CN112722294A - Unmanned aerial vehicle with radar topography exploration function - Google Patents
Unmanned aerial vehicle with radar topography exploration function Download PDFInfo
- Publication number
- CN112722294A CN112722294A CN202110095330.3A CN202110095330A CN112722294A CN 112722294 A CN112722294 A CN 112722294A CN 202110095330 A CN202110095330 A CN 202110095330A CN 112722294 A CN112722294 A CN 112722294A
- Authority
- CN
- China
- Prior art keywords
- radar
- unmanned aerial
- aerial vehicle
- mounting
- main body
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000012876 topography Methods 0.000 title claims description 10
- 238000013016 damping Methods 0.000 claims abstract description 27
- 238000003466 welding Methods 0.000 claims description 7
- 238000003780 insertion Methods 0.000 claims description 5
- 230000037431 insertion Effects 0.000 claims description 5
- 230000006978 adaptation Effects 0.000 claims description 4
- 238000009434 installation Methods 0.000 abstract description 7
- 230000001846 repelling effect Effects 0.000 abstract description 3
- 238000001125 extrusion Methods 0.000 description 5
- 230000004888 barrier function Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D2045/0095—Devices specially adapted to avoid bird strike
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Geophysics And Detection Of Objects (AREA)
Abstract
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle with radar terrain exploration function, aiming at the problem of inconvenience in radar installation, the unmanned aerial vehicle comprises a main body, wherein a ferrule is arranged on the outer side of the main body, a connecting rod is welded on the outer side of the ferrule, a shell is welded at the top end of the connecting rod, a distance sensor is inlaid on the outer wall of the shell, a fixed plate is welded in the middle of the bottom of the main body, a mounting plate is arranged below the fixed plate, a sliding groove is formed in the fixed plate, a bar-shaped sliding block is arranged in the sliding groove, L-shaped inserting rods are welded on two sides of the middle of the top of the mounting plate, a damping rod is welded between one end of the sliding groove and one end of the. The radar has the advantages of simple mounting and dismounting steps, convenient and quick operation, time and labor saving, bird repelling and obstacle avoidance.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a radar terrain exploration function.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle is currently applied to the fields of aerial photography, wild animal observation, infectious disease monitoring, surveying and mapping, film and television shooting, terrain exploration and the like, and the application of the unmanned aerial vehicle is greatly expanded.
The existing radar of the unmanned aerial vehicle with the radar terrain exploration function is complex to operate during installation, and is inconvenient to operate and time-consuming and labor-consuming when the radar needs to be disassembled; moreover, the unmanned aerial vehicle with the radar terrain exploration function is generally used more in mountain areas and forest areas, and birds are more in the areas, so that more birds collide the unmanned aerial vehicle to cause the unmanned aerial vehicle to crash, and the economic loss is larger; the existing unmanned aerial vehicle with the radar terrain exploration function does not have the obstacle avoidance function, and the existing unmanned aerial vehicle easily collides with an obstacle in a region with complex terrain to cause crash.
Disclosure of Invention
Based on the technical problems in the background art, the invention provides an unmanned aerial vehicle with a radar terrain exploration function.
The invention provides an unmanned aerial vehicle with radar terrain exploration function, which comprises a main body and a radar, wherein the top of the outer side of the main body is rotatably connected with a ferrule, the outer side of the ferrule is welded with a connecting rod, the connecting rod is horizontally arranged, the top end of the connecting rod is welded with a shell, the shell is hemispherical and hollow, a distance sensor is embedded in the middle of the outer wall of the shell, a fixed plate is welded in the middle of the bottom of the main body, a mounting plate is arranged below the fixed plate, a sliding chute is formed in the fixed plate, a strip-shaped sliding block is arranged in the sliding chute, two sides of the middle of the top of the mounting plate are welded with L-shaped inserting rods, one end in the sliding chute is welded with a damping rod, the damping rod is horizontally arranged, the other end of the damping rod is welded, the bottom of bar slider is located the top of two L type inserted bars and has seted up the fixed slot, the fixed slot is equipped with two, two one side inner wall of fixed slot all is equipped with the slope, two the interior top of fixed slot respectively with the top looks adaptation of two L type inserted bars.
Preferably, the welding of the outside bottom of main part has the erection column, the erection column level sets up, the erection column is equipped with four, four the erection column is in the bottom outside evenly distributed of main part.
Preferably, the top ends of the four mounting columns are provided with propellers, and the two sides of the bottom of the main body are provided with landing gears.
Preferably, the top of the outer side of the main body is provided with an annular clamping groove, the middle part of the inner wall of the ferrule is welded with a clamping ring, the clamping ring is matched with the annular clamping groove, and the clamping ring is rotatably connected with the annular clamping groove.
Preferably, the number of the connecting rods is three, the three connecting rods are uniformly distributed on the outer side of the ferrule, and the length of each connecting rod is greater than that of each mounting column.
Preferably, the radar is installed in the bottom middle part of mounting panel, signal reception antenna is installed to bottom one side of mounting panel, signal emission antenna is installed to the bottom opposite side of mounting panel.
Preferably, the signal receiving antenna and the signal transmitting antenna are both arranged vertically, and the radar is arranged vertically downwards.
Preferably, the sliding groove is horizontally arranged, and the strip-shaped sliding block is horizontally arranged inside the sliding groove and is in sliding connection with the sliding groove.
Preferably, two the equal vertical setting of L type inserted bar, the jack with L type inserted bar top looks adaptation is seted up to the bottom of fixed plate, and jack and spout intercommunication.
Preferably, the bolt passes through the screw thread and is connected with the fixed plate, inside the bolt stretches into the spout, the bolt level sets up, the bolt other end and the butt of bar slider other end.
The beneficial effects of the invention are as follows:
1. this unmanned aerial vehicle with radar topography exploration function, insert post and bar slider through being provided with the L type, when needs installation radar, insert the jack of post alignment fixed plate bottom with two L types inside the spout, the top rebound extrusion slope of post is inserted to the L type, drive bar slider and remove extrusion damping rod to the damping rod direction in the spout is inside, the top of inserting the post until the L type removes the interior top to the fixed slot, bar slider restores the normal position under the bounce effect of damping rod, insert the top card of post at the interior top of fixed slot with the L type, make the L type insert the post unable downstream, then with mounting panel fixed mounting in the bottom of fixed plate, the installation steps of radar is simple, high convenience and fast operation, time and labor saving.
2. This unmanned aerial vehicle with radar topography exploration function, through being provided with the bolt, when the radar is dismantled to needs, only need to rotate the top that the bolt made the bolt and to spout inside removal, then the bolt drives the bar slider and removes the extrusion damping rod to the damping rod direction inside the spout, insert the top of post until the L type and shift out from the interior top of fixed slot, thereby can insert the post with the L type and extract downwards, dismantle the mounting panel from the fixed plate bottom, the derotation bolt can make the bar slider answer the normal position, the dismantlement of radar is convenient and fast equally, time saving and labor saving.
3. This unmanned aerial vehicle with radar topography exploration function, through being provided with connecting rod and casing, when unmanned aerial vehicle goes the in-process at the eminence, thereby the influence that the casing received wind-force drives the lasso through the connecting rod and rotates in the main part outside, thereby make three connecting rod and casing rotate in the main part periphery, and the length of connecting rod is greater than the length of erection column, then the casing in the rotation can play the effect of driving the bird, prevent that birds from offeing unmanned aerial vehicle and leading to the unmanned aerial vehicle crash, avoid causing unnecessary economic loss.
4. This unmanned aerial vehicle with radar topography exploration function through being provided with distance sensor, through the mid-mounting at three casing outer wall with distance sensor, the pivoted in-process of three casing, and distance sensor is real-time surveys the casing and the distance of barrier all around, and when the distance is nearer, control system control unmanned aerial vehicle conversion direction of travel avoids unmanned aerial vehicle to collide the barrier and leads to the crash, has the obstacle avoidance function.
The parts of the device not involved are the same as or can be implemented using prior art.
Drawings
Fig. 1 is a schematic diagram of a split state of an unmanned aerial vehicle with radar terrain exploration provided by the invention;
FIG. 2 is a schematic diagram of an installation state of an unmanned aerial vehicle with radar terrain exploration function according to the present invention;
FIG. 3 is a partial sectional view of an installation state of an unmanned aerial vehicle with radar terrain surveying function according to the present invention;
FIG. 4 is a partial sectional view of a disassembled state of the UAV with radar topography function according to the present invention;
fig. 5 is a top cross-sectional view of a housing of a drone with radar terrain surveying capability according to the present invention.
In the figure: 1. a housing; 2. a connecting rod; 3. a ferrule; 4. a snap ring; 5. an annular neck; 6. a distance sensor; 7. mounting a column; 8. a propeller; 9. a main body; 10. a signal receiving antenna; 11. a radar; 12. mounting a plate; 13. a landing gear; 14. a fixing plate; 15. a signal transmitting antenna; 16. an L-shaped inserted link; 17. a chute; 18. a bar-shaped slider; 19. a bolt; 20. a damping lever; 21. a slope; 22. and fixing the grooves.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
Referring to fig. 1-5, an unmanned aerial vehicle with radar topography exploration function comprises a main body 9 and a radar 11, wherein the top of the outer side of the main body 9 is rotatably connected with a ferrule 3, the outer side of the ferrule 3 is welded with a connecting rod 2, the connecting rod 2 is horizontally arranged, the top end of the connecting rod 2 is welded with a shell 1, the shell 1 is hemispherical and hollow, the shell 1 receives the influence of wind power so as to drive the ferrule 3 to rotate on the outer side of the main body 9 through the connecting rod 2, so that the three connecting rods 2 and the shell 1 rotate on the periphery of the main body 9, and the length of the connecting rod 2 is greater than that of a mounting 7 column, so that the rotating shell 1 can play a role of repelling birds, prevent birds from colliding with the unmanned aerial vehicle to cause crash, avoid causing unnecessary economic loss, a distance sensor 6 is inlaid in the middle part of, the distance sensor 6 detects the distance between the shell 1 and surrounding obstacles in real time, when the distance is short, the control system controls the unmanned aerial vehicle to change the driving direction to avoid the unmanned aerial vehicle from colliding with the obstacles to cause crash, and the distance sensor has an obstacle avoidance function, the middle part of the bottom of the main body 9 is welded with the fixed plate 14, the lower part of the fixed plate 14 is provided with the mounting plate 12, the inside of the fixed plate 14 is provided with a sliding chute 17, the inside of the sliding chute 17 is provided with a bar-shaped sliding block 18, the two sides of the middle part of the top of the mounting plate 12 are welded with L-shaped inserting rods 16, one end inside the sliding chute 17 is welded with a damping rod 20, the damping rod 20 is horizontally arranged, the other end of the damping rod 20 is welded with one end of the bar-shaped sliding block 18, one side of the outside of the fixed plate 14, which is far away from the, the interior top of two fixed slots 22 respectively with the top looks adaptation of two L type inserted bars 16, the top of post 16 is inserted to the L type moves extrusion slope 21 upwards, drive bar slider 18 and remove extrusion damping rod 20 to damping rod 20 direction in spout 17 is inside, the top of inserting post 16 until the L type removes to the interior top of fixed slot 22, bar slider 18 restores the normal position under damping rod 20's bounce-back effect, insert the top card of post 16 with the L type at the interior top of fixed slot 22, make the L type insert the unable downstream of post 16, then with mounting panel 12 fixed mounting in the bottom of fixed plate 14, radar 11's installation step is simple, and convenient operation is swift, time saving and labor saving.
According to the invention, the mounting columns 7 are welded at the bottom of the outer side of the main body 9, the mounting columns 7 are horizontally arranged, the number of the mounting columns 7 is four, and the four mounting columns 7 are uniformly distributed at the outer side of the bottom of the main body 9.
In the invention, propellers 8 are arranged at the top ends of four mounting columns 7, and landing gears 13 are arranged on two sides of the bottom of a main body 9.
According to the invention, the top of the outer side of the main body 9 is provided with the annular clamping groove 5, the middle part of the inner wall of the ferrule 3 is welded with the clamping ring 4, the clamping ring 4 is matched with the annular clamping groove 5, the clamping ring 4 is rotatably connected with the annular clamping groove 5, and the ferrule 3 is clamped into the annular clamping groove 5 through the clamping ring 4 and is arranged on the outer side of the main body 9.
In the invention, three connecting rods 2 are arranged, the three connecting rods 2 are uniformly distributed on the outer side of the ferrule 3, and the length of each connecting rod 2 is greater than that of the mounting column 7.
In the invention, a radar 11 is arranged in the middle of the bottom of a mounting plate 12, a signal receiving antenna 10 is arranged on one side of the bottom of the mounting plate 12, a signal transmitting antenna 15 is arranged on the other side of the bottom of the mounting plate 12, the radar 11 detects the terrain, and the signal receiving antenna 10 and the signal transmitting antenna 15 respectively reinforce the signal receiving and transmitting of the signal.
In the present invention, the signal receiving antenna 10 and the signal transmitting antenna 15 are both vertically disposed, and the radar 11 is disposed vertically downward.
In the invention, the sliding groove 17 is horizontally arranged, and the strip-shaped sliding block 18 is horizontally arranged in the sliding groove 17 and is in sliding connection with the sliding groove 17.
In the invention, two L-shaped inserting rods 16 are both vertically arranged, the bottom of the fixing plate 14 is provided with an inserting hole matched with the top end of the L-shaped inserting rod 16, the inserting hole is communicated with the sliding groove 17, and the two L-shaped inserting columns 16 are inserted into the sliding groove 17 by aligning with the inserting hole at the bottom of the fixing plate 14.
In the invention, a bolt 19 is connected with a fixed plate 14 through threads, the bolt 19 extends into a sliding groove 17, the bolt 19 is horizontally arranged, the other end of the bolt 19 is abutted against the other end of a strip-shaped sliding block 18, the bolt 19 is rotated to enable the top end of the bolt 19 to move towards the inside of the sliding groove 17, and then the bolt 19 drives the strip-shaped sliding block 18 to move towards a damping rod 20 in the sliding groove 17 to extrude the damping rod 20.
The working principle is as follows: when the radar 11 needs to be installed, two L-shaped inserting columns 16 are aligned with insertion holes in the bottom of a fixing plate 14 and inserted into a sliding groove 17, the top ends of the L-shaped inserting columns 16 move upwards to extrude a slope 21, a strip-shaped sliding block 18 is driven to move towards a damping rod 20 in the sliding groove 17 to extrude the damping rod 20 until the top ends of the L-shaped inserting columns 16 move to the inner top of the fixing groove 22, the strip-shaped sliding block 18 returns to the original position under the action of the rebound force of the damping rod 20, the top ends of the L-shaped inserting columns 16 are clamped at the inner top of the fixing groove 22, the L-shaped inserting columns 16 cannot move downwards, the mounting plate 12 is fixedly installed at the bottom of the fixing plate 14, and the radar 11 is simple in mounting step, convenient and; when the radar 11 needs to be disassembled, the bolt 19 is only required to be rotated to enable the top end of the bolt 19 to move towards the inside of the sliding groove 17, the bolt 19 drives the strip-shaped sliding block 18 to move towards the direction of the damping rod 20 in the sliding groove 17 to extrude the damping rod 20 until the top end of the L-shaped inserting column 16 moves out of the inner top of the fixing groove 22, so that the L-shaped inserting column 16 can be pulled out downwards, the mounting plate 12 is disassembled from the bottom of the fixing plate 14, the strip-shaped sliding block 18 can be restored to the original position by reversely rotating the bolt 19, the radar 11 is also convenient and rapid to disassemble, and time; when the unmanned aerial vehicle runs at a high place, the shell 1 receives the influence of wind power so as to drive the ferrule 3 to rotate outside the main body 9 through the connecting rods 2, so that the three connecting rods 2 and the shell 1 rotate around the main body 9, and the length of the connecting rods 2 is greater than that of the mounting 7 columns, so that the rotating shell 1 can play a role in repelling birds, birds are prevented from colliding with the unmanned aerial vehicle to cause the unmanned aerial vehicle to crash, and unnecessary economic loss is avoided; through the mid-mounting at the 1 outer wall of three casing there is distance sensor 6, the pivoted in-process of three casing 1, and distance sensor 6 is real-time surveys casing 1 and the distance of barrier all around, and when the distance was nearer, control system control unmanned aerial vehicle conversion direction of travel avoided unmanned aerial vehicle to collide the barrier and lead to the crash, has the obstacle avoidance function.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle with radar topography exploration function, includes main part (9) and radar (11), its characterized in that, the outside top of main part (9) is rotated and is connected with lasso (3), the outside welding of lasso (3) has connecting rod (2), connecting rod (2) level sets up, the top welding of connecting rod (2) has casing (1), casing (1) is hemisphere and inside cavity, inlay in the outer wall middle part of casing (1) has distance sensor (6), the bottom middle part welding of main part (9) has fixed plate (14), the below of fixed plate (14) is equipped with mounting panel (12), spout (17) have been seted up to the inside of fixed plate (14), spout (17) inside is equipped with bar slider (18), the top middle part both sides welding of mounting panel (12) has L type inserted bar (16), the welding of the inside one end of spout (17) has damping rod (20), damping rod (20) level sets up, the one end welding of damping rod (20) other end and bar slider (18), damping rod (20) one side is kept away from in fixed plate (14) outside runs through bolt (19), fixed slot (22) have been seted up to the top that the bottom of bar slider (18) is located two L type inserted bars (16), fixed slot (22) are equipped with two, two one side inner wall of fixed slot (22) all is equipped with slope (21), two the interior top of fixed slot (22) respectively with the top looks adaptation of two L type inserted bars (16).
2. The unmanned aerial vehicle with radar terrain surveying function of claim 1, characterized in that mounting columns (7) are welded to the bottom of the outer side of the main body (9), the mounting columns (7) are horizontally arranged, the number of the mounting columns (7) is four, and the four mounting columns (7) are uniformly distributed on the outer side of the bottom of the main body (9).
3. The drone with radar terrain surveying function of claim 2, characterized in that the four mounting columns (7) are each fitted with a propeller (8) at their top end and the main body (9) is fitted with landing gears (13) on both sides of its bottom.
4. The unmanned aerial vehicle with radar terrain surveying function of claim 3, characterized in that the top of the outer side of the main body (9) is provided with a ring-shaped clamping groove (5), the middle part of the inner wall of the ferrule (3) is welded with a clamping ring (4), the clamping ring (4) is matched with the ring-shaped clamping groove (5), and the clamping ring (4) is rotatably connected with the ring-shaped clamping groove (5).
5. The drone with radar terrain surveying function of claim 4, characterized in that there are three connecting rods (2), three connecting rods (2) being evenly distributed outside the collar (3), the length of the connecting rods (2) being greater than the length of the mounting posts (7).
6. A drone with radar topographic exploration function according to claim 5, characterised in that the radar (11) is mounted in the middle of the bottom of the mounting plate (12), the bottom side of the mounting plate (12) being equipped with a signal receiving antenna (10) and the other bottom side of the mounting plate (12) being equipped with a signal transmitting antenna (15).
7. A drone with radar terrain surveying functionality according to claim 6, characterised in that the signal receiving antenna (10) and the signal transmitting antenna (15) are both arranged vertically, the radar (11) being arranged vertically downwards.
8. The drone with radar terrain surveying function of claim 7, characterized in that the chute (17) is horizontally arranged, the bar-shaped slider (18) being horizontally arranged inside the chute (17) and being in sliding connection with the chute (17).
9. The unmanned aerial vehicle with radar terrain surveying function of claim 8, wherein the two L-shaped insertion rods (16) are vertically arranged, the bottom of the fixing plate (14) is provided with insertion holes matched with the top ends of the L-shaped insertion rods (16), and the insertion holes are communicated with the sliding grooves (17).
10. The unmanned aerial vehicle with radar topography exploration function of claim 9, wherein the bolt (19) is connected with the fixing plate (14) through a thread, the bolt (19) extends into the sliding groove (17), the bolt (19) is horizontally arranged, and the other end of the bolt (19) is abutted with the other end of the strip-shaped sliding block (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110095330.3A CN112722294A (en) | 2021-01-25 | 2021-01-25 | Unmanned aerial vehicle with radar topography exploration function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110095330.3A CN112722294A (en) | 2021-01-25 | 2021-01-25 | Unmanned aerial vehicle with radar topography exploration function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112722294A true CN112722294A (en) | 2021-04-30 |
Family
ID=75593852
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110095330.3A Pending CN112722294A (en) | 2021-01-25 | 2021-01-25 | Unmanned aerial vehicle with radar topography exploration function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112722294A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104656665A (en) * | 2015-03-06 | 2015-05-27 | 云南电网有限责任公司电力科学研究院 | Novel general obstacle avoidance module for UAV (unmanned aerial vehicle) and steps |
| CN204409380U (en) * | 2015-01-27 | 2015-06-24 | 马鞍山市赛迪智能科技有限公司 | One drives bird unmanned vehicle |
| CN105093237A (en) * | 2015-09-08 | 2015-11-25 | 零度智控（北京）智能科技有限公司 | Detection device of barriers for unmanned plane and detection method thereof |
| CN205390157U (en) * | 2016-03-18 | 2016-07-27 | 马春 | Drive bird unmanned aerial vehicle |
| CN105955303A (en) * | 2016-07-05 | 2016-09-21 | 北京奇虎科技有限公司 | UAV autonomous obstacle avoidance method and device |
| CN109625283A (en) * | 2019-01-22 | 2019-04-16 | 广州市妙伊莲科技有限公司 | A kind of unmanned flight's device with rainproof function for logistics distribution |
| CN110226438A (en) * | 2019-06-20 | 2019-09-13 | 潍坊学院 | A kind of hybrid orchard bird-repellent robots of solar wind-energy |
| CN210027950U (en) * | 2019-03-26 | 2020-02-07 | 徐新宇 | Unmanned aerial vehicle with protection architecture has obstacle avoidance function |
| CN211592976U (en) * | 2019-12-12 | 2020-09-29 | 扬州几何无人机科技有限公司 | Unmanned aerial vehicle with radar topography exploration function |
| CN111746811A (en) * | 2020-07-17 | 2020-10-09 | 杭州同济测绘有限公司 | Unmanned aerial vehicle photogrammetry mounting platform |
-
2021
- 2021-01-25 CN CN202110095330.3A patent/CN112722294A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204409380U (en) * | 2015-01-27 | 2015-06-24 | 马鞍山市赛迪智能科技有限公司 | One drives bird unmanned vehicle |
| CN104656665A (en) * | 2015-03-06 | 2015-05-27 | 云南电网有限责任公司电力科学研究院 | Novel general obstacle avoidance module for UAV (unmanned aerial vehicle) and steps |
| CN105093237A (en) * | 2015-09-08 | 2015-11-25 | 零度智控（北京）智能科技有限公司 | Detection device of barriers for unmanned plane and detection method thereof |
| CN205390157U (en) * | 2016-03-18 | 2016-07-27 | 马春 | Drive bird unmanned aerial vehicle |
| CN105955303A (en) * | 2016-07-05 | 2016-09-21 | 北京奇虎科技有限公司 | UAV autonomous obstacle avoidance method and device |
| CN109625283A (en) * | 2019-01-22 | 2019-04-16 | 广州市妙伊莲科技有限公司 | A kind of unmanned flight's device with rainproof function for logistics distribution |
| CN210027950U (en) * | 2019-03-26 | 2020-02-07 | 徐新宇 | Unmanned aerial vehicle with protection architecture has obstacle avoidance function |
| CN110226438A (en) * | 2019-06-20 | 2019-09-13 | 潍坊学院 | A kind of hybrid orchard bird-repellent robots of solar wind-energy |
| CN211592976U (en) * | 2019-12-12 | 2020-09-29 | 扬州几何无人机科技有限公司 | Unmanned aerial vehicle with radar topography exploration function |
| CN111746811A (en) * | 2020-07-17 | 2020-10-09 | 杭州同济测绘有限公司 | Unmanned aerial vehicle photogrammetry mounting platform |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206147927U (en) | Unmanned aerial vehicle's remote controller structure | |
| US11629937B2 (en) | Device and method of anti-unmanned aerial vehicle based on multi-camera tracking and positioning | |
| CN107505953B (en) | Unmanned aerial vehicle automatic tracking antenna system and tracking method thereof | |
| CN109283521A (en) | It blocks the method for unmanned plane and blocks the anti-UAV system of formula | |
| CN112291726A (en) | Unmanned aerial vehicle cluster communication transmission system based on public wireless communication network | |
| CN112722294A (en) | Unmanned aerial vehicle with radar topography exploration function | |
| CN107943084A (en) | A kind of trailing type electromagnetic interference system and method for civilian multi-rotor unmanned aerial vehicle | |
| CN105827260A (en) | Voice control unmanned aerial vehicle | |
| CN219044414U (en) | Rotatable camera cradle head capable of carrying common unmanned aerial vehicle | |
| CN210912907U (en) | Unmanned aerial vehicle that can diversely survey | |
| CN212163312U (en) | ADS-B receiving equipment | |
| CN113446492A (en) | Fixing support of synthetic aperture radar | |
| CN107628226A (en) | The attachment structure of rotor wing unmanned aerial vehicle horn and fuselage | |
| CN208860915U (en) | A kind of grounded screen topological structure adaptive cruise measuring device | |
| CN214420716U (en) | Unmanned aerial vehicle received signal prevents interrupting auto-change over device | |
| CN206989809U (en) | The electromagnetic gun of Full-automatic reverse unmanned plane | |
| CN210321424U (en) | Unmanned on duty's anti unmanned aerial vehicle wireless spectrum detection device | |
| CN212435682U (en) | Broadcast signal transmitting device | |
| CN218645225U (en) | Unmanned Aerial Vehicle (UAV) ground-imitating radar | |
| CN211127945U (en) | Intelligent pipeline camera | |
| CN220673820U (en) | Monitoring equipment for community security protection | |
| CN220272732U (en) | Antenna device for inducing unmanned aerial vehicle navigation | |
| CN220544241U (en) | High-power antenna | |
| CN216774855U (en) | Unmanned aerial vehicle image data real-time processing system | |
| CN214473935U (en) | Agricultural unmanned aerial vehicle keeps away barrier device based on radar system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20210430 |