CN112902758A - Anti-unmanned aerial vehicle flight platform - Google Patents
Anti-unmanned aerial vehicle flight platform Download PDFInfo
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- CN112902758A CN112902758A CN202110350406.2A CN202110350406A CN112902758A CN 112902758 A CN112902758 A CN 112902758A CN 202110350406 A CN202110350406 A CN 202110350406A CN 112902758 A CN112902758 A CN 112902758A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
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Abstract
The invention belongs to the technical field of anti-unmanned aerial vehicles, and relates to an anti-unmanned aerial vehicle flight platform which comprises: the device comprises a first flying wing, a second flying wing, a separation module fixed on the first flying wing and an adjusting module fixed on the second flying wing; the separation module separates the first flying wing from the second flying wing; the adjusting module is used for adjusting the distance between the first flying wing and the second flying wing; the separation module is movably connected with the adjustment module, and also comprises a control module and a communication module, wherein the control module is used for processing target information returned by the detection module, performing three-dimensional detection and positioning on a target, and outputting a tracking instruction to the power module and the adjustment module; the communication module is used for establishing two-way communication between the first flying wing and the second flying wing. The invention can realize positioning, tracking and capturing of the invading unmanned aerial vehicles, can capture the invading unmanned aerial vehicles with different sizes, has the advantages of high positioning precision, flexible response, repeated capturing and no secondary damage, and has flexible and efficient capturing mode and no secondary damage risk to the ground.
Description
Technical Field
The invention belongs to the technical field of anti-unmanned aerial vehicles, and particularly relates to an anti-unmanned aerial vehicle identification, tracking and capturing platform.
Background
At present, the counter measure of the unmanned aerial vehicle is various, such as suppression type radio interference, deception type unmanned aerial vehicle interference, direct damage or physical counter measure of catching, but the counter measure has the problems of unsatisfactory counter measure effect, overhigh cost, easy secondary damage and the like.
For example, the patent application No. 201610062946.X discloses a fixed anti-drone interceptor system, which intercepts a drone by an interceptor net, a traction net rocket device, a collision air foaming impact device and an electromagnetic guiding device. When the unmanned aerial vehicle comes, the net body rocket device is pulled to carry the intercepting net body to rise and reach the highest point, the net body is suspended in the air, the net body is folded through the electromagnetic guiding device, a net bag is formed, and the function of capturing the unmanned aerial vehicle is achieved. The disadvantage of this invention is that the maneuverability is poor and the drone can only be captured in one fixed position.
An anti-unmanned aerial vehicle system based on a fixed-wing platform is provided as patent application No. 201910814581.5, and remote capture of an intruding unmanned aerial vehicle is realized by installing a capture system on a fixed-wing aircraft. The fixed wing unmanned aerial vehicle is immediately launched after receiving the task of the long-distance anti-unmanned aerial vehicle and flies to a target area under the guidance of a ground radar and a middle guidance device; after entering a target area, the tail end vision guidance system finishes tracking and returns accurate target position information and attitude information, and the fixed wing unmanned aerial vehicle platform resolves in real time and rapidly launches the net capture system to carry out net capture on the target. The invention has the defect that after the capture net captures the invading unmanned aerial vehicle, the capture net can not be controlled, so that secondary damage to a ground target is easily caused.
Patent application for application No. 201720455823.2 provides a high maneuvering active capture type anti-unmanned aerial vehicle system, which captures an invading unmanned aerial vehicle through a capture net installed in a capture frame at the front part of a fuselage. However, the unmanned aerial vehicle in the scheme only has two wings, and has poor control stability when flying without ailerons, horizontal tails and vertical tails; in addition, the capturing frame is arranged at the front part of the machine body, so that the posture is easy to fall down and is easy to lose control after the unmanned aerial vehicle is captured and invaded; furthermore, the catch frame size is fixed, can only catch the unmanned aerial vehicle that the size is less than catch frame size.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention provides the anti-unmanned aerial vehicle flight platform, which can realize positioning, tracking and capturing of the invading unmanned aerial vehicle, can capture the invading unmanned aerial vehicles with different sizes, and has the advantages of high positioning precision, flexible response, repeated capturing and no secondary damage. In order to achieve the purpose, the invention adopts the following specific technical scheme:
an anti-drone flight platform comprising: the device comprises a first flying wing, a second flying wing, a separation module fixed on the first flying wing and an adjusting module fixed on the second flying wing;
the separation module separates the first flying wing from the second flying wing;
the adjusting module is used for adjusting the distance between the first flying wing and the second flying wing;
the separation module is movably connected with the adjusting module.
Preferably, the first flying wing and the second flying wing are in a swept-back wing layout and are two identical flat flying wings arranged in parallel.
Preferably, the sweep angle of the first and second flyers is between 5 ° and 45 °.
Preferably, the separation module comprises a base, a connecting shaft and an electromagnet fixed on the base;
the base is fixed on the first flying wing, vertical plate through holes are processed on two parallel base vertical plates of the base, the two vertical plate through holes are coaxial, and the diameter of each vertical plate through hole is larger than the outer diameter of the connecting shaft, so that the connecting shaft can pass through the vertical plate through holes;
the connecting shaft is rigidly connected with the electromagnet;
the electromagnet is a push-pull electromagnet, so that the connecting shaft is pulled away from the through hole of the vertical plate.
Preferably, the adjusting module comprises a ball screw linear mechanism and a scissor-type lifting mechanism, and the ball screw linear mechanism drives the scissor-type lifting mechanism to stretch and retract so as to realize the adjustment of the spacing; the telescopic direction is perpendicular to the first flying wing and the second flying wing.
Preferably, the adjusting module further comprises an upper support frame and a lower support frame for fixing the scissor lift mechanism; a ball screw linear mechanism is also fixed on one surface of the lower support frame, which is fixed with the scissor type lifting mechanism; the other side of the lower support frame is fixed on the second flying wing.
Preferably, one side of the upper support frame is used for fixing the scissor type lifting mechanism, and the other side of the upper support frame is used for connecting the separation mechanism; the surface processing for connecting the separating mechanism has two parallel connection risers, the interval of the connection riser is greater than or less than the interval of the base riser, the center processing of the connection riser has a connecting through hole, the two connecting through holes are coaxial with the riser through hole, and the diameter of the connecting through hole is not less than the diameter of the riser through hole.
Preferably, a connecting shell matched with the shape of the adjusting module is attached to the adjusting module, and the connecting shell is used for accommodating the adjusting module and the separating module.
Preferably, the connecting shell is a foldable or telescopic shell with a symmetrical wing-shaped cross section.
Preferably, the system comprises a detection module, wherein the detection module comprises at least eight pairs of leading edge cameras and trailing edge cameras symmetrically arranged close to the wing root parts of the first flying wing and the second flying wing;
the front edge camera and the rear edge camera on the first flying wing and the second flying wing form a binocular system used for three-dimensional positioning of the target and obtaining of the image of the target.
Preferably, the leading edge camera and the trailing edge camera are visible light cameras or infrared cameras.
Preferably, the capturing module comprises a traction rope for connecting the capturing net and a steering engine, the steering engine is connected to the rear edges of the wingtips of the first flying wing and the second flying wing, and the traction rope and the steering engine are controlled by the steering engine to be connected and disconnected.
Preferably, the capture net and the tow rope are of an elastic material, reducing disturbance to the drone module when capturing the target.
Preferably, the power module comprises a power source and a propeller, and the lift-drag ratio and the control capability of the whole machine are improved by controlling the rotation direction of the propeller; the power source is a motor or an oil engine.
Preferably, the system also comprises a control module and a communication module,
the control module is used for processing the target information returned by the detection module, performing three-dimensional detection and positioning on the target and outputting a tracking instruction to the power module and the adjustment module;
the communication module is used for establishing communication with the ground command center when the first flying wing and the second flying wing are taken as a whole; and when the first flying wing and the second flying wing are separated, the two-way communication between the first flying wing and the second flying wing is established.
The invention can obtain the following technical effects:
1. the positioning, tracking and capturing of the invading unmanned aerial vehicle can be realized, the invading unmanned aerial vehicles with different sizes can be captured, and the positioning device has the advantages of high positioning precision, flexible reaction, repeated capturing and no secondary damage.
2. The unmanned aerial vehicle capturing device can capture small slow unmanned aerial vehicles and large high-speed unmanned aerial vehicles, is flexible and efficient in capturing mode, and does not have secondary damage risk to the ground.
Drawings
Fig. 1 is a schematic structural view of an anti-drone flight platform according to an embodiment of the present invention;
FIG. 2 is a functional block diagram of one embodiment of the present invention;
FIG. 3 is a schematic view of the position of a leading edge camera of one embodiment of the present invention;
FIG. 4 is a schematic illustration of the position of a trailing edge camera of one embodiment of the present invention;
FIG. 5 is a schematic view of a flying wing according to one embodiment of the present invention;
FIG. 6 is a schematic diagram of a capture module of one embodiment of the present invention;
FIG. 7 is a schematic diagram of a tuning module according to one embodiment of the invention;
FIG. 8 is a schematic view of a connection housing of one embodiment of the present invention;
FIG. 9 is a schematic diagram of a separation module according to one embodiment of the invention;
FIG. 10 is a schematic diagram of a separation module and an adjustment module according to one embodiment of the invention;
FIG. 11 is a schematic structural view of a second embodiment of the present invention;
FIG. 12 is a schematic structural view of a third embodiment of the present invention;
fig. 13 is a schematic structural diagram of a fourth embodiment of the present invention.
Reference numerals:
a first flying wing 1, a second flying wing 2, an aileron 21, a landing gear 22,
An adjusting module 3,
A ball screw linear mechanism 31, a ball slider 311, a screw shaft 312, a screw motor 313,
A scissor type lifting mechanism 32, a scissor hinge 321, a scissor arm 322, a sliding rod 323,
An upper supporting frame 33, a connecting vertical plate 34, a connecting shell 35, a lower supporting frame 36,
A separation module 4, a base 41, a base vertical plate 42, a connecting shaft 43, an electromagnet 44,
A detection module 5, a front edge camera 51, a rear edge camera 52,
A capture module 6, a capture net 61, a traction rope 62, a steering engine 63,
A power module 7, a first power module 71, a second power module 72, a third power module 73, a fourth power module 74, a propeller 75, a motor 76,
A control module 8,
The device comprises a communication module 9, a vertical tail 10, a horizontal tail 101, a connecting plate 102 and a machine body 103.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not to be construed as limiting the invention.
The invention aims to provide an anti-unmanned aerial vehicle flight platform which can realize positioning, tracking and capturing of an invasive unmanned aerial vehicle, can capture invasive unmanned aerial vehicles with different sizes, and has the advantages of high positioning precision, flexible reaction, repeated capturing and no secondary damage. The following will describe in detail an anti-drone flight platform provided by the present invention by using specific embodiments.
The anti-unmanned aerial vehicle flight platform structure shown in fig. 1 comprises a first flying wing 1, a second flying wing 2, a separation module 4 fixed on the first flying wing 1 and an adjustment module 3 fixed on the second flying wing 2, wherein the separation module 4 and the adjustment module 3 are movably connected and used for controlling the distance and the separation between the first flying wing 1 and the second flying wing 2.
In a preferred embodiment of the invention, the first flying wing 1 and the second flying wing 2 are two identical flat flying wings in a swept-wing layout, and the two flying wings are arranged in parallel; the device is connected with the adjusting module 3 through the separating modules 4 which are symmetrically distributed at two ends; the sweepback angle of the first flying wing 1 and the second flying wing 2 ranges from 5 degrees to 45 degrees.
Fig. 9 is a schematic view of a separation module, see fig. 9, comprising a base 41 fixed to the first flying wing 1, a connecting shaft 43 and an electromagnet 44;
two parallel base vertical plates 42 are processed on the base 41, and two ends of a connecting shaft 43 are respectively erected on the two base vertical plates 42; the height of the base vertical plates 42 is not lower than that of the electromagnets 44, and vertical plate through holes matched with the shaft diameter of the connecting shaft 43 are respectively processed on the two base vertical plates 42, so that the connecting shaft 43 can pass through the through holes;
the other end of the connecting shaft 43 is rigidly connected with an electromagnet 44, and the electromagnet 44 is a push-pull electromagnet which can enable the connecting shaft 43 to be pulled away from the vertical plate through hole.
Referring to the connection manner between the separation module and the adjustment module shown in fig. 10 and the structure of the adjustment module 3 shown in fig. 7, a connection vertical plate 34 corresponding to the position and height of the base vertical plate 42 is processed on the upper surface of the upper support frame 33 of the adjustment module 3, and a connection through hole having the same size as the vertical plate through hole is processed at the corresponding position of the connection vertical plate 34, so that the connection shaft 43 can pass through the vertical plate through hole and the connection through hole.
When the electromagnet 44 is not electrified, the connecting shaft 43 penetrates through the two vertical plate through holes and the two connecting through holes, so that the separation module 4 is connected with the adjusting module 3;
when the electromagnet 44 is energized, the connecting shaft 43 is pulled out from the two riser through holes and the two connecting through holes by the electromagnet 44, so that the separation of the separation module 4 from the adjustment module 3, that is, the separation of the first flying wing 1 from the second flying wing 2 is realized.
With continued reference to fig. 7, the adjusting module 3 further includes a ball screw linear mechanism 31, a scissor lift mechanism 32 and a lower support frame 36, one end of the scissor lift mechanism 32 is fixed on the bottom surface of the upper support frame 33, the other end and the ball screw linear mechanism 31 are fixed on the lower support frame 36, and the lower support frame 36 is fixed on the second flying wing 2.
In a preferred embodiment of the present invention, the ball slide block 311 of the ball screw linear mechanism 31 is rigidly connected to the slide bar 323 of the scissor lift mechanism 32, the screw motor 313 drives the screw shaft 312 to rotate, and the screw shaft 312 drives the ball slide block 311 to move linearly, so that the slide bar 323 moves linearly along the moving direction of the ball slide block 311;
meanwhile, the linear motion of the sliding rod 323 is converted into the rotation of the scissor arm 322 with the scissor hinge 321 as the center, and the up-and-down motion of the upper support frame 33 is realized through the rotation of the scissor arm 322 with a certain amplitude, so that the stepless adjustment of the distance between the first flying wing 1 and the second flying wing 2 is realized.
As shown in fig. 8, the connection housing 35 has a symmetrical wing profile for reducing the adverse effect of the adjustment module 3 on the aerodynamic performance of the anti-drone platform.
In a preferred embodiment of the present invention, the connection housing 35 is made of flexible material, and is attached to the adjustment module 3, and can be folded or slid to deform with the extension or contraction of the adjustment module 3 without affecting the operation of the adjustment module 3.
The anti-unmanned aerial vehicle flight platform further comprises a detection module 5, a capture module 6, a power module 7, a control module 8 and a communication module 9;
taking the structure of the second flying wing 2 shown in fig. 5 as an example, ailerons 21 for steering are symmetrically arranged on both sides of the first flying wing 1 and the second flying wing 2, and a landing gear 22 is further connected to the rear edges of the wing tip parts of the first flying wing 1 and the second flying wing 2; the first flying wing 1 and the second flying wing 2 are fixed with power modules 7 at the front edges of wing tip parts at two ends to realize lifting.
In a preferred embodiment of the present invention, with continued reference to fig. 5, a first power module 71 and a second power module 72 are respectively secured across the first flying wing 1, and a third power module 73 and a fourth power module 74 are respectively secured across the second flying wing 2; each power module 7 comprises a motor 76 and a propeller 75 connected to the motor 76; the motor 76 may be replaced with an oil engine.
In a preferred embodiment of the present invention, the propellers 75 on the first power module 71 and the third power module 73 rotate clockwise, and the propellers 75 on the second power module 72 and the fourth power module 74 rotate counterclockwise, so that the downwash flow of the propellers 75 inhibits the upwash flow of the wingtips of the flying wings, and the aerodynamic efficiency of the flying wings is increased.
Fig. 3 and 4 show the positions of eight sets of leading edge cameras 51 and trailing edge cameras 52 included in the detection module 5, four leading edge cameras 51 symmetrically fixing the leading edges of the first flying wing 1 and the second flying wing 2;
four trailing edge cameras 52 are symmetrically arranged at the trailing edges of the first flying wing 1 and the second flying wing 2;
the leading edge camera 51 is used for acquiring an image of the target unmanned aerial vehicle, and the control module 8 positions the position, speed and direction of the target unmanned aerial vehicle according to the acquired image of the target unmanned aerial vehicle;
the trailing edge camera 52 is used for acquiring landing area images, and the control module 8 calculates a safe landing position according to the acquired landing area images and guides the anti-unmanned aerial vehicle flying platform to land at the safe landing position.
In a preferred embodiment of the invention, the leading edge camera 51 and the trailing edge camera 52 on the same flying wing constitute a binocular system; the front edge camera 51 and the rear edge camera 52 are visible light cameras or are replaced by infrared cameras to meet the requirement of night work.
The airborne capturing module 6 shown in fig. 6 comprises a capturing net 61, steering engines 63 respectively symmetrically connected to the rear edges of wing tips of the first flying wing 1 and the second flying wing 2, and traction ropes 62 respectively connected to one ends of four steering engines 63;
the other ends of the four pulling ropes 62 are respectively connected with the four edges of the capturing net 61, and the pulling ropes 62 are disconnected from the steering engine 63 under the control of the steering engine 63 to release the capturing net 61.
In a preferred embodiment of the invention, elastic materials are chosen as the material of the capture net 61 and the tow rope 62 to reduce the disturbance to the anti-drone flight platform when capturing the target drone.
In a preferred embodiment of the present invention, the control module 8 is configured to process the target information returned by the detection module 5, perform stereo detection and positioning on the target, and output a tracking instruction to the power module 7 and the adjustment module 3.
In another embodiment of the present invention, the control module 8 is respectively disposed on the first flying wing 1 and the second flying wing 2, and is configured to receive the information from the detection module 5, locate and identify the target, and control the flight of the drone.
When the first flying wing 1 and the second flying wing 2 are not separated into two unmanned aerial vehicles, the two control modules 8 work simultaneously, one is a master control module, and the other is a slave control module for slave hot backup; when the first flying wing 1 and the second flying wing 2 are separated into two unmanned planes, the control module 8 controls the single flying wing where the control module is located.
In a preferred embodiment of the present invention, the communication module 9 is configured to send information such as position, speed, attitude, and the like of the anti-drone flight platform of the present invention and information such as position, speed, model, and size of the invading drone to the ground command control center.
The working principle of the invention is described in detail with reference to the working block diagram of the anti-unmanned aerial vehicle flight platform shown in fig. 2:
the anti-unmanned aerial vehicle flying platform flies to a target unmanned aerial vehicle at a high speed under the guidance of the detection module 5 and the control module 8, converts the invading unmanned aerial vehicle into a vertical landing mode after being captured in the capture net 61, and carries the captured target unmanned aerial vehicle to land to a safe place;
when the detection module 5 judges that the size of the target unmanned aerial vehicle is larger than the maximum value of the elongation of the adjustment module 3, the first flying wing 1 and the second flying wing 2 are separated to be changed into two capturing nets 61 of the unmanned aerial vehicle traction airborne capturing module 6 to capture the target unmanned aerial vehicle and convert the target unmanned aerial vehicle into a vertical landing mode, and the captured target unmanned aerial vehicle is carried to land to a safe place;
when the control module 8 judges that the weight of the captured unmanned aerial vehicle exceeds the load capacity processed by the platform, the control module 8 judges the safety range of the ground through the four groups of trailing edge cameras 52, guides the anti-unmanned aerial vehicle flight platform to fly to the safety range, controls the steering engine 63 to release the four traction ropes 62, and releases the captured target unmanned aerial vehicle to the ground safety place.
Fig. 11 is a schematic structural diagram of a second embodiment of the present invention, which operates in the same principle, except that a vertical tail 10 is installed at the rear edge of the connecting shell 35 to increase the control capability of the anti-drone flight platform during horizontal and vertical flight.
Fig. 12 is a schematic structural diagram of a third embodiment of the present invention, and on the basis of the second embodiment, horizontal tails 101 are symmetrically arranged at the rear portions of the trailing edges of a first flying wing 1 and a second flying wing 2, respectively, so as to increase the control capability of the anti-drone flight platform during horizontal and vertical flight.
Fig. 13 is a schematic structural diagram of a fourth embodiment of the present invention, which has the same working principle, and is different from the fourth embodiment in that the present invention does not include an adjusting module 3 and a separating module 4, two sets of connecting plates 102 are symmetrically added at the middle and near both ends of the first flying wing 1 and the second flying wing 2, respectively, and a fuselage 103 is added at the middle axis of the anti-drone flight platform, and a special spray and a spraying system can be carried on the fuselage 103.
When an invading unmanned aerial vehicle is found, the anti-unmanned aerial vehicle flight platform quickly approaches the invading unmanned aerial vehicle in a high-speed flat flying mode and emits special spraying agent to destroy a power system and a pneumatic structure of the anti-unmanned aerial vehicle flight platform so as to finish the counter-control of the invading unmanned aerial vehicle.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples and features of different embodiments or examples described in this specification can be combined and combined by one skilled in the art without contradiction.
Although embodiments of the present invention have been shown and described above, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art within the scope of the present invention.
The above embodiments of the present invention should not be construed as limiting the scope of the present invention. Any other corresponding changes and modifications made according to the technical idea of the present invention should be included in the protection scope of the claims of the present invention.
Claims (15)
1. An anti-unmanned aerial vehicle flight platform, comprising: the device comprises a first flying wing, a second flying wing, a separation module fixed on the first flying wing and an adjustment module fixed on the second flying wing;
the separation module separates the first flying wing from the second flying wing;
the adjusting module is used for adjusting the distance between the first flying wing and the second flying wing;
the separation module is movably connected with the adjusting module.
2. An anti-drone flight platform according to claim 1, wherein the first and second flyer bodies are in a swept-back wing configuration, being two identical, parallel, side-by-side flat flyers.
3. An anti-drone flight platform according to claim 2, wherein the sweepback angle of the first and second flying wings is between 5 ° and 45 °.
4. An anti-drone flight platform according to claim 1, wherein the separation module includes a base, a connecting shaft and an electromagnet fixed on the base;
the base is fixed on the first flying wing, vertical plate through holes are processed on two parallel base vertical plates of the base, the two vertical plate through holes are coaxial, and the diameter of each vertical plate through hole is larger than the outer diameter of the connecting shaft, so that the connecting shaft can penetrate through the corresponding vertical plate through hole;
the connecting shaft is rigidly connected with the electromagnet;
the electromagnet is a push-pull electromagnet, so that the connecting shaft is pulled away from the vertical plate through hole.
5. The anti-unmanned aerial vehicle flight platform of claim 1, wherein the adjustment module comprises a ball screw linear mechanism and a scissor type lifting mechanism, and the ball screw linear mechanism drives the scissor type lifting mechanism to extend and retract so as to adjust the distance; the telescopic direction is perpendicular to the first flying wing and the second flying wing.
6. An anti-drone flight platform according to claim 5, wherein the adjustment module further includes an upper support frame and a lower support frame for securing the scissor lift mechanism; the ball screw linear mechanism is also fixed on one surface of the lower support frame, which is used for fixing the scissor type lifting mechanism; the other side of the lower support frame is fixed on the second flying wing.
7. An anti-drone flight platform according to claim 6, wherein the upper support frame is used on one side to fix the scissor lift mechanism and on the other side to connect the disconnect mechanism; the surface processing for connecting branch the branch is said to have two parallel connection risers from the mechanism, the interval of connecting the riser is greater than or is less than the interval of base riser, the central processing of connecting the riser has connect the through-hole, two connect the through-hole with the riser through-hole is coaxial, and its diameter is not less than riser through-hole diameter.
8. An anti-drone flight platform according to claim 7, wherein the adjustment module has attached to it a connection housing adapted to the shape of the adjustment module, the connection housing being adapted to receive the adjustment module and the separation module.
9. An anti-drone flight platform according to claim 8, characterised in that the connection housing is collapsible or telescopic, with a cross-sectional shape of a shell of symmetrical wing profile.
10. The anti-drone flight platform of claim 1, further comprising a detection module comprising at least eight pairs of leading edge cameras and trailing edge cameras symmetrically disposed proximate the first and second flying wings at a wing root;
the leading edge cameras and the trailing edge cameras on the first flying wing and the second flying wing form a binocular system used for carrying out three-dimensional positioning on the target and obtaining an image of the target.
11. The anti-drone flight platform of claim 10, wherein the leading edge camera and the trailing edge camera are visible light cameras or infrared cameras.
12. The anti-UAV flight platform of claim 1, further comprising a capture module, wherein the capture module comprises a traction rope connecting a capture net and a steering engine, the steering engine is connected to the rear edges of the wingtips of the first and second flying wings, and the traction rope and the steering engine are controlled by the steering engine to be disconnected.
13. An anti-drone flight platform according to claim 12, wherein the capture net and the tow rope are resilient materials that reduce disturbance to the drone module when capturing the target.
14. The anti-unmanned aerial vehicle flight platform of claim 1, further comprising a power module, wherein the power module comprises a power source and a propeller, and the lift-drag ratio and the control capability of the whole machine are improved by controlling the rotation direction of the propeller; the power source is a motor or an oil engine.
15. An anti-drone flight platform according to claim 1, further comprising a control module and a communication module,
the control module is used for processing the target information returned by the detection module, performing three-dimensional detection and positioning on the target, and outputting a tracking instruction to the power module and the adjustment module;
the communication module is used for establishing communication with a ground command center when the first flying wing and the second flying wing are taken as a whole; and when the first flying wing and the second flying wing are separated, the two-way communication device is used for establishing two-way communication between the first flying wing and the second flying wing.
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113959267A (en) * | 2021-09-30 | 2022-01-21 | 国研软件股份有限公司 | Mist wall spray for interfering small aircraft, and using equipment and using method thereof |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113959267A (en) * | 2021-09-30 | 2022-01-21 | 国研软件股份有限公司 | Mist wall spray for interfering small aircraft, and using equipment and using method thereof |
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