CN115376379B - Unmanned aerial vehicle electronic war simulation efficiency supporting system and method - Google Patents
Unmanned aerial vehicle electronic war simulation efficiency supporting system and method Download PDFInfo
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- CN115376379B CN115376379B CN202210990475.4A CN202210990475A CN115376379B CN 115376379 B CN115376379 B CN 115376379B CN 202210990475 A CN202210990475 A CN 202210990475A CN 115376379 B CN115376379 B CN 115376379B
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- G—PHYSICS
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- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/003—Simulators for teaching or training purposes for military purposes and tactics
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- G—PHYSICS
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- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/085—Special purpose teaching, e.g. alighting on water, aerial photography
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- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/30—Simulation of view from aircraft
- G09B9/301—Simulation of view from aircraft by computer-processed or -generated image
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Abstract
The invention provides an unmanned aerial vehicle electronic warfare simulation efficiency supporting system, which relates to the field of unmanned aerial vehicles and comprises a communication base station, wherein a supporting and carrying platform is arranged above the communication base station, a lift-off platform is arranged above the supporting and carrying platform, a weapon interference platform and a shooting platform are respectively arranged on the left side and the right side of the supporting and carrying platform, a photovoltaic power generation platform is arranged below the weapon interference platform, and a first connecting wire is fixedly connected to the top of the communication base station. The photovoltaic power generation platform lift-off platform is installed and carried through the first lifting line and the second lifting line respectively, and the third lifting line and the fourth lifting line carry and assemble the weapon interference platform and the shooting platform respectively, so that a plurality of platforms are supported and installed conveniently, a plurality of platforms are installed, a plurality of functions are carried, and the use effect is improved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle electronic warfare simulation efficiency supporting system and method.
Background
Unmanned aerial vehicle is simply unmanned aerial vehicle, unmanned aerial vehicle is the unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, perhaps by on-vehicle computer is operated independently entirely or intermittently, unmanned aerial vehicle is according to the application, can divide into for military use and civilian, for military use, unmanned aerial vehicle divides into reconnaissance and target aircraft, for civilian, unmanned aerial vehicle adds the trade application, unmanned aerial vehicle electronic combat simulation refers to military unmanned aerial vehicle, wherein, unmanned aerial vehicle is in the simulation test of anti-efficiency research, offer the support for electronic countermeasure system fight demonstration evaluation, test, training etc. electronic countermeasure system efficiency simulation is important component content therein, because in the development to multiple in electronic countermeasure, electronic countermeasure field has put forward higher wider application demand to imitate straight realization and application, not only need to satisfy the demonstration of single weapon equipment, debug, test training and teaching, but also need to support by many platforms, finally because unmanned aerial vehicle can only play simple reconnaissance, and unmanned aerial vehicle can not take the unstability that the shooting probably caused by reconnaissance in the process of reconnaissance.
In order to enhance the installation of the simulation efficacy support to multiple platforms, reduce the multifunctional of the unmanned aerial vehicle electronic warfare simulation efficacy support to the multiple platforms, and solve the reconnaissance of the multiple platforms in the carrying process, the method is an important method for solving the multiple platforms of the unmanned aerial vehicle, so as to enhance the multifunctional of the unmanned aerial vehicle, the unmanned aerial vehicle is unstable in shooting due to the fact that the examination shooting is not ideal in the reconnaissance process, and the unmanned aerial vehicle does not have the protection or the force function, and based on the problems, the unmanned aerial vehicle electronic warfare simulation efficacy support system is provided.
Disclosure of Invention
(one) solving the technical problems
Aiming at the defects of the prior art, the invention provides an unmanned aerial vehicle electronic war simulation efficiency supporting system, which solves the problem that an important method for carrying a plurality of platforms of an unmanned aerial vehicle is adopted to enhance the multifunction of the unmanned aerial vehicle, the unmanned aerial vehicle possibly causes unstable shooting due to non-ideal shooting during the reconnaissance process, and the unmanned aerial vehicle does not have the protection or force function.
(II) technical scheme
In order to achieve the above purpose, the invention is realized by the following technical scheme: the unmanned aerial vehicle electronic war simulation efficiency supporting system comprises a communication base station, wherein a supporting carrying platform is arranged above the communication base station, an elevating platform is arranged above the supporting carrying platform, weapon interference platforms and shooting platforms are respectively arranged on the left side and the right side of the supporting carrying platform, a photovoltaic power generation platform is arranged below the weapon interference platforms, a first connecting wire is fixedly connected to the top of the communication base station, a lifting hook receiving module is fixedly connected to the tail end of the first connecting wire, and a supporting component is connected to the top of the lifting hook receiving module;
the top of the communication base station is fixedly connected with an assembly line, the surface of the lift-off platform is fixedly connected with a flight control simulation system, the tail end of the assembly line is fixedly connected with the flight control simulation system, the top of the flight control simulation system is fixedly connected with a first branch line, and the tail end of the first branch line is fixedly connected with a lift-off assembly;
the top of the communication base station is fixedly connected with a first installation line, the tail end of the first installation line is fixedly connected with a solar battery pack, the back of the solar battery pack is fixedly connected with a photovoltaic power generation platform, and the top of the solar battery pack is connected with a photovoltaic module;
the communication base station is characterized in that a first fixed line is fixedly connected to the side wall of the communication base station, a simulation interference system is fixedly connected to the tail end of the first fixed line, the back of the simulation interference system is fixedly connected with a weapon interference platform, and a weapon interference assembly is connected to the top of the simulation interference system;
the communication base station side wall fixedly connected with a first transmission line, the tail end of the first transmission line is connected with a camera control module, the back of the camera control module is fixedly connected with a shooting platform, and the top of the camera control module is connected with a shooting assembly.
As a further description of the above technical solution:
the supporting component comprises a second connecting wire fixedly connected with the top of the lifting hook receiving module, the tail end of the second connecting wire is fixedly connected with a lifting hook conversion module, the top of the lifting hook conversion module is fixedly connected with a third connecting wire, the tail end of the third connecting wire is fixedly connected with a lifting hook processing module, the top of the lifting hook processing module is fixedly connected with a fourth connecting wire, and the tail end of the fourth connecting wire is fixedly connected with a lifting hook spiral suspension.
As a further description of the above technical solution:
the lifting hook spiral suspension top fixedly connected with a first lifting wire and a second lifting wire, the tail end of the first lifting wire is fixedly connected with a photovoltaic power generation platform, the tail end of the second lifting wire is fixedly connected with a lift-off platform, the two sides of the outer side wall of the lifting hook spiral suspension are respectively fixedly connected with a third lifting wire and a fourth lifting wire, the tail end of the third lifting wire is fixedly connected with a weapon interference platform, and the tail end of the fourth lifting wire is fixedly connected with a shooting platform.
As a further description of the above technical solution:
the lift-off subassembly includes the navigation track management planning with the terminal fixedly connected with of first branch, navigation track management planning top fixedly connected with second branch, second branch terminal fixedly connected with CPU control module, CPU control module lateral wall fixedly connected with third branch, the terminal fixedly connected with unmanned aerial vehicle instrument display module of third branch, CPU control module top fixedly connected with fourth branch, the terminal fixedly connected with autonomous navigation module of fourth branch.
As a further description of the above technical solution:
the photovoltaic module comprises a second mounting line fixedly connected with the side wall of the solar battery pack, a power distribution controller is fixedly connected to the tail end of the second mounting line, a third mounting line is fixedly connected to the side wall of the power distribution controller, a photoelectric receiver is fixedly connected to the tail end of the third mounting line, a fourth mounting line is fixedly connected to the side wall of the photoelectric receiver, and a solar storage battery is fixedly connected to the tail end of the fourth mounting line.
As a further description of the above technical solution:
the weapon interference assembly comprises a second fixed wire fixedly connected with the side wall of the simulation interference system, the tail end of the second fixed wire is fixedly connected with a signal receiving module, the side wall of the signal receiving module is fixedly connected with a third fixed wire, the tail end of the third fixed wire is fixedly connected with a signal conversion module, the side wall of the signal conversion module is fixedly connected with a fourth fixed wire, the tail end of the fourth fixed wire is fixedly connected with a signal CPU processing module, the top of the signal CPU processing module is fixedly connected with a first conveying line, the tail end of the first conveying line is fixedly connected with a radar positioning system, and the side wall of the radar positioning system is fixedly connected with a second conveying line.
As a further description of the above technical solution:
the device comprises a first conveying line, a second conveying line, a third conveying line, a photoelectric interference device, a fourth conveying line and an interference gun, wherein the wireless interference device is fixedly connected to the tail end of the second conveying line, the third conveying line is fixedly connected to the bottom of the wireless interference device, the photoelectric interference device is fixedly connected to the tail end of the third conveying line, and the fourth conveying line is fixedly connected to the fourth conveying line.
As a further description of the above technical solution:
the shooting assembly comprises a second transmission line fixedly connected with the side wall of the camera control module, the tail end of the second transmission line is fixedly connected with an image receiving module, the side wall of the image receiving module is fixedly connected with a fourth transmission line, and the tail end of the fourth transmission line is fixedly connected with an image analysis module.
As a further description of the above technical solution:
the image analysis module is characterized in that the side wall of the image analysis module is fixedly connected with a first analysis line, the tail end of the first analysis line is fixedly connected with a PC end, the side wall of the PC end is fixedly connected with a second analysis line, the tail end of the second analysis line is fixedly connected with a photo transmission module, the side wall of the photo transmission module is fixedly connected with a third analysis line, the tail end of the third analysis line is fixedly connected with an image analysis machine, the bottom of the image analysis machine is fixedly connected with a fourth analysis line, and the tail end of the fourth analysis line is fixedly connected with an image display.
The unmanned aerial vehicle electronic war simulation efficiency supporting method comprises the following steps:
s1, a communication base station is started firstly, signals are driven to enter a first mounting line through the communication base station, then the signals enter a solar battery pack from the first mounting line, then the solar battery pack is started to transmit energy into a second mounting line, then the energy is transmitted to a power distribution controller from the second mounting line, so that electricity is subjected to frequency conversion, regulated and controlled electricity is discharged into a third mounting line, then the introduced electricity enters a photoelectric receiver to receive the regulated and controlled electricity, the regulated and controlled electricity enters a fourth mounting line, and then the electricity enters the solar battery from the fourth mounting line to be stored in the solar battery, and the solar battery drives a supporting assembly, a weapon interference platform and a shooting platform to be electrified through external wires;
s2, starting a communication base station, driving signals to enter a first connecting wire through the communication base station, then entering a lifting hook receiving module from the first connecting wire, enabling the received signals to enter a second connecting wire, then transmitting the signals to be transmitted to a lifting hook converting module from the second connecting wire for converting information, then transmitting the converted signals to a third connecting wire, then transmitting the signals to a lifting hook processing module from the third connecting wire, processing the converted signals, then transmitting the processed signals to a fourth connecting wire, simultaneously entering a lifting hook spiral suspension from the fourth connecting wire, then carrying and assembling a photovoltaic power generation platform and a lifting platform respectively from a first lifting wire and a second lifting wire on the lifting hook spiral suspension, carrying and assembling a weapon interference platform and a shooting platform respectively from a third lifting wire and a fourth lifting wire on the lifting hook spiral suspension, and supporting and installing a plurality of platforms;
s3, driving signals to enter an assembly line by a communication base station, transmitting the signals to a flight control simulation system from the assembly line, transmitting the signals to a first branch line from the flight control simulation system, transmitting the signals to a navigation track management planning from the first branch line, planning and controlling the signals, transmitting the signals to a second branch line, transmitting the signals to a CPU control module from the second branch line, processing the signals by the CPU control module, transmitting the processed signals to a third branch line, transmitting the processed signals to an unmanned aerial vehicle instrument display module from the third branch line, displaying the processed signals, transmitting the processed signals to a fourth branch line, transmitting the processed signals to an autonomous navigation module from the fourth branch line, and driving an external unmanned aerial vehicle to automatically cruise;
s4, transmitting signals into a first fixed line again through a communication base station, then entering a simulation interference system from the first fixed line, transmitting interference information into a second fixed line, transmitting signals into a signal receiving module, receiving the signals, then transmitting the received signals into a third fixed line, transmitting the received signals into a signal conversion module, converting the signals, transmitting the converted signals into a fourth fixed line, transmitting the converted signals into a signal CPU processing module from the fourth fixed line, processing the processed signals into a first conveying line, transmitting positioning signals into a radar positioning system from the first conveying line, transmitting the signals received at a point location into a second conveying line, transmitting the signals into a wireless interference device from the second conveying line, transmitting the signals with interference into a third conveying line, transmitting the signals into a photoelectric interference device from the third conveying line, transmitting the signals with light sensation from the photoelectric interference device into an interference gun, and interfering external electronic equipment through the interference gun;
s5, enabling signals transmitted by the communication base station to enter a first transmission line, then enter a camera control module from the first transmission line, then enter a second transmission line from the camera control module, then enter an image receiving module from the second transmission line to receive the signals, then enter a fourth transmission line, then enter an image analyzing module from the fourth transmission line to analyze the signals, then enter the first analysis line, then enter a PC end from the first analysis line to process the received signals, then enter the second analysis line, then enter a photo transmission module from the photo transmission module, then enter a third analysis line, then enter an image analyzer from the third analysis line, further analyze the signals, then enter the fourth analysis line, and then enter an image display from the fourth analysis line to display.
(III) beneficial effects
The invention has the following beneficial effects:
1. compared with the prior art, this unmanned aerial vehicle electron war simulation efficiency braced system utilizes lifting hook receiving module, the second connecting wire, lifting hook conversion module, the third connecting wire, lifting hook processing module, the fourth connecting wire, lifting hook spiral suspension, first hoist line, the second hoist line, photovoltaic power generation platform, lift-off platform, the third hoist line, the fourth hoist line, weapon interference platform and shooting platform cooperation, be convenient for install respectively through first hoist line and second hoist line and carry on photovoltaic power generation platform lift-off platform, and third hoist line and fourth hoist line carry the assembly respectively to weapon interference platform and shooting platform, the convenience supports the installation to a plurality of platforms for install multiple platforms, and carry multiple functions, improve the result of use.
2. Compared with the prior art, the unmanned aerial vehicle electronic warfare simulation efficiency supporting system utilizes a simulation interference system, a second fixed line, a signal receiving module, a third fixed line, a signal conversion module, a fourth fixed line, a signal CPU processing module, a first conveying line, a radar positioning system, a second conveying line, a wireless interference device, a third conveying line, a photoelectric interference device, a fourth conveying line and an interference gun to cooperate, so that the radar positioning system can conveniently carry out point location on external signals, and the wireless interference device, the photoelectric interference device and the interference gun can be used for interfering external network signals.
3. Compared with the prior art, the unmanned aerial vehicle electronic warfare simulation efficiency supporting system utilizes a camera control module, a second transmission line, an image receiving module, an image analysis module, a fourth transmission line, a first analysis line, a PC end, a second analysis line, a photo transmission module, a third analysis line, an image analysis machine, a fourth analysis line and an image display to cooperate, so that external signals can be conveniently shot through the camera control module, and the signals are processed through the PC end, then transmitted through the photo transmission module, then analyzed through the image analysis machine, then displayed through the image display, and the signals can be conveniently received and displayed.
4. Compared with the prior art, the unmanned aerial vehicle electronic war simulation efficiency supporting system comprises a navigation track management planning, a second branch line, a CPU control module, a third branch line, an unmanned aerial vehicle instrument display module, a fourth branch line and an autonomous navigation module, wherein the unmanned aerial vehicle instrument display module, the fourth branch line and the autonomous navigation module are matched, a planning route is conveniently carried out through the navigation track management planning, then the CPU control module is used for processing the planned signals, the unmanned aerial vehicle instrument display module is respectively displayed, and meanwhile the planned signals are processed through the autonomous navigation module, so that the unmanned aerial vehicle automatically cruises.
5. Compared with the prior art, the unmanned aerial vehicle electronic war simulation efficiency supporting system utilizes the cooperation of the solar battery pack, the second mounting line, the power distribution controller, the photoelectric receiver, the third mounting line, the fourth mounting line and the solar battery, so that the solar battery can be used for carrying out light energy conversion on solar energy, and the unmanned aerial vehicle can conduct endurance in a wireless mode.
Drawings
Fig. 1 is a schematic diagram of the overall structure of an electronic warfare simulation efficiency support system for an unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of a supporting and carrying platform of the unmanned aerial vehicle electronic warfare simulation efficiency supporting system according to the present invention;
fig. 3 is a schematic diagram of an elevating platform structure of an unmanned aerial vehicle electronic warfare simulation efficiency supporting system according to the present invention;
fig. 4 is a schematic structural diagram of a photovoltaic power generation platform of the unmanned aerial vehicle electronic warfare simulation efficiency supporting system provided by the invention;
fig. 5 is a schematic diagram of a weapon interference platform structure of an unmanned aerial vehicle electronic warfare simulation efficiency support system according to the present invention;
fig. 6 is a schematic diagram of a wireless jammer and a jammer gun of the unmanned aerial vehicle electronic warfare simulation effectiveness supporting system according to the present invention;
fig. 7 is a schematic view of a shooting platform structure of an electronic warfare simulation efficiency supporting system for an unmanned aerial vehicle according to the present invention.
Legend description:
1. a communication base station; 2. supporting the carrying platform; 3. lifting off the platform; 4. a photovoltaic power generation platform; 5. a weapon interference platform; 6. a shooting platform; 7. a hook receiving module; 8. a hook conversion module; 9. a hook processing module; 10. the lifting hook is spirally hung; 11. a flight control simulation system; 12. planning navigation track management; 13. a CPU control module; 14. an unmanned aerial vehicle instrument display module; 15. an autonomous navigation module; 16. a solar cell stack; 17. a power distribution controller; 18. a photoelectric receiver; 19. a solar storage battery; 20. simulating an interference system; 21. a signal receiving module; 22. a signal conversion module; 23. a signal CPU processing module; 24. a radar positioning system; 25. a wireless jammer; 26. a photoelectric interference device; 27. a disturbance gun; 28. a camera control module; 29. an image receiving module; 30. an image analysis module; 31. a PC end; 32. a photo transmission module; 33. an image analyzer; 34. an image display.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Examples:
as shown in fig. 1-7, the embodiment of the invention provides an unmanned aerial vehicle electronic war simulation efficiency supporting system, which comprises a communication base station 1, wherein a supporting carrying platform 2 is arranged above the communication base station 1, a lift-off platform 3 is arranged above the supporting carrying platform 2, a weapon interference platform 5 and a shooting platform 6 are respectively arranged on the left side and the right side of the supporting carrying platform 2, a photovoltaic power generation platform 4 is arranged below the weapon interference platform 5, a first connecting wire is fixedly connected to the top of the communication base station 1, a lifting hook receiving module 7 is fixedly connected to the tail end of the first connecting wire, and a supporting component is connected to the top of the lifting hook receiving module 7. The lifting platform 3, the photovoltaic power generation platform 4, the weapon interference platform 5 and the shooting platform 6 are carried through the supporting component, as shown in fig. 2, the supporting component comprises a second connecting wire fixedly connected with the top of the lifting hook receiving module 7, the tail end of the second connecting wire is fixedly connected with the lifting hook conversion module 8, the top of the lifting hook conversion module 8 is fixedly connected with a third connecting wire, the tail end of the third connecting wire is fixedly connected with the lifting hook processing module 9, the top of the lifting hook processing module 9 is fixedly connected with a fourth connecting wire, the tail end of the fourth connecting wire is fixedly connected with the lifting hook spiral suspension 10, the top of the lifting hook spiral suspension 10 is fixedly connected with a first lifting wire and a second lifting wire, the tail end of the first lifting wire is fixedly connected with the photovoltaic power generation platform 4, the tail end of the second lifting wire is fixedly connected with the lifting platform 3, the two sides of the outer side wall of the lifting hook spiral suspension 10 are respectively fixedly connected with a third lifting wire and a fourth lifting wire, the tail end of the third lifting wire is fixedly connected with the weapon interference platform 5, the tail end of the fourth lifting wire is fixedly connected with the shooting platform 6, the lifting hook spiral suspension 10 is respectively connected with the lifting hook interference platform 4, the weapon interference platform 5 is carried by the lifting hook spiral suspension 10, the lifting hook interference platform 5 and the lifting platform 3 and the shooting platform 6 are carried by the lifting hook interference platform 4.
The communication base station 1 top fixedly connected with assembly line, lift-off platform 3 fixed surface is connected with flies to control the emulation system 11, assembly line end and flies to control the emulation system 11 fixed connection, fly to control the first branch of emulation system 11 top fixedly connected with, first branch end fixedly connected with assembly that lifts off, as shown in fig. 3, the assembly that lifts off includes navigation track management plan 12 with the terminal fixedly connected of first branch, navigation track management plan 12 top fixedly connected with second branch, the terminal fixedly connected with CPU control module 13 of second branch, CPU control module 13 lateral wall fixedly connected with third branch, the terminal fixedly connected with unmanned aerial vehicle instrument display module 14 of third branch, CPU control module 13 top fixedly connected with fourth branch, the terminal fixedly connected with autonomous navigation module 15 of fourth branch, play the effect to unmanned aerial vehicle through the assembly that lifts off and remove the navigation.
The first mounting line of communication base station 1 top fixedly connected with, the terminal fixedly connected with solar cell group 16 of first mounting line, solar cell group 16 back and photovoltaic power generation platform 4 fixed connection, solar cell group 16 top is connected with photovoltaic module, as shown in fig. 4, photovoltaic module includes the second mounting line with solar cell group 16 lateral wall fixed connection, the terminal fixedly connected with distribution controller 17 of second mounting line, distribution controller 17 lateral wall fixedly connected with third mounting line, the terminal fixedly connected with photoelectric receiver 18 of third mounting line, photoelectric receiver 18 lateral wall fixedly connected with fourth mounting line, the terminal fixedly connected with solar cell 19 of fourth mounting line plays the effect of carrying out the circular telegram to outside lift-off platform 3, interference platform 5 and shooting platform 6 through photovoltaic module.
The communication base station 1 lateral wall fixedly connected with first fixed line, the terminal fixedly connected with emulation interference system 20 of first fixed line, emulation interference system 20 back and weapon interference platform 5 fixed connection, emulation interference system 20 top is connected with weapon interference subassembly, as shown in fig. 5 and 6, weapon interference subassembly includes the second fixed line with emulation interference system 20 lateral wall fixedly connected with, the terminal fixedly connected with signal receiving module 21 of second fixed line, signal receiving module 21 lateral wall fixedly connected with third fixed line, the terminal fixedly connected with signal conversion module 22 of third fixed line, signal conversion module 22 lateral wall fixedly connected with fourth fixed line, the terminal fixedly connected with signal CPU processing module 23 of fourth fixed line, signal CPU processing module 23 top fixedly connected with first transfer chain, the terminal fixedly connected with radar positioning system 24 of first transfer chain, radar positioning system 24 lateral wall fixedly connected with second transfer chain, the terminal fixedly connected with wireless interference ware 25 of second transfer chain, wireless interference ware 25 bottom fixedly connected with third transfer chain, the terminal fixedly connected with photoelectric interference ware 26 of third transfer chain, the terminal fixedly connected with fourth transfer chain of interference transfer chain 26 bottom, the terminal fixedly connected with interference transfer chain is provided with interference rifle 27, the effect of interference subassembly through the weapon interference.
The communication base station 1 lateral wall fixedly connected with first transmission line, first transmission line end and camera control module 28, camera control module 28 back and shooting platform 6 fixed connection, camera control module 28 top is connected with shooting subassembly, as shown in fig. 7, shooting subassembly includes the second transmission line with camera control module 28 lateral wall fixed connection, second transmission line end fixedly connected with image receiving module 29, image receiving module 29 lateral wall fixedly connected with fourth transmission line, fourth transmission line end fixedly connected with image analysis module 30, image analysis module 30 lateral wall fixedly connected with first analysis line, first analysis line end fixedly connected with PC end 31, PC end 31 lateral wall fixedly connected with second analysis line, second analysis line end fixedly connected with photo transmission module 32, photo transmission module 32 lateral wall fixedly connected with third analysis line, third analysis line end fixedly connected with image analysis machine 33, image analysis machine 33 bottom fixedly connected with fourth analysis line, fourth analysis line end fixedly connected with image display 34 plays the effect of shooting through shooting subassembly.
The unmanned aerial vehicle electronic war simulation efficiency supporting method comprises the following steps:
s1, a communication base station 1 is started firstly, signals are driven to enter a first mounting line through the communication base station 1, then the signals enter a solar battery pack 16 from the first mounting line, then the solar battery pack 16 is started to transmit energy to a second mounting line, then the energy is transmitted to a power distribution controller 17 from the second mounting line, so that electricity is subjected to frequency conversion, regulated and controlled electricity is discharged to a third mounting line, then the input electricity enters a photoelectric receiver 18 to receive the regulated and controlled electricity, the regulated and controlled electricity enters a fourth mounting line, then the regulated and controlled electricity enters a solar battery 19 from the fourth mounting line to be stored in the solar battery 19, and the solar battery 19 drives a supporting component, a weapon interference platform 5 and a shooting platform 6 to be electrified through external wires;
s2, starting a communication base station 1, driving a signal to enter a first connecting wire through the communication base station 1, then entering a lifting hook receiving module 7 from the first connecting wire, enabling the received signal to enter a second connecting wire, then transmitting the received signal to a lifting hook converting module 8 from the second connecting wire to convert information, then transmitting the converted signal to a third connecting wire, then transmitting the converted signal to a lifting hook processing module 9 from the third connecting wire, enabling the converted signal to be processed, then transmitting the processed signal to a fourth connecting wire, simultaneously entering a lifting hook spiral suspension 10 from the fourth connecting wire, then respectively carrying and assembling a photovoltaic power generation platform 4 and a lifting platform 3 from a first lifting wire and a second lifting wire on the lifting hook spiral suspension 10, respectively carrying and assembling a weapon interference platform 5 and a shooting platform 6 from a third lifting wire and a fourth lifting wire on the lifting hook spiral suspension 10, and supporting and installing a plurality of platforms;
s3, the communication base station 1 drives signals to enter an assembly line, the signals are transmitted to the flight control simulation system 11 from the assembly line, the signals are transmitted to the first branch line from the flight control simulation system 11, the signals are transmitted to the navigation track management planning 12 from the first branch line, the planning control is carried out on the signals, the signals of the planning control are transmitted to the second branch line, the signals are transmitted to the CPU control module 13 from the second branch line, the signals are processed through the CPU control module 13, the processed signals enter the third branch line, the processed signals enter the unmanned aerial vehicle instrument display module 14 from the third branch line and are displayed, the signals enter the fourth branch line, and the signals enter the autonomous navigation module 15 from the fourth branch line, so that the unmanned aerial vehicle outside the unmanned aerial vehicle is driven to automatically cruise;
s4, then, the signal is transmitted to a first fixed line again through the communication base station 1, then the signal enters the simulation interference system 20 from the first fixed line, so that the interference information is transmitted to a second fixed line, then the transmitted signal enters the signal receiving module 21, so that the signal is received, then the received signal enters a third fixed line, then the received signal is transmitted to the signal conversion module 22, so that the signal is converted, then the converted signal enters a fourth fixed line, then the signal enters the signal CPU processing module 23 from the fourth fixed line to process the converted signal, then the processed signal is transmitted to a first conveying line, then the positioning signal is received from the first conveying line to the radar positioning system 24, then the signal received at the point location enters a second conveying line, then the wireless interference device 25 from the second conveying line, the interference signal is driven to enter the third conveying line to the photoelectric interference device 26 from the third conveying line, then the photoelectric interference device 26 enters the light sensing transmission, and then the light sensing transmission signal enters the interference gun 27, so that the external electronic equipment is interfered through the interference gun 27;
s5, the signal transmitted by the communication base station 1 enters the first transmission line, then enters the camera control module 28 from the first transmission line, then enters the second transmission line from the camera control module 28, then enters the image receiving module 29 from the second transmission line to receive the signal, then enters the fourth transmission line, then enters the image analyzing module 30 from the fourth transmission line to analyze the signal, then enters the first analysis line, then enters the PC terminal 31 from the first analysis line to process the received signal, then enters the second analysis line, then enters the photo transmission module 32 from the second analysis line, then enters the third analysis line from the photo transmission module 32, then enters the image analyzer 33 from the third analysis line to further analyze the signal, then enters the fourth analysis line, and then enters the image display 34 from the fourth analysis line to display.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an unmanned aerial vehicle electron war simulation efficiency braced system, includes communication base station, its characterized in that: a supporting carrying platform is arranged above the communication base station, a lift-off platform is arranged above the supporting carrying platform, a weapon interference platform and a shooting platform are respectively arranged on the left side and the right side of the supporting carrying platform, a photovoltaic power generation platform is arranged below the weapon interference platform, a first connecting wire is fixedly connected to the top of the communication base station, a lifting hook receiving module is fixedly connected to the tail end of the first connecting wire, and a supporting component is connected to the top of the lifting hook receiving module;
the top of the communication base station is fixedly connected with an assembly line, the surface of the lift-off platform is fixedly connected with a flight control simulation system, the tail end of the assembly line is fixedly connected with the flight control simulation system, the top of the flight control simulation system is fixedly connected with a first branch line, and the tail end of the first branch line is fixedly connected with a lift-off assembly;
the top of the communication base station is fixedly connected with a first installation line, the tail end of the first installation line is fixedly connected with a solar battery pack, the back of the solar battery pack is fixedly connected with a photovoltaic power generation platform, and the top of the solar battery pack is connected with a photovoltaic module;
the side wall of the communication base station is fixedly connected with a first fixed line, the tail end of the first fixed line is fixedly connected with a simulation interference system, the back of the simulation interference system is fixedly connected with a weapon interference platform, and the top of the simulation interference system is connected with a weapon interference assembly;
the side wall of the communication base station is fixedly connected with a first transmission line, the tail end of the first transmission line is fixedly connected with a camera control module, the back of the camera control module is fixedly connected with a shooting platform, and the top of the camera control module is connected with a shooting assembly;
the supporting component comprises a second connecting wire fixedly connected with the top of the lifting hook receiving module, the tail end of the second connecting wire is fixedly connected with a lifting hook conversion module, the top of the lifting hook conversion module is fixedly connected with a third connecting wire, the tail end of the third connecting wire is fixedly connected with a lifting hook processing module, the top of the lifting hook processing module is fixedly connected with a fourth connecting wire, and the tail end of the fourth connecting wire is fixedly connected with a lifting hook spiral suspension;
the top of the lifting hook spiral suspension is fixedly connected with a first lifting line and a second lifting line, the tail end of the first lifting line is fixedly connected with a photovoltaic power generation platform, the tail end of the second lifting line is fixedly connected with a lift-off platform, the two sides of the outer side wall of the lifting hook spiral suspension are respectively fixedly connected with a third lifting line and a fourth lifting line, the tail end of the third lifting line is fixedly connected with a weapon interference platform, and the tail end of the fourth lifting line is fixedly connected with a shooting platform;
the lift-off assembly comprises a navigation track management plan fixedly connected with the tail end of the first branch line, the top of the navigation track management plan is fixedly connected with a second branch line, the tail end of the second branch line is fixedly connected with a CPU control module, the side wall of the CPU control module is fixedly connected with a third branch line, the tail end of the third branch line is fixedly connected with an unmanned plane instrument display module, the top of the CPU control module is fixedly connected with a fourth branch line, and the tail end of the fourth branch line is fixedly connected with an autonomous navigation module;
the photovoltaic module comprises a second mounting line fixedly connected with the side wall of the solar battery pack, the tail end of the second mounting line is fixedly connected with a power distribution controller, the side wall of the power distribution controller is fixedly connected with a third mounting line, the tail end of the third mounting line is fixedly connected with a photoelectric receiver, the side wall of the photoelectric receiver is fixedly connected with a fourth mounting line, and the tail end of the fourth mounting line is fixedly connected with a solar storage battery;
the weapon interference assembly comprises a second fixed wire fixedly connected with the side wall of the simulation interference system, the tail end of the second fixed wire is fixedly connected with a signal receiving module, the side wall of the signal receiving module is fixedly connected with a third fixed wire, the tail end of the third fixed wire is fixedly connected with a signal conversion module, the side wall of the signal conversion module is fixedly connected with a fourth fixed wire, the tail end of the fourth fixed wire is fixedly connected with a signal CPU processing module, the top of the signal CPU processing module is fixedly connected with a first conveying line, the tail end of the first conveying line is fixedly connected with a radar positioning system, and the side wall of the radar positioning system is fixedly connected with a second conveying line.
2. The unmanned aerial vehicle electronic warfare simulation effectiveness support system of claim 1, wherein: the end fixedly connected with wireless interference ware of second transfer chain, wireless interference ware bottom fixedly connected with third transfer chain, the end fixedly connected with photoelectricity interference ware of third transfer chain, photoelectricity interference ware bottom fixedly connected with fourth transfer chain, the end fixedly connected with of fourth transfer chain interferes with the rifle.
3. The unmanned aerial vehicle electronic warfare simulation effectiveness support system of claim 2, wherein: the shooting assembly comprises a second transmission line fixedly connected with the side wall of the camera control module, the tail end of the second transmission line is fixedly connected with an image receiving module, the side wall of the image receiving module is fixedly connected with a fourth transmission line, and the tail end of the fourth transmission line is fixedly connected with an image analysis module.
4. The unmanned aerial vehicle electronic warfare simulation effectiveness support system of claim 3, wherein: the side wall of the image analysis module is fixedly connected with a first analysis line, the tail end of the first analysis line is fixedly connected with a PC end, the side wall of the PC end is fixedly connected with a second analysis line, the tail end of the second analysis line is fixedly connected with a photo transmission module, the side wall of the photo transmission module is fixedly connected with a third analysis line, the tail end of the third analysis line is fixedly connected with an image analysis machine, the bottom of the image analysis machine is fixedly connected with a fourth analysis line, and the tail end of the fourth analysis line is fixedly connected with an image display.
5. A method for supporting simulation efficiency of electronic warfare using the system as claimed in any one of claims 1 to 4, characterized in that: the method comprises the following steps:
s1, a communication base station is started firstly, signals are driven to enter a first mounting line through the communication base station, then the signals enter a solar battery pack from the first mounting line, then the solar battery pack is started to transmit energy into a second mounting line, then the energy is transmitted to a power distribution controller from the second mounting line, so that electricity is subjected to frequency conversion, regulated and controlled electricity is discharged into a third mounting line, then the introduced electricity enters a photoelectric receiver to receive the regulated and controlled electricity, the regulated and controlled electricity enters a fourth mounting line, and then the electricity enters the solar battery from the fourth mounting line to be stored in the solar battery, and the solar battery drives a supporting assembly, a weapon interference platform and a shooting platform to be electrified through external wires;
s2, starting a communication base station, driving signals to enter a first connecting wire through the communication base station, then entering a lifting hook receiving module from the first connecting wire, enabling the received signals to enter a second connecting wire, then transmitting the signals to be transmitted to a lifting hook converting module from the second connecting wire for converting information, then transmitting the converted signals to a third connecting wire, then transmitting the signals to a lifting hook processing module from the third connecting wire, processing the converted signals, then transmitting the processed signals to a fourth connecting wire, simultaneously entering a lifting hook spiral suspension from the fourth connecting wire, then carrying and assembling a photovoltaic power generation platform and a lifting platform respectively from a first lifting wire and a second lifting wire on the lifting hook spiral suspension, carrying and assembling a weapon interference platform and a shooting platform respectively from a third lifting wire and a fourth lifting wire on the lifting hook spiral suspension, and supporting and installing a plurality of platforms;
s3, driving signals to enter an assembly line by a communication base station, transmitting the signals to a flight control simulation system from the assembly line, transmitting the signals to a first branch line from the flight control simulation system, transmitting the signals to a navigation track management planning from the first branch line, planning and controlling the signals, transmitting the signals to a second branch line, transmitting the signals to a CPU control module from the second branch line, processing the signals by the CPU control module, transmitting the processed signals to a third branch line, transmitting the processed signals to an unmanned aerial vehicle instrument display module from the third branch line, displaying the processed signals, transmitting the processed signals to a fourth branch line, transmitting the processed signals to an autonomous navigation module from the fourth branch line, and driving an external unmanned aerial vehicle to automatically cruise;
s4, transmitting signals into a first fixed line again through a communication base station, then entering a simulation interference system from the first fixed line, transmitting interference information into a second fixed line, transmitting signals into a signal receiving module, receiving the signals, then transmitting the received signals into a third fixed line, transmitting the received signals into a signal conversion module, converting the signals, transmitting the converted signals into a fourth fixed line, transmitting the converted signals into a signal CPU processing module from the fourth fixed line, processing the processed signals into a first conveying line, transmitting positioning signals into a radar positioning system from the first conveying line, transmitting the signals received at a point location into a second conveying line, transmitting the signals into a wireless interference device from the second conveying line, transmitting the signals with interference into a third conveying line, transmitting the signals into a photoelectric interference device from the third conveying line, transmitting the signals with light sensation from the photoelectric interference device into an interference gun, and interfering external electronic equipment through the interference gun;
s5, enabling signals transmitted by the communication base station to enter a first transmission line, then enter a camera control module from the first transmission line, then enter a second transmission line from the camera control module, then enter an image receiving module from the second transmission line to receive the signals, then enter a fourth transmission line, then enter an image analyzing module from the fourth transmission line to analyze the signals, then enter the first analysis line, then enter a PC end from the first analysis line to process the received signals, then enter the second analysis line, then enter a photo transmission module from the photo transmission module, then enter a third analysis line, then enter an image analyzer from the third analysis line, further analyze the signals, then enter the fourth analysis line, and then enter an image display from the fourth analysis line to display.
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