and antiaircraft gun emission system, solve the problem that need to expend more human resources in prior art by the transmitting of staff's Artificial Control rocket projectile and antiaircraft gun.
Brief description of the drawings
A kind of shadow rocket based on radar information that Fig. 1 provides for the utility model embodiment and the concrete structure schematic diagram of figure antiaircraft gun cooperative control system.
Detailed description of the invention
In prior art, the catalysis rainfall system that realizes the 2nd kind of Catalysis work mode can comprise 4 parts, be respectively meteorological detection subsystem, commander controls industrial computer, and (it is chip or computer or the circuit board for comprising central processing unit often, also claim command and control center equipment), (it is chip or computer or the circuit board for comprising central processing unit often for earth station's industrial computer, Ye Cheng earth station subsystem) and aircraft control signal transceiver is installed, weather environment data acquisition unit (is generally various sensors, for example temperature sensor, humidity sensor etc.), increasing rain catalyst sows equipment and controls and increase rain catalyst and sow equipment the people that has of the control appliance that increases rain catalyst and process is increased to rain aircraft.
Meteorological detection subsystem generally comprises satellite and/or meteorological detection radiation gauge.The function of this meteorological detection subsystem is to gather remote sensing meteorological data and offers command and control center equipment.Depending on the different demands in reality, can be the one or more of satellite and meteorological probe radiation instrument for gathering the equipment of remote sensing meteorological data.
Command and control center equipment is mainly used in: obtain the remote sensing meteorological data that meteorological detection subsystem provides, and determine someone according to remote sensing meteorological data and increase after the search coverage positional information of rain aircraft, send search coverage positional information; And the weather environment data of satellite receiver subsystem transmission, judge whether to urge rain operation in search coverage; And in judged result when being, send and urge rain instruction;
Earth station's subsystem is mainly used in: receive the search coverage positional information that command and control center equipment sends; And according to search coverage positional information, determine and send flight path information to there being people to increase rain aircraft; The weather environment data that have people to increase the transmission of rain aircraft are sent to command and control center equipment; And the rain instruction of urging that command and control center equipment is sent sends to someone to increase rain aircraft.
In addition, rocket bomb transmitting system of the prior art mainly comprises: rocket bomb transmitting controller, processor and rocket launcher.Wherein, rocket bomb transmitting controller, for by the information transmission interface of self, receives manually rocket bomb transmitting instruction and the target position information of input of staff, and is receiving after this rocket bomb transmitting instruction to processor transmission target position information; Processor is used for receiving after target position information, carries out ballistic solution according to target position information, adjusts behind the transmitting inclination angle of rocket launcher according to ballistic solution result, sends firing command to rocket launcher; Rocket launcher is used for installing rocket projectile, and for receiving after firing command, realizes rocket bomb transmitting thereby light rocket projectile lead-in wire.Wherein, rocket bomb transmitting controller can be control circuit, the chip or the computer etc. that comprise CPU; Chip or computer etc. that processor can be control circuit, comprise CPU; Rocket launcher often comprises rocket projectile installing rack, control circuit (can be also chip or the computer etc. that comprises CPU) and igniter etc.
Similarly, antiaircraft gun emission system of the prior art mainly comprises: antiaircraft gun mission controller, processor and antiaircraft gun transmitter.Wherein, antiaircraft gun mission controller, for by the information transmission interface of self, receives manually antiaircraft gun firing order and the target position information of input of staff, and is receiving after this antiaircraft gun firing order to processor transmission target position information; Processor is used for receiving after target position information, carries out ballistic solution according to target position information, adjusts behind the transmitting inclination angle of antiaircraft gun transmitter according to ballistic solution result, sends firing command to antiaircraft gun transmitter; Antiaircraft gun transmitter is used for installing antiaircraft gun, and for receiving after firing command, realizes antiaircraft gun transmitting thereby light antiaircraft gun lead-in wire.Wherein, antiaircraft gun mission controller can be control circuit, the chip or the computer etc. that comprise CPU; Chip or computer etc. that processor can be control circuit, comprise CPU; Antiaircraft gun transmitter often comprises antiaircraft gun installing rack, control circuit (can be also chip or the computer etc. that comprises CPU) and igniter etc.
In the prior art, rocket bomb transmitting controller can receive the triggering signal from control appliance, and sends firing command using this triggering signal as rocket bomb transmitting instruction to corresponding processor; Similarly, antiaircraft gun mission controller also can receive the triggering signal from control appliance, and sends firing command using this triggering signal as antiaircraft gun firing order to corresponding processor.
Further, weather radar of the prior art is a kind of this meteorological detection function that gathers remote sensing meteorological data and send that both possessed, and also possesses target is followed the tracks of to the also radar of the target following function of output tracking result (being generally the coordinate information of target).Corresponding to these two kinds of functions, it both can receive the remote sensing meteorological data collection instruction of sending from the equipment at radar control center, also can receive the target following instruction (can comprise the information of the current position of target to be tracked in this instruction) that this equipment sends.Usually, weather radar can utilize its radar signal transceiver comprising to realize the transmitting-receiving of various signals; And utilize its target-sighting apparatus comprising, realize and treat the tracking of tracking target and tracking results is outputed to radar signal transceiver.Wherein, target-sighting apparatus can be the hardware device such as chip or industrial computer that possesses CPU.Weather radar of the prior art and common active or passive radar are similar, can realize accurate tracking the output tracking result for the treatment of tracking target.
Commander based in catalysis rainfall system of the prior art controls industrial computer and can export the function of catalysis instruction, and the above-mentioned functions of rocket bomb transmitting system, antiaircraft gun emission system and weather radar, the utility model embodiment considers to utilize commander's control industrial computer to come Collaborative Control rocket bomb transmitting system and antiaircraft gun emission system.Further, the utility model embodiment also consider to introduce weather radar for the tracking results of target cloud layer for the treatment of catalysis rainfall as the target position information of the information transmission interface input from antiaircraft gun transmitter and rocket launcher, what make that rocket bomb transmitting system and/or antiaircraft gun emission system can fill up that aircraft control signal transceiver is difficult to successfully that satellite receiver subsystem sends urges rain notification message and causes and miss the best and urge rain this leak on opportunity.
Below in conjunction with Figure of description, embodiment of the present utility model is described, should be appreciated that embodiment described herein, only for description and interpretation the utility model, is not limited to the utility model.And in the situation that not conflicting, the feature in embodiment and embodiment in this explanation can be interosculated.
Particularly, the concrete structure schematic diagram of the utility model embodiment provides a kind of shadow rocket based on radar information and figure antiaircraft gun cooperative control system (hereinafter to be referred as cooperative control system) as shown in Figure 1, comprises following equipment:
Send search coverage positional information and urge the commander of rain instruction to control industrial computer 11;
Treat the target cloud layer of catalysis according to search coverage positional information and follow the tracks of the also weather radar 12 of output tracking result;
Rocket bomb transmitting system 13 and antiaircraft gun emission system 14.
Below illustrate each part of the cooperative control system that the utility model embodiment provides.
Commander controls industrial computer 11:
The function that its commander who comprises with catalysis rainfall system of the prior art controls industrial computer is identical, does not repeat them here.
It should be noted that, in the utility model embodiment, if desired commander controls industrial computer 11 output multi-channel instructions, can be simply commands the mode such as number of the signal output port of control industrial computer 11 to realize by increase.In the utility model embodiment, according to the actual requirements, commander controls industrial computer 11 and can only send and urge rain instruction to rocket bomb transmitting system 13, also can only send and urge rain instruction to antiaircraft gun emission system 14.I.e. commander's control industrial computer 11 can be operated under different control models.Under the first control model, commander controls industrial computer 11 and can send and urge rain instruction to rocket bomb transmitting system 13; Under the second control model, commander controls industrial computer 11 and can send and urge rain instruction to antiaircraft gun emission system 14; Under the third control model, commander controls industrial computer 11 can urge rain instruction to rocket bomb transmitting system 13 and 14 transmissions of antiaircraft gun emission system simultaneously.
Commander is controlled to the search coverage positional information that sends of industrial computer 11 receives and to according to search coverage positional information and the radar signal transceiver sending follow the tracks of the tracking results that obtains in the target cloud layer for the treatment of catalysis of search coverage;
According to search coverage positional information, the target cloud layer for the treatment of catalysis in search coverage is followed the tracks of, and tracking results is outputed to the target-sighting apparatus of radar signal transceiver.
Rocket bomb transmitting system 13, comprising:
Rocket bomb transmitting equipment;
The rocket projectile operation control signal transceiver of the tracking results of urging rain instruction and the transmission of radar signal transceiver that reception commander control industrial computer 11 sends;
The processor launching a rocket shell according to tracking results control rocket bomb transmitting equipment.
The difference of this rocket bomb transmitting system 13 that rocket bomb transmitting system of the prior art and the utility model embodiment provide is: variation has occurred in the source of the signal that the rocket projectile operation control signal transceiver in rocket bomb transmitting system 13 receives, no longer manually inputted by staff, but sent by commander's control industrial computer 11 and radar signal transceiver respectively.
Antiaircraft gun emission system 14, comprising:
Antiaircraft gun transmitter;
The antiaircraft gun operation control signal transceiver of the tracking results of urging rain instruction and the transmission of radar signal transceiver that reception commander control industrial computer 11 sends;
According to the processor of tracking results control antiaircraft gun transmitter transmitting antiaircraft gun.
The difference of this antiaircraft gun emission system 14 that antiaircraft gun emission system of the prior art and the utility model embodiment provide is: variation has occurred in the source of the signal that the antiaircraft gun operation control signal transceiver in antiaircraft gun emission system 14 receives, no longer manually inputted by staff, but sent by commander's control industrial computer 11 and radar signal transceiver respectively.
In the utility model embodiment, in described rocket projectile and described antiaircraft gun, be all filled with and increase rain catalyst.
In the utility model embodiment, the number of rocket bomb transmitting system 13 and antiaircraft gun emission system 14 is not limited.Due to can be by increasing or expand the modes such as signal output port that commander controls industrial computer 12 and radar signal transceiver, make commander control industrial computer 12 and radar signal transceiver outputting multiplex signals, thereby the utility model embodiment can realize the control to multiple rocket bomb transmitting systems 13 and antiaircraft gun emission system 14.
The utility model embodiment provides above-mentioned a kind of shadow rocket based on radar information and figure antiaircraft gun cooperative control system controlled and increased rocket bomb transmitting system and antiaircraft gun emission system by utilizing commander in catalysis rainfall system of the prior art to control industrial computer, and introduce weather radar and provide ballistic solution foundation for rocket bomb transmitting system and antiaircraft gun emission system, realize the automatic control to rocket bomb transmitting system and antiaircraft gun emission system, solve the problem that need to expend more human resources in prior art by the transmitting of staff's Artificial Control rocket projectile and antiaircraft gun.
Obviously, those skilled in the art can carry out various changes and modification and not depart from spirit and scope of the present utility model the utility model.Like this, if these amendments of the present utility model and within modification belongs to the scope of the utility model claim and equivalent technologies thereof, the utility model is also intended to comprise these changes and modification interior.
Claims (2)
1. the shadow rocket based on radar information and a figure antiaircraft gun cooperative control system, is characterized in that, comprising:
Send search coverage positional information and urge the commander of rain instruction to control industrial computer;
Treat the target cloud layer of catalysis according to search coverage positional information and follow the tracks of the also weather radar of output tracking result;
Rocket bomb transmitting system and antiaircraft gun emission system; In the antiaircraft gun of the rocket projectile of described rocket bomb transmitting system transmitting and the transmitting of described antiaircraft gun emission system, be all filled with and increase rain catalyst;
Wherein, described weather radar comprises:
Described commander is controlled to described search coverage positional information that industrial computer sends receives and to the target cloud layer in treating catalysis described in search coverage being followed the tracks of to the radar signal transceiver that the tracking results that obtains sends according to described search coverage positional information;
According to described search coverage positional information, the target cloud layer in treating catalysis described in search coverage is followed the tracks of, and tracking results is outputed to the target-sighting apparatus of radar signal transceiver;
Described rocket bomb transmitting system comprises:
Rocket bomb transmitting equipment, the rocket projectile operation control signal transceiver of urging the tracking results that rain instruction and described radar signal transceiver send that receives that described commander controls that industrial computer sends, and the processor launching a rocket shell according to described tracking results control rocket bomb transmitting equipment;
Described antiaircraft gun emission system comprises:
Antiaircraft gun transmitter, the antiaircraft gun operation control signal transceiver of urging the tracking results that rain instruction and described radar signal transceiver send that receives that described commander controls that industrial computer sends, and according to the processor of described tracking results control antiaircraft gun transmitter transmitting antiaircraft gun.
2. shadow rocket and the figure antiaircraft gun cooperative control system based on radar information as claimed in claim 1, is characterized in that:
Described commander controls industrial computer and adopts wireless connections mode to be connected with described radar signal transceiver;
Described commander controls industrial computer and adopts wireless connections mode to be connected with described rocket projectile operation control signal transceiver;
Described commander controls industrial computer and adopts wireless connections mode to be connected with described antiaircraft gun operation control signal transceiver;
Described radar signal transceiver adopts wireless connections mode to be connected with described rocket projectile operation control signal transceiver;
Described radar signal transceiver adopts wireless connections mode to be connected with described antiaircraft gun operation control signal transceiver;
The processor launching a rocket shell according to described tracking results control rocket bomb transmitting equipment adopts wired or wireless connected mode to be connected with described rocket projectile operation control signal transceiver;
The processor launching a rocket shell according to described tracking results control antiaircraft gun transmitter adopts wired or wireless connected mode to be connected with described antiaircraft gun operation control signal transceiver;
The processor launching a rocket shell according to described tracking results control rocket bomb transmitting equipment adopts wired or wireless connected mode to be connected with described rocket bomb transmitting equipment;
The processor launching a rocket shell according to described tracking results control antiaircraft gun transmitter adopts wired or wireless connected mode to be connected with described antiaircraft gun transmitter;
Described radar signal transceiver adopts wired or wireless connected mode to be connected with described target-sighting apparatus.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320835740.8U CN203687785U (en) | 2013-09-10 | 2013-12-17 | Shadow rocket and shadow antiaircraft cooperative control system based on radar information |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320560943.0 | 2013-09-10 | ||
| CN201320560943 | 2013-09-10 | ||
| CN201320835740.8U CN203687785U (en) | 2013-09-10 | 2013-12-17 | Shadow rocket and shadow antiaircraft cooperative control system based on radar information |
Publications (1)
| Publication Number | Publication Date |
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| CN203687785U true CN203687785U (en) | 2014-07-02 |
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Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310693641.5A Expired - Fee Related CN104412877B (en) | 2013-09-10 | 2013-12-17 | It is a kind of to collect the full-automatic rocket system that radar detection and integration are sowed |
| CN201310693848.2A Expired - Fee Related CN104422351B (en) | 2013-09-10 | 2013-12-17 | A kind of shadow rocket based on radar information and figure antiaircraft gun cooperative control system |
| CN201320835740.8U Withdrawn - After Issue CN203687785U (en) | 2013-09-10 | 2013-12-17 | Shadow rocket and shadow antiaircraft cooperative control system based on radar information |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201310693641.5A Expired - Fee Related CN104412877B (en) | 2013-09-10 | 2013-12-17 | It is a kind of to collect the full-automatic rocket system that radar detection and integration are sowed |
| CN201310693848.2A Expired - Fee Related CN104422351B (en) | 2013-09-10 | 2013-12-17 | A kind of shadow rocket based on radar information and figure antiaircraft gun cooperative control system |
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| CN (3) | CN104412877B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104422351A (en) * | 2013-09-10 | 2015-03-18 | 中国兵器科学研究院 | Figure rocket and figure artillery cooperative control system based on radar information |
| CN106096911A (en) * | 2016-06-03 | 2016-11-09 | 北京理工大学 | A kind of based role have people/unmanned collaborative command and control system and method thereof |
| CN108983314A (en) * | 2018-04-25 | 2018-12-11 | 成都润联科技开发有限公司 | A kind of Weather modification operation safety management application system and its working method |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106688744A (en) * | 2016-12-29 | 2017-05-24 | 雷神科技（天津）有限公司 | Novel artillery rainfall system |
| CN107517793A (en) * | 2017-09-29 | 2017-12-29 | 青海大学 | Artificial snowfall operation device |
| CN108419585A (en) * | 2018-06-01 | 2018-08-21 | 西安华腾微波有限责任公司 | A kind of device of automation Weather modification operation |
| CN110175793B (en) * | 2019-06-14 | 2023-04-25 | 吉林工程技术师范学院 | Artificial precipitation aircraft route design method based on ground demand analysis |
| CN110764091B (en) * | 2019-11-21 | 2020-05-01 | 武义仙合电子有限公司 | Radar device for detecting cloud layer in automatic rainfall |
| CN111373967B (en) * | 2020-04-22 | 2022-01-07 | 广东省突发事件预警信息发布中心(广东省人工影响天气中心) | Rain enhancement operation method and system based on rocket |
| CN111466247B (en) * | 2020-06-22 | 2020-09-22 | 成都信息工程大学 | Catalytic bomb control system and launching method |
| CN112219633A (en) * | 2020-09-21 | 2021-01-15 | 海南省气象科学研究所 | Control method for artificially influencing weather and related device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| JP2961243B2 (en) * | 1996-12-02 | 1999-10-12 | 防衛庁技術研究本部長 | Flying object launch control device and flying object launch control method |
| JP3738521B2 (en) * | 1997-03-24 | 2006-01-25 | 三菱電機株式会社 | Flying object guidance device |
| JP2000088948A (en) * | 1998-09-16 | 2000-03-31 | Toshiba Corp | Radar device |
| JP3978156B2 (en) * | 2003-06-23 | 2007-09-19 | 三菱重工業株式会社 | Weather control method |
| WO2007033448A1 (en) * | 2005-09-19 | 2007-03-29 | Imai Takeshi | Production of localized artificial rains in polar stratospheric clouds, to promote a rain wash in the cio gas, reduce the destruction of the ozone layer and a replacement process in situ of the stratospheric ozone |
| CN100559395C (en) * | 2006-02-23 | 2009-11-11 | 山东省气象科学研究所 | Aircraft artificial rainmaking work technology system |
| CN1845171A (en) * | 2006-02-23 | 2006-10-11 | 山东省气象科学研究所 | Prefecture-level artificial rainfall hail-proof service technique system |
| CN201017230Y (en) * | 2006-11-06 | 2008-02-06 | 山东省气象科学研究所 | Remote control weather modification rocket automatization operation system |
| CN101940140B (en) * | 2010-09-29 | 2011-10-19 | 山东省气象科学研究所 | BL-1 type rocket artificial precipitation method |
| CN102735115A (en) * | 2011-04-08 | 2012-10-17 | 中国兵器工业计算机应用技术研究所 | Remote control method for weather-modification rocket launcher |
| CN102870635A (en) * | 2011-07-15 | 2013-01-16 | 句容天安奇科技有限公司 | Artificial rainfall system |
| CN104412877B (en) * | 2013-09-10 | 2017-07-18 | 中国兵器科学研究院 | It is a kind of to collect the full-automatic rocket system that radar detection and integration are sowed |
-
2013
- 2013-12-17 CN CN201310693641.5A patent/CN104412877B/en not_active Expired - Fee Related
- 2013-12-17 CN CN201310693848.2A patent/CN104422351B/en not_active Expired - Fee Related
- 2013-12-17 CN CN201320835740.8U patent/CN203687785U/en not_active Withdrawn - After Issue
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104422351A (en) * | 2013-09-10 | 2015-03-18 | 中国兵器科学研究院 | Figure rocket and figure artillery cooperative control system based on radar information |
| CN104422351B (en) * | 2013-09-10 | 2016-09-28 | 中国兵器科学研究院 | A kind of shadow rocket based on radar information and figure antiaircraft gun cooperative control system |
| CN106096911A (en) * | 2016-06-03 | 2016-11-09 | 北京理工大学 | A kind of based role have people/unmanned collaborative command and control system and method thereof |
| CN108983314A (en) * | 2018-04-25 | 2018-12-11 | 成都润联科技开发有限公司 | A kind of Weather modification operation safety management application system and its working method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104422351A (en) | 2015-03-18 |
| CN104422351B (en) | 2016-09-28 |
| CN104412877B (en) | 2017-07-18 |
| CN104412877A (en) | 2015-03-18 |
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