CN211505886U - Unmanned aerial vehicle's radar detection system - Google Patents
Unmanned aerial vehicle's radar detection system Download PDFInfo
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- CN211505886U CN211505886U CN201921783068.6U CN201921783068U CN211505886U CN 211505886 U CN211505886 U CN 211505886U CN 201921783068 U CN201921783068 U CN 201921783068U CN 211505886 U CN211505886 U CN 211505886U
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Abstract
The utility model discloses a radar detection system of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle reverse gun, wherein a control panel is embedded and installed at one end of the unmanned aerial vehicle reverse gun, the bottom end of the unmanned aerial vehicle reverse gun is connected with the handle, one end of the unmanned aerial vehicle reverse gun is connected with the interference unit, the utility model has scientific and reasonable structure and safe and convenient use, and through the arranged first placing clamp plate, the second placing clamp plate, the clamping bandage and the fixed block, the clamping bandage can be penetrated through the armpit of a user, the unmanned aerial vehicle reverse lance is placed on the shoulder for stable placement, the fixation of the unmanned aerial vehicle reverse lance during use is convenient, and through the arranged clamping block, the clamping spring and the penetrating rod, the inserted storage battery can be fixedly clamped, and the two pulling plates can be pulled when the storage battery needs to be disassembled, dismantle the battery, can avoid the condition that the battery is not hard up and drops because of rocking the production when unmanned aerial vehicle reverse system rifle uses.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle surveys technical field, specifically is an unmanned aerial vehicle's radar detection system.
Background
Unmanned aerial vehicle is called unmanned aerial vehicle for short, it is the unmanned aerial vehicle who utilizes radio remote control equipment and self-contained program control device to control, or by the on-vehicle computer independently operate completely or intermittently, unmanned aerial vehicle is because its control is stable, advantages such as aerial shot map, widely receive people's liking, but unmanned aerial vehicle is in the use, at the airport, place such as military control area all are forbidden to fly, the user then ignores this point easily when using unmanned aerial vehicle, consequently need design an unmanned aerial vehicle's radar detection system, detect the unmanned aerial vehicle that gets into the guard area within range, and implement the interference counter-measure to unmanned aerial vehicle according to the detection result.
SUMMERY OF THE UTILITY MODEL
The utility model provides a technical scheme can effectively solve the problem of proposing among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a radar detection system of an unmanned aerial vehicle comprises an unmanned aerial vehicle reverse gun, wherein a control panel is embedded into one end of the unmanned aerial vehicle reverse gun, a handle is connected to the bottom end of the unmanned aerial vehicle reverse gun, an interference unit is connected to one end of the unmanned aerial vehicle reverse gun, a control handle is installed at a position, corresponding to one side of the handle, of the bottom end of the unmanned aerial vehicle reverse gun, and a storage battery is installed at a position, corresponding to the middle of the handle and the control handle, of the bottom end of the unmanned aerial vehicle reverse gun;
the other end of the unmanned aerial vehicle reverse braking gun is connected with a fixed mounting mechanism, and the fixed mounting mechanism comprises a placing groove, a connecting rod, a limiting plate, a reset spring, a rotating connecting seat, a fixed connecting seat, a first placing clamp plate, a penetrating connecting rod, a limiting connecting plate, a second placing clamp plate, a placing spring, a clamping binding band and a fixed seat;
the unmanned aerial vehicle reverse-production gun is characterized in that a placing groove is symmetrically formed in the other end of the unmanned aerial vehicle reverse-production gun, a connecting rod is slidably mounted on the inner wall of the placing groove, a limiting plate is connected to one end of the connecting rod corresponding to the position inside the placing groove, a reset spring is connected to the position on one side of the limiting plate on the outer side of the connecting rod, a rotating connecting seat is connected to the other end of the connecting rod, a fixed connecting seat is rotatably mounted on the outer side of the rotating connecting seat, a first placing clamp plate is fixedly mounted at one end of the fixed connecting seat, a penetrating connecting rod is symmetrically connected to one end of the first placing clamp plate, a limiting connecting plate is connected to one end of the penetrating connecting rod, a second placing clamp plate is slidably mounted on the position on one side of the limiting connecting plate on the outer side of the penetrating connecting rod corresponding, the position of one end of the first placing clamp plate, which corresponds to the clamping bandage, is connected with a fixed seat.
Preferably, the storage battery fixing mechanism is arranged at the position, corresponding to the two sides of the storage battery, of the bottom end of the unmanned aerial vehicle reverse braking gun and comprises a fixing block, a fixing groove, a penetrating rod, a clamping block, a clamping spring, a clamping block and a pulling plate;
the bottom of the anti-system rifle of unmanned aerial vehicle corresponds battery both sides position department and installs the fixed block, the fixed slot has been seted up to the one end of fixed block, the one end of fixed block evenly runs through and is connected with and runs through the pole, the one end that runs through the pole is connected with the fixture block, the outside that runs through the pole corresponds fixture block one side position department and installs the joint spring, the both ends of battery correspond fixture block position department fixed mounting and have the joint piece, the other end that runs through the pole passes the fixed block and is connected with the arm-tie.
Preferably, a placing mechanism is embedded into one end of the unmanned aerial vehicle reverse gun and comprises a placing groove, an L-shaped placing plate, a mounting groove, a fixing rod, a sliding clamping plate, a clamping spring, a sun shield, a fixing belt and a magic tape;
the one end of the reverse system rifle of unmanned aerial vehicle has been seted up and has been placed the recess, the inner wall sliding connection who places the recess has the L type to place the board, the L type is placed the top of board and has been seted up the mounting groove, the one end inner wall symmetric connection of mounting groove has the dead lever, the outside slidable mounting of dead lever has the slip splint, the outside of dead lever corresponds slip splint one side position department and is connected with the centre gripping spring, the L type is placed the one end of board and is rotated and be connected with the sunshading board, the fixed band is installed in the top embedding of sunshading board, the L type is placed the other end of board.
According to above-mentioned technical characteristic, including probe end, processing end, control transmission end and control display terminal, the probe end includes radio monitoring, radar monitoring and the infrared monitoring of visible light, the processing end includes server, spectrum characteristic discernment and analysis processor, the control transmission end includes remote controller, signal transmitter and signal receiver, control display terminal is including showing submodule piece, control terminal, the local storage of monitoring information and unmanned aerial vehicle reverse system rifle, the output of probe end is connected with the input of processing end, the output of processing end is connected with control display terminal's input, the output of control transmission end is connected with the input of probe end.
According to the technical characteristics, the detection end includes radio monitoring, radar monitoring and visible light infrared monitoring, the radio monitoring specifically indicates through signal detection technique, to the remote control signal that unmanned aerial vehicle flight in-process needs received, extracts relevant signal characteristic from it to the signal characteristic that will extract transmits, the radar monitoring specifically indicates to use the radar to scan the unmanned aerial vehicle forbidden area and detect, monitors the unmanned aerial vehicle that obviously deviates flight plan and break into. The visible light infrared monitoring is to adopt an infrared radiation detection technology to collect infrared radiation information emitted in a no-fly area of the unmanned aerial vehicle and extract infrared waveband information for transmission.
According to the technical characteristics, the display sub-module comprises unmanned aerial vehicle model display, longitude and latitude height display, monitoring report display, carrier frequency display and monitoring video playing, the unmanned aerial vehicle model display refers to the identification of the model of the unmanned aerial vehicle by extracting key characteristic items in frequency spectrum data acquired in real time and comparing and identifying the key characteristic items with a pre-constructed transmitter frequency spectrum characteristic library of a common unmanned aerial vehicle, the longitude and latitude height display refers to the identification and display of the longitude and latitude and the height of the unmanned aerial vehicle through the analysis and processing results of radar monitoring, radio monitoring and visible infrared light monitoring, the monitoring report display refers to the automatic generation of an activity summary report for receiving the unmanned aerial vehicle monitoring condition, the unmanned aerial vehicle control result and the unmanned aerial vehicle detailed condition, and transmitting the activity summary report to the display equipment for display, the carrier frequency display refers to the real-time display of the carrier frequency of the unmanned, the monitoring video playing refers to combining the monitoring results of radar monitoring, radio monitoring and visible-infrared monitoring with a monitoring area map and displaying in real time.
A radar detection method of an unmanned aerial vehicle comprises the following steps:
s1, no-fly monitoring: erecting required monitoring equipment, and monitoring a distribution control area in real time;
s2, information processing: analyzing and processing the information acquired by real-time monitoring to obtain the information of the unmanned aerial vehicle;
s3, displaying the result: classifying the analyzed and processed information, and then uniformly displaying the analyzed and processed information;
s4, unmanned aerial vehicle control: remotely transmitting the monitoring result, and performing linkage control on a corresponding unmanned aerial vehicle control gun to perform interference control on the unmanned aerial vehicle target;
s5, report generation: and after the monitoring is finished, an activity summary report is automatically generated, and the unmanned aerial vehicle control result is summarized.
According to the technical characteristics, in the step S1, radio monitoring, radar monitoring and visible infrared monitoring are set up according to the area size of the controlled area, so as to realize real-time monitoring of the controlled area.
According to the technical characteristics, in the step S2, the information of the unmanned aerial vehicle collected by real-time monitoring is analyzed, and the frequency spectrum characteristic information, the longitude and latitude height information, the carrier frequency information and the remote control position information of the unmanned aerial vehicle are obtained by analysis.
According to the technical characteristics, in the step S3, the frequency spectrum characteristic information, the longitude and latitude height information, the carrier frequency information and the remote control position information of the unmanned aerial vehicle which are analyzed and processed are classified, and then the analyzed and processed information is arranged and displayed on the display device.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model has the advantages of being scientific and reasonable in structure, convenience safe in utilization:
1. through the first splint, the second of placing that set up place splint, centre gripping bandage and fixed block, can pull the first splint of placing to place splint and the first splint separation of placing with the second, pass the centre gripping bandage from the user armpit, fix through the fixing base, the user can place unmanned aerial vehicle reverse system rifle and stabilize on the shoulder and place, the unmanned aerial vehicle of being convenient for reverse the fixed when rifle uses.
2. Through the joint piece that sets up, the fixture block, the joint spring with run through the pole, can drive the fixture block and run through the pole and remove when joint piece and fixture block contact, carry out the joint to the joint piece, be convenient for carry out fixed joint to the battery of filling in to can be when needs are dismantled the battery, two arm-tie of pulling drive joint piece and fixture block separation, dismantle the battery, can avoid the condition that the battery that unmanned aerial vehicle reverse system rifle produced when using is not hard up and drops because of rocking.
3. Place the board, place recess, slip splint and clamping spring through the L type that sets up, can place the L type and pull out in the board is followed and is placed the recess, carry out the centre gripping through slip splint and clamping spring to display device and place to the sunshading board can overturn, carries out the sunshade protection to display device, and when the user of being convenient for held unmanned aerial vehicle reverse system rifle, carries out the centre gripping to all the other display devices that need use and places.
4. When the radar detection system of the unmanned aerial vehicle is used, the radio monitoring, the radar monitoring and the visible light infrared monitoring contained in the detection end can carry out multi-aspect monitoring on the no-fly area, the monitoring result is transmitted to the processing end in real time through the signal transmitter and the signal receiver, the information transmitted by the radio monitoring, the radar monitoring and the visible light infrared monitoring can be analyzed and processed through the server and the spectrum characteristic recognition and analysis processor contained in the processing end, the information is compared and recognized with a pre-constructed transmitter spectrum characteristic library of a common unmanned aerial vehicle, the model of the unmanned aerial vehicle is recognized, the longitude and latitude information, the carrier frequency information and the height information of the unmanned aerial vehicle are obtained through analysis, then the model, the carrier frequency information, the longitude and latitude information and the height information of the unmanned aerial vehicle are transmitted to the display terminal through the display sub-module, and are displayed to a user in real time, and the monitoring information is stored locally in real time, if the unmanned aerial vehicle breaks into the no-fly area, the user can transmit the monitoring result to the corresponding unmanned aerial vehicle anti-gun position, and the unmanned aerial vehicle breaking into the no-fly area is subjected to interference anti-gun through the unmanned aerial vehicle anti-gun.
5. When this unmanned aerial vehicle's radar detection method uses, at first according to the regional size in the control area, erect radio monitoring, radar monitoring and visible infrared monitoring, realize carrying out real-time supervision to the control area, the unmanned aerial vehicle information that real-time supervision gathered can carry out analysis processes, the analysis reachs unmanned aerial vehicle's spectral feature information, unmanned aerial vehicle longitude and latitude height information, unmanned aerial vehicle carrier frequency information and unmanned aerial vehicle remote control position information, and classify, show on display device after with analysis processes ' information arrangement afterwards, the user can be according to the monitoring and the result that show, the remote transmission monitoring result, the corresponding unmanned aerial vehicle of coordinated control counteracts rifle, disturb the reaction to the unmanned aerial vehicle target, after last monitoring ends, the activity summary report is generated automatically, summarize the unmanned aerial vehicle control result.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention.
In the drawings:
fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a schematic view of the installation structure of the handle and the storage battery of the present invention;
FIG. 3 is a schematic structural view of the fixing and mounting mechanism of the present invention;
FIG. 4 is a schematic view of the installation structure of the rotary connecting seat and the fixed connecting seat of the present invention;
FIG. 5 is a schematic structural view of the battery fixing mechanism of the present invention;
FIG. 6 is a schematic view of the area A in FIG. 5 according to the present invention;
fig. 7 is a schematic structural view of the placing mechanism of the present invention;
fig. 8 is a schematic diagram of the system structure of the present invention;
fig. 9 is a schematic structural diagram of the display sub-module of the present invention;
fig. 10 is a schematic view of the flow structure of the present invention;
reference numbers in the figures: 1. the unmanned aerial vehicle controls the gun in a reverse mode; 2. a control panel; 3. a grip; 4. an interferer; 5. a control handle; 6. a storage battery;
7. a fixed mounting mechanism; 701. a placement groove; 702. a connecting rod; 703. a limiting plate; 704. a return spring; 705. rotating the connecting seat; 706. fixing the connecting seat; 707. a first placing splint; 708. The connecting rod penetrates through the connecting rod; 709. a limiting connecting plate; 710. a second placing splint; 711. placing a spring; 712. clamping the binding band; 713. a fixed seat;
8. a battery fixing mechanism; 801. a fixed block; 802. fixing grooves; 803. penetrating the rod; 804. A clamping block; 805. clamping a spring; 806. a clamping block; 807. pulling a plate;
9. a placement mechanism; 901. placing a groove; 902. an L-shaped placing plate; 903. mounting grooves; 904. Fixing the rod; 905. a sliding clamp plate; 906. a clamping spring; 907. a sun visor; 908. fixing belts; 909. magic tape.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
Example (b): as shown in fig. 1-10, the utility model provides a technical scheme, an unmanned aerial vehicle's radar detection system, including unmanned aerial vehicle reverse gun 1, the one end embedding of unmanned aerial vehicle reverse gun 1 is installed with control panel 2, the bottom of unmanned aerial vehicle reverse gun 1 is connected with handle 3, the one end of unmanned aerial vehicle reverse gun 1 is connected with interference unit 4, the bottom of unmanned aerial vehicle reverse gun 1 is corresponding to handle 3 one side position and is installed and control handle 5, the bottom of unmanned aerial vehicle reverse gun 1 is corresponding to handle 3 and is installed battery 6 with control handle 5 intermediate position;
the other end of the unmanned aerial vehicle reverse braking gun 1 is connected with a fixing and mounting mechanism 7, and the fixing and mounting mechanism 7 comprises a placing groove 701, a connecting rod 702, a limiting plate 703, a return spring 704, a rotating connecting seat 705, a fixing connecting seat 706, a first placing clamping plate 707, a penetrating connecting rod 708, a limiting connecting plate 709, a second placing clamping plate 710, a placing spring 711, a clamping binding belt 712 and a fixing seat 713;
the other end of the unmanned aerial vehicle reverse braking gun 1 is symmetrically provided with a placing groove 701, the inner wall of the placing groove 701 is slidably provided with a connecting rod 702, one end of the connecting rod 702 is connected with a limiting plate 703 corresponding to the inner position of the placing groove 701, the outer side of the connecting rod 702 is connected with a return spring 704 corresponding to one side of the limiting plate 703, the other end of the connecting rod 702 is connected with a rotating connecting seat 705, the outer side of the rotating connecting seat 705 is rotatably provided with a fixed connecting seat 706, one end of the fixed connecting seat 706 is fixedly provided with a first placing clamping plate 707, one end of the first placing clamping plate 707 is symmetrically connected with a penetrating connecting rod 708, one end of the penetrating connecting rod 708 is connected with a limiting connecting plate 709, the outer side of the penetrating connecting rod 708 is slidably provided with a second placing clamping plate 710 corresponding to one side of the second placing clamping plate 710, the bottom end of the second placing, a fixing seat 713 is connected to one end of the first placing clamp plate 707 at a position corresponding to the clamping strap 712.
The storage battery fixing mechanism 8 is arranged at the position, corresponding to the two sides of the storage battery 6, of the bottom end of the unmanned aerial vehicle reverse-braking gun 1, and the storage battery fixing mechanism 8 comprises a fixing block 801, a fixing groove 802, a penetrating rod 803, a clamping block 804, a clamping spring 805, a clamping block 806 and a pulling plate 807;
the bottom of unmanned aerial vehicle reverse system rifle 1 corresponds battery 6 both sides position department and installs fixed block 801, fixed slot 802 has been seted up to the one end of fixed block 801, the even through connection of one end of fixed block 801 has run through pole 803, the one end that runs through pole 803 is connected with fixture block 804, the outside that runs through pole 803 corresponds fixture block 804 one side position department and installs joint spring 805, the both ends of battery 6 correspond fixture block 804 position department fixed mounting has joint piece 806, the other end that runs through pole 803 passes fixed block 801 and is connected with arm-tie 807.
One end of the unmanned aerial vehicle reverse-braking gun 1 is embedded with a placing mechanism 9, and the placing mechanism 9 comprises a placing groove 901, an L-shaped placing plate 902, a mounting groove 903, a fixing rod 904, a sliding clamp plate 905, a clamping spring 906, a sun shield 907, a fixing band 908 and a magic tape 909;
unmanned aerial vehicle reverse system rifle 1's one end has been seted up and has been placed recess 901, the inner wall sliding connection who places recess 901 has the L type to place board 902, the L type is placed the top of board 902 and has been seted up mounting groove 903, the one end inner wall symmetric connection of mounting groove 903 has dead lever 904, the outside sliding mounting of dead lever 904 has sliding clamp 905, the outside of dead lever 904 corresponds sliding clamp 905 one side position department and is connected with clamping spring 906, the L type is placed the one end of board 902 and is rotated and be connected with sunshading board 907, fixed band 908 is installed in the top embedding of sunshading board 907, the L type is placed the other end that board 902 and is corresponded fixed band.
According to above-mentioned technical characteristic, including the probe end, the processing end, control transmission end and control display terminal, the probe end includes radio monitoring, radar monitoring and visible light infrared monitoring, the processing end includes the server, spectrum feature recognition and analysis processor, the control transmission end includes the remote controller, signal transmitter and signal receiver, control display terminal is including showing submodule piece, control terminal, the local storage of monitoring information and unmanned aerial vehicle reverse system rifle, the output of probe end is connected with the input of processing end, the output of processing end is connected with control display terminal's input, the output of control transmission end is connected with the input of probe end.
According to the technical characteristics, the detection end includes radio monitoring, radar monitoring and visible light infrared monitoring, radio monitoring specifically indicates the passing signal detection technique, to the remote control signal that unmanned aerial vehicle flight in-process needs to receive, relevant signal characteristic is extracted from it, and transmit the signal characteristic who extracts, radar monitoring specifically indicates to use the radar to scan the no-fly area of unmanned aerial vehicle and detect, unmanned aerial vehicle to obvious skew flight plan and break into is monitored, visible light infrared monitoring indicates to adopt infrared radiation detection technique, the infrared radiation information that gives off in the no-fly area of unmanned aerial vehicle gathers, and extract infrared wave band information and transmit.
According to the technical characteristics, the display sub-module comprises unmanned aerial vehicle model display, longitude and latitude height display, monitoring report display, carrier frequency display and monitoring video playing, the unmanned aerial vehicle model display refers to the identification of the model of the unmanned aerial vehicle by extracting key characteristic items in frequency spectrum data acquired in real time and comparing and identifying the key characteristic items with a pre-constructed frequency spectrum characteristic library of a transmitter of a common unmanned aerial vehicle, the longitude and latitude height display refers to the identification and display of longitude and latitude and height of the unmanned aerial vehicle through the analysis and processing results of radar monitoring, radio monitoring and visible infrared monitoring, the monitoring report display refers to the automatic generation of an activity summary report for receiving the unmanned aerial vehicle monitoring condition, the unmanned aerial vehicle control result and the unmanned aerial vehicle detailed condition and transmitting the activity summary report to the display device for display, the carrier frequency display refers to the real-time display of the carrier frequency, the monitoring video playing refers to combining the monitoring results of radar monitoring, radio monitoring and visible-infrared monitoring with a monitoring area map and displaying in real time.
A radar detection method of an unmanned aerial vehicle comprises the following steps:
s1, no-fly monitoring: erecting required monitoring equipment, and monitoring a distribution control area in real time;
s2, information processing: analyzing and processing the information acquired by real-time monitoring to obtain the information of the unmanned aerial vehicle;
s3, displaying the result: classifying the analyzed and processed information, and then uniformly displaying the analyzed and processed information;
s4, unmanned aerial vehicle control: remotely transmitting the monitoring result, and performing linkage control on a corresponding unmanned aerial vehicle control gun to perform interference control on the unmanned aerial vehicle target;
s5, report generation: and after the monitoring is finished, an activity summary report is automatically generated, and the unmanned aerial vehicle control result is summarized.
According to the technical characteristics, in step S1, radio monitoring, radar monitoring and visible infrared monitoring are set up according to the area size of the controlled area, so as to realize real-time monitoring of the controlled area.
According to the technical characteristics, in step S2, the information of the unmanned aerial vehicle collected by real-time monitoring is analyzed, and the frequency spectrum characteristic information, the longitude and latitude height information, the carrier frequency information and the remote control position information of the unmanned aerial vehicle are obtained by analysis.
According to the technical characteristics, in step S3, the frequency spectrum characteristic information, the longitude and latitude height information, the carrier frequency information and the remote control position information of the unmanned aerial vehicle which are analyzed and processed are classified, and then the analyzed and processed information is arranged and displayed on the display device.
The utility model discloses a theory of operation and use flow: when the radar detection device of the unmanned aerial vehicle is used, a user can pull the first placing clamp plate 707 to drive the connecting rod 702 to move along the placing groove 701, the second placing clamp plate 710 and the first placing clamp plate 707 are separated, then the second placing clamp plate 710 and the first placing clamp plate 707 are placed on two sides of the shoulder of the user, the clamping straps 712 penetrate through the armpit of the user, the fixing base 713 is used for fixing, and the user can stably place the reverse braking gun 1 of the unmanned aerial vehicle;
when the storage battery 6 is plugged into the unmanned aerial vehicle reverse braking gun 1, the clamping block 806 on the outer side of the storage battery 6 can be in contact with the clamping block 804 to drive the clamping block 804 and the through rod 803 to move, the clamping spring 805 contracts, and when the clamping block 806 moves above the clamping block 804, the clamping spring 805 rebounds to drive the clamping block 804 to move to clamp the clamping block 806, so that the plugged storage battery 6 can be conveniently and fixedly clamped, and when the storage battery 6 needs to be disassembled, the two pull plates 807 are pulled to drive the clamping block 806 to be separated from the clamping block 804, so that the storage battery 6 is disassembled;
before the user uses the unmanned aerial vehicle reverse braking gun 1, the L-shaped placing plate 902 can be pulled out from the placing groove 901, the user can place the display equipment on one side of the sliding clamp 905, the display equipment is clamped and placed through the sliding clamp 905 and the clamping spring 906, the sun visor 907 can be turned over, the position of the sun visor 907 is fixed through the fixing band 908 and the magic tape 909 at the top end of the sun visor 907, and the user can hold and place the rest display equipment required to be used when holding the unmanned aerial vehicle reverse braking gun 1;
when the radar detection system of the unmanned aerial vehicle is used, the radio monitoring, the radar monitoring and the visible light infrared monitoring contained in the detection end can carry out multi-aspect monitoring on the no-fly area, the monitoring result is transmitted to the processing end in real time through the signal transmitter and the signal receiver, the information transmitted by the radio monitoring, the radar monitoring and the visible light infrared monitoring can be analyzed and processed through the server and the spectrum characteristic recognition and analysis processor contained in the processing end, the information is compared and recognized with a pre-constructed transmitter spectrum characteristic library of a common unmanned aerial vehicle, the model of the unmanned aerial vehicle is recognized, the longitude and latitude information, the carrier frequency information and the height information of the unmanned aerial vehicle are obtained through analysis, then the model, the carrier frequency information, the longitude and latitude information and the height information of the unmanned aerial vehicle are transmitted to the display terminal through the display sub-module, and are displayed to a user in real time, the monitoring information is stored locally in real time, if the unmanned aerial vehicle breaks into the no-fly area, a user can transmit the monitoring result to a corresponding unmanned aerial vehicle anti-gun position, and the unmanned aerial vehicle breaking into the no-fly area is subjected to interference anti-gun by the unmanned aerial vehicle;
when this unmanned aerial vehicle's radar detection method uses, at first according to the regional size in the control area, erect radio monitoring, radar monitoring and visible infrared monitoring, realize carrying out real-time supervision to the control area, the unmanned aerial vehicle information that real-time supervision gathered can carry out analysis processes, the analysis reachs unmanned aerial vehicle's spectral feature information, unmanned aerial vehicle longitude and latitude height information, unmanned aerial vehicle carrier frequency information and unmanned aerial vehicle remote control position information, and classify, show on display device after with analysis processes ' information arrangement afterwards, the user can be according to the monitoring and the result that show, the remote transmission monitoring result, the corresponding unmanned aerial vehicle of coordinated control counteracts rifle, disturb the reaction to the unmanned aerial vehicle target, after last monitoring ends, the activity summary report is generated automatically, summarize the unmanned aerial vehicle control result.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (4)
1. The utility model provides an unmanned aerial vehicle's radar detection system, includes unmanned aerial vehicle reverse braking rifle (1), its characterized in that: a control panel (2) is embedded into one end of the unmanned aerial vehicle reverse gun (1), a handle (3) is connected to the bottom end of the unmanned aerial vehicle reverse gun (1), an interference unit (4) is connected to one end of the unmanned aerial vehicle reverse gun (1), a control handle (5) is installed at a position, corresponding to one side of the handle (3), of the bottom end of the unmanned aerial vehicle reverse gun (1), and a storage battery (6) is installed at a position, corresponding to the middle of the handle (3) and the control handle (5), of the bottom end of the unmanned aerial vehicle reverse gun (1);
the unmanned aerial vehicle reverse braking gun (1) is characterized in that the other end of the unmanned aerial vehicle reverse braking gun (1) is connected with a fixed mounting mechanism (7), and the fixed mounting mechanism (7) comprises a placing groove (701), a connecting rod (702), a limiting plate (703), a return spring (704), a rotating connecting seat (705), a fixed connecting seat (706), a first placing clamp plate (707), a penetrating connecting rod (708), a limiting connecting plate (709), a second placing clamp plate (710), a placing spring (711), a clamping binding band (712) and a fixed seat (713);
the unmanned aerial vehicle reverse-braking gun is characterized in that a placing groove (701) is symmetrically formed in the other end of the unmanned aerial vehicle reverse-braking gun (1), a connecting rod (702) is slidably mounted on the inner wall of the placing groove (701), a limiting plate (703) is connected to the position, corresponding to the inside of the placing groove (701), of one end of the connecting rod (702), a reset spring (704) is connected to the position, corresponding to one side of the limiting plate (703), of the outer side of the connecting rod (702), a rotating connecting seat (705) is connected to the other end of the connecting rod (702), a fixed connecting seat (706) is rotatably mounted on the outer side of the rotating connecting seat (705), a first placing clamp plate (707) is fixedly mounted at one end of the first placing clamp plate (707), a penetrating connecting rod (708) is symmetrically connected to one end of the first placing clamp plate (707), a limiting connecting plate (709) is connected to one end of the penetrating connecting rod (708), and a, the outer side of the penetrating connecting rod (708) is connected with a placing spring (711) at a position corresponding to one side of a second placing clamping plate (710), the bottom end of the second placing clamping plate (710) is connected with a clamping binding band (712), and a fixing seat (713) is connected at a position corresponding to the clamping binding band (712) at one end of the first placing clamping plate (707).
2. The radar detection system of the unmanned aerial vehicle as claimed in claim 1, wherein a storage battery fixing mechanism (8) is installed at the bottom end of the unmanned aerial vehicle reverse braking gun (1) corresponding to positions on two sides of the storage battery (6), and the storage battery fixing mechanism (8) comprises a fixing block (801), a fixing groove (802), a penetrating rod (803), a clamping block (804), a clamping spring (805), a clamping block (806) and a pulling plate (807);
the bottom of unmanned aerial vehicle reverse system rifle (1) corresponds battery (6) both sides position department and installs fixed block (801), fixed slot (802) have been seted up to the one end of fixed block (801), the even through connection of one end of fixed block (801) has through pole (803), the one end that runs through pole (803) is connected with fixture block (804), the outside that runs through pole (803) corresponds fixture block (804) one side position department and installs joint spring (805), the both ends of battery (6) correspond fixture block (804) position department fixed mounting has joint piece (806), the other end that runs through pole (803) passes fixed block (801) and is connected with arm-tie (807).
3. The radar detection system of the unmanned aerial vehicle as claimed in claim 1, wherein a placement mechanism (9) is embedded in one end of the unmanned aerial vehicle reverse braking gun (1), and the placement mechanism (9) comprises a placement groove (901), an L-shaped placement plate (902), a mounting groove (903), a fixing rod (904), a sliding clamp plate (905), a clamping spring (906), a sun shield (907), a fixing strap (908) and a magic tape (909);
the utility model discloses an unmanned aerial vehicle reverse system rifle (1) of unmanned aerial vehicle reverse system, including unmanned aerial vehicle reverse system rifle (1), the inner wall sliding connection who places recess (901) has the L type to place board (902), mounting groove (903) have been seted up on the top of board (902) is placed to the L type, the one end inner wall symmetric connection of mounting groove (903) has dead lever (904), the outside sliding mounting of dead lever (904) has slide plate (905), the outside of dead lever (904) corresponds slide plate (905) one side position department and is connected with grip spring (906), the L type is placed the one end rotation of board (902) and is connected with sunshading board (907), fixed band (908) is installed in the top embedding of sunshading board (907), the other end that board (902) was placed to the L type corresponds fixed band (908) position department and has magic.
4. The radar detection system of the unmanned aerial vehicle of claim 1, comprising a detection end, a processing end, a control transmission end and a control display terminal, wherein the detection end comprises radio monitoring, radar monitoring and visible light infrared monitoring, the processing end comprises a server, a spectrum feature recognition and analysis processor, the control transmission end comprises a remote controller, a signal transmitter and a signal receiver, the control display terminal comprises a display sub-module, a control terminal, a monitoring information local storage and an unmanned aerial vehicle reverse-control gun, the output end of the detection end is connected with the input end of the processing end, the output end of the processing end is connected with the input end of the control display terminal, and the output end of the control transmission end is connected with the input end of the detection end.
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