CN115285367A - Triphibian unmanned aerial vehicle monitoring devices of land, water and air - Google Patents
Triphibian unmanned aerial vehicle monitoring devices of land, water and air Download PDFInfo
- Publication number
- CN115285367A CN115285367A CN202210958195.5A CN202210958195A CN115285367A CN 115285367 A CN115285367 A CN 115285367A CN 202210958195 A CN202210958195 A CN 202210958195A CN 115285367 A CN115285367 A CN 115285367A
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- aerial vehicle
- unmanned aerial
- monitoring
- monitoring box
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- 238000012806 monitoring device Methods 0.000 title claims abstract description 21
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 13
- 238000012544 monitoring process Methods 0.000 claims abstract description 69
- 229920001971 elastomer Polymers 0.000 claims abstract description 14
- 238000007789 sealing Methods 0.000 claims description 17
- 206010020649 Hyperkeratosis Diseases 0.000 claims description 9
- 230000006978 adaptation Effects 0.000 claims description 3
- 125000004122 cyclic group Chemical group 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 10
- 239000000428 dust Substances 0.000 abstract description 5
- 230000000694 effects Effects 0.000 abstract description 4
- 239000008187 granular material Substances 0.000 abstract 1
- 239000002245 particle Substances 0.000 description 3
- 229920000459 Nitrile rubber Polymers 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000741 silica gel Substances 0.000 description 1
- 229910002027 silica gel Inorganic materials 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
- 239000005341 toughened glass Substances 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- 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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/181—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a plurality of remote sources
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicle monitoring, in particular to a land, water and air triphibian unmanned aerial vehicle monitoring device which comprises an unmanned aerial vehicle main body, wherein a chute is formed in the lower surface of the unmanned aerial vehicle main body, a connecting plate is arranged on the upper surface of a monitoring box, which corresponds to the chute, a baffle is arranged at the end part of the chute, a storage bin is formed in the monitoring box, transparent plates are embedded on the side walls of the monitoring box, a mounting plate is arranged at the bottom of the storage bin, and a monitoring camera is arranged on the upper surface of the mounting plate; this triphibian type unmanned aerial vehicle monitoring devices of land, water and air has the monitoring box of connecting plate through setting up, can with the quick cooperation of pegging graft of spout in the unmanned aerial vehicle main part, and carry out the rigidity through first gim peg under the baffle effect, inlay on monitoring box outer wall and establish a plurality of transparent plates, a plurality of surveillance cameras of installation can realize multi-direction monitoring operation on the mounting panel, sealed lid can increase the leakproofness of monitoring box under the cooperation of rubber pad, reduce external dust granule and water droplet entering monitoring incasement portion, reduce inside damage.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle monitoring, in particular to a water-land-air triphibian unmanned aerial vehicle monitoring device.
Background
The unmanned aerial vehicle can be divided into military use and civil use according to the application field, and is really just needed by the unmanned aerial vehicle in the civil aspect. Unmanned aerial vehicle is as a flight carrier, and different people can take it to do different things.
The invention patent with the publication number of CN215155743U discloses an unmanned aerial vehicle monitoring device, which comprises an unmanned aerial vehicle body and a carrying assembly, wherein the lower surface of the unmanned aerial vehicle body is fixedly connected with a mounting plate, a sliding groove is formed in the mounting plate, the inner wall of the sliding groove is slidably connected with a positioning block, an electric telescopic rod for driving the positioning block to slide is arranged in the mounting plate, the lower surface of the mounting plate is fixedly connected with a buffer strip, the upper surface of the mounting plate is provided with a through hole, the carrying assembly comprises a connecting column inserted into the through hole, the top end of the connecting column is fixedly connected with a transmitter, and the bottom end of the connecting column is fixedly connected with a load-bearing platform;
although the connecting column can be separated from the unmanned aerial vehicle body by arranging the connecting column, the positioning block and the butt-joint camera, the flying suspended unmanned aerial vehicle can be automatically and accurately clamped with the connecting column by taking a video shot by the butt-joint camera as a reference, so that the effects of automatic separation and connection are realized; but the monitoring devices of installation on this unmanned aerial vehicle, it is not stable enough, dustproof and waterproof seals the effect poor, and monitoring direction is single, can not the multi-angle monitor the record comprehensively, and whole and unmanned aerial vehicle aggregate erection is convenient not enough, is not convenient for carry out quick dismantlement and changes the operation.
Disclosure of Invention
The invention aims to provide a water, land and air triphibian unmanned aerial vehicle monitoring device to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme:
the utility model provides a triphibian type unmanned aerial vehicle monitoring devices in land, water and air, includes the unmanned aerial vehicle main part, the spout has been seted up to unmanned aerial vehicle main part lower surface, the spout below is equipped with the monitoring case, monitoring case upper surface is equipped with the connecting plate with the spout department of correspondence, be equipped with the baffle on the spout tip, the inside storage storehouse of having seted up of monitoring case, the terminal surface is equipped with the opening before the monitoring case, is equipped with sealed lid at the opening part, all inlay on the monitoring case lateral wall and be equipped with the transparent plate, storage storehouse bottom is equipped with the mounting panel, the mounting panel upper surface all is equipped with the surveillance camera head with the transparent plate department of correspondence.
As a preferred technical scheme of the invention, the positions, close to the bottoms of the propeller blades, of the unmanned aerial vehicle main body are provided with supporting columns.
According to a preferable technical scheme, the top of the support column is fixedly connected with the unmanned aerial vehicle main body through screws, foot pads are arranged at the bottoms of the support columns, the foot pads are sleeved on the support columns, and the foot pads are fixedly bonded with the support columns.
As a preferred technical scheme of the invention, the connecting plate and the monitoring box are of an integrally formed structure, and the width of the outer wall of the connecting plate is matched with the width of the inner wall of the sliding chute.
As a preferred technical scheme of the invention, the baffle is arc-shaped, the baffle is in insertion fit with the chute, and the width of the baffle is matched with the width at the port of the chute.
As a preferable technical scheme of the invention, the baffle plate is provided with a connecting hole, a first fixing bolt is arranged in the connecting hole, and a first threaded hole is formed in the position, corresponding to the connecting hole, of the bottom of the unmanned aerial vehicle main body.
As a preferable technical scheme of the invention, the transparent plates are distributed at equal intervals in a ring shape and are fixedly bonded with the monitoring box.
According to a preferable technical scheme, the width of the outer wall of the sealing cover is matched with the width of the front end face of the monitoring box, the rear end face of the sealing cover is provided with a rubber pad, the rubber pad is fixedly bonded with the sealing cover, and the width of the outer wall of the rubber pad is matched with the width of the inner wall of the storage bin.
According to a preferable technical scheme of the invention, through holes are formed in the sealing cover close to four corners, second fixing bolts are arranged in the through holes, and second threaded holes are formed in the front end face of the monitoring box and correspond to the through holes.
As a preferred technical scheme of the invention, the width of the outer wall of the mounting plate is matched with the width of the bottom of the storage bin, a handle is further arranged on the upper surface of the mounting plate close to the front end, the monitoring camera is fixedly connected with the mounting plate through screws, an air bag ring is further arranged on the lower surface of the monitoring box, the air bag ring is annular, and the air bag ring is fixedly bonded with the monitoring box.
Compared with the prior art, the invention has the beneficial effects that:
1. according to the invention, the monitoring box with the connecting plate is arranged, can be rapidly inserted and matched with the chute on the unmanned aerial vehicle main body, is fixed in position through the first fixing bolt under the action of the baffle plate, the plurality of transparent plates are embedded on the outer wall of the monitoring box, the plurality of monitoring cameras are arranged on the mounting plate, so that the multi-directional monitoring operation can be realized, the sealing cover can increase the sealing property of the monitoring box under the matching of the rubber pad, the phenomenon that external dust particles and water drops enter the monitoring box is reduced, and the internal damage is reduced.
2. According to the unmanned aerial vehicle, the support columns and the foot pads are arranged to increase the independent stability of the main body of the unmanned aerial vehicle, the sealing cover is matched with the second fixing bolt, manual combination and installation are facilitated, the air bag ring is installed at the bottom of the monitoring box, the impact force possibly suffered during landing is reduced, and the damage possibly suffered in the interior is reduced.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic overall bottom view of the present invention;
fig. 3 is a schematic structural diagram of a main frame of the unmanned aerial vehicle of the present invention;
FIG. 4 is a schematic view of the combination structure of the monitoring box and the sealing cover of the present invention;
FIG. 5 is a schematic view of a combination structure of the monitoring box and the mounting plate of the present invention.
The various reference numbers in the figures mean:
1. an unmanned aerial vehicle main body; 10. a chute; 11. a first threaded hole;
2. a support column; 20. a foot pad;
3. a monitoring box; 30. a connecting plate; 31. a transparent plate; 32. a second threaded hole; 33. mounting a plate; 330. a handle; 331. a surveillance camera; 34. a storage bin;
4. a baffle plate; 40. connecting holes; 41. a first securing latch;
5. a sealing cover; 50. perforating; 51. a second securing latch; 52. a rubber pad;
6. an air bag ring.
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. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations or positional relationships based on those shown in the drawings, merely for convenience of description and simplification of the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a number" means at least two, e.g., two, three, etc., unless specifically limited otherwise.
Referring to fig. 1-5, the present embodiment provides a technical solution:
the utility model provides a triphibian type unmanned aerial vehicle monitoring devices in land, water and air, including unmanned aerial vehicle main part 1, spout 10 has been seted up to 1 lower surface of unmanned aerial vehicle main part, spout 10 below is equipped with monitoring box 3, 3 upper surfaces of monitoring box are equipped with connecting plate 30 with spout 10 department of correspondence, be equipped with baffle 4 on the 10 tip of spout, 3 inside storage storehouse 34 of having seted up of monitoring box, the terminal surface is equipped with the opening before the monitoring box 3, be equipped with sealed lid 5 at the opening part, it is equipped with transparent plate 31 all to inlay on 3 lateral walls of monitoring box, 34 bottoms in storage storehouse are equipped with mounting panel 33, the mounting panel 33 upper surface all is equipped with surveillance camera 331 with the transparent plate 31 department of correspondence.
In this embodiment, all be equipped with support column 2 on the unmanned aerial vehicle main part 1 near propeller blade bottom position department, the installation of support column 2 increases holistic independent stability, and the principle of unmanned aerial vehicle main part 1 is as known by technical personnel in the field, and the switch-on external power realizes corresponding taking off or descending.
Further, 2 tops of support column and unmanned aerial vehicle main part 1 pass through screw fixed connection, 2 bottoms of support column all are equipped with callus on the sole 20, and callus on the sole 20 all overlaps and establish on support column 2, and callus on the sole 20 bonds fixedly with support column 2, and callus on the sole 20 adopts the hydrogenated nitrile rubber preparation, and anticorrosive, anti tearing and resistance to compression deformation, the installation of callus on the sole 20 increases the frictional force of support column 2 and contact surface, increases the stability of structure.
Specifically, connecting plate 30 and monitoring case 3 are integrated into one piece structure, and the width of connecting plate 30 outer wall and the width looks adaptation of spout 10 inner wall are under the cooperation of connecting plate 30, and the stable quick grafting installation of monitoring case 3 and spout 10 of being convenient for.
It should be noted that the baffle 4 is arc-shaped, the baffle 4 is matched with the chute 10 in an inserting manner, the width of the baffle 4 is matched with the width at the port of the chute 10, and the installation of the baffle 4 increases the stability of the inserting installation of the connecting plate 30.
Secondly, seted up connecting hole 40 on baffle 4, be equipped with first gim peg 41 in the connecting hole 40, first screw hole 11 has been seted up with connecting hole 40 department of corresponding in the 1 bottom of unmanned aerial vehicle main part, and first gim peg 41 passes connecting hole 40 to with 11 threaded connection of first screw hole, realize baffle 4 fixed mounting.
Further, the transparent plate 31 is the equidistant distribution of annular, and transparent plate 31 and monitoring case 3 bonding are fixed, and transparent plate 31 adopts toughened glass preparation, and the monitoring camera 331 of being convenient for sees through transparent plate 31 and monitors external environment and change the situation.
It is worth supplementing, the width of the outer wall of the sealing cover 5 is matched with the width of the front end face of the monitoring box 3, the rubber pad 52 is arranged on the rear end face of the sealing cover 5, the rubber pad 52 is fixedly bonded with the sealing cover 5, the width of the outer wall of the rubber pad 52 is matched with the width of the inner wall of the storage bin 34, the rubber pad 52 is made of silica gel, the sealing performance between the sealing cover 5 and the monitoring box 3 is improved, dust particles and water drops in the external environment are reduced, the internal elements are damaged due to the fact that the dust particles and the water drops enter the inside, and the monitoring effect is influenced.
Secondly, all seted up perforation 50 near four corners on the sealed lid 5, all be equipped with second gim peg 51 in the perforation 50, all seted up second screw hole 32 with perforation 50 department of correspondence on the terminal surface before the monitoring case 3, second gim peg 51 passes perforation 50 to with second screw hole 32 threaded connection, realize sealed lid 5 and monitoring case 3 fast assembly installation.
In addition, the width of the outer wall of the mounting plate 33 is matched with the width of the bottom of the storage bin 34, a handle 330 is further arranged on the upper surface of the mounting plate 33 close to the front end, the monitoring camera 331 is fixedly connected with the mounting plate 33 through screws, an air bag ring 6 is further arranged on the lower surface of the monitoring box 3, the air bag ring 6 is annular, the air bag ring 6 is fixedly bonded with the monitoring box 3, the handle 330 is fixedly connected with the mounting plate 33 through screws, the mounting plate 33 can be pushed and pulled manually for use, the impact force during landing is realized under the matching of the air bag ring 6, the damage to internal elements is reduced, and the principle of the monitoring camera 331 is as known by those skilled in the art, and is electrically connected with an internal processor through a wire to monitor and match the external environment in real time.
The triphibian type unmanned aerial vehicle monitoring devices of this embodiment is when using, the user is manual installs transparent plate 31 on monitoring box 3, then will have the mounting panel 33 of surveillance camera 331 and the cooperation of pegging graft of storage storehouse 34 in the monitoring box 3, will have sealed lid 5 of rubber pad 52 to fix on monitoring box 3 through second gim peg 51 again, manual with monitoring box 3 through connecting plate 30 and spout 10 cooperation of pegging graft, baffle 4 and the cooperation of pegging graft of spout 10 tip, and fix its position through first gim peg 41, it is fixed with monitoring box 3 bonding with gasbag circle 6 at last, support column 2 and the unmanned aerial vehicle main part 1 fixed connection with callus on the sole 20, when needing to be changed monitoring box 3, manual dismantlement baffle 4, help quick replacement monitoring box 3, the convenient laborsaving of integral assembly installation, and to monitoring box 3 internal protection stability, reduce the influence of external water droplet and dust to inside.
The foregoing shows and describes the general principles, principal features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (10)
1. The utility model provides a triphibian unmanned aerial vehicle monitoring devices of land, water and air, includes unmanned aerial vehicle main part (1), its characterized in that: spout (10) have been seted up to unmanned aerial vehicle main part (1) lower surface, spout (10) below is equipped with monitoring box (3), monitoring box (3) upper surface corresponds department with spout (10) and is equipped with connecting plate (30), be equipped with baffle (4) on spout (10) tip, monitoring box (3) inside has been seted up and has been stored storehouse (34), the terminal surface is equipped with the opening before monitoring box (3), is equipped with sealed lid (5) at the opening part, all inlay on monitoring box (3) lateral wall and be equipped with transparent plate (31), store storehouse (34) bottom is equipped with mounting panel (33), mounting panel (33) upper surface all is equipped with surveillance camera head (331) with transparent plate (31) department of corresponding.
2. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: and the positions, close to the bottom of the propeller blades, of the unmanned aerial vehicle main body (1) are provided with support columns (2).
3. The triphibian unmanned aerial vehicle monitoring device of claim 2, wherein: support column (2) top passes through screw fixed connection with unmanned aerial vehicle main part (1), support column (2) bottom all is equipped with callus on the sole (20), callus on the sole (20) all the cover is established on support column (2), just callus on the sole (20) are fixed with support column (2) bonding.
4. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: the connecting plate (30) and the monitoring box (3) are of an integrally formed structure, and the width of the outer wall of the connecting plate (30) is matched with the width of the inner wall of the sliding groove (10).
5. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: baffle (4) are circular-arcly, just baffle (4) and spout (10) cooperation of pegging graft, the width of baffle (4) and the width looks adaptation of spout (10) port department.
6. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: connecting hole (40) have been seted up on baffle (4), be equipped with first gim peg (41) in connecting hole (40), first screw hole (11) have been seted up with connecting hole (40) correspondence department in unmanned aerial vehicle main part (1) bottom.
7. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: the transparent plate (31) is distributed in an annular shape at equal intervals, and the transparent plate (31) is fixedly bonded with the monitoring box (3).
8. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: the width of the outer wall of the sealing cover (5) is matched with the width of the front end face of the monitoring box (3), a rubber pad (52) is arranged on the rear end face of the sealing cover (5), the rubber pad (52) is fixedly bonded with the sealing cover (5), and the width of the outer wall of the rubber pad (52) is matched with the width of the inner wall of the storage bin (34).
9. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: sealed lid (5) are gone up and are all seted up perforation (50) near four corners, all be equipped with second gim peg (51) in perforation (50), second screw hole (32) have all been seted up with perforation (50) department of corresponding on the terminal surface before monitoring box (3).
10. The triphibian unmanned aerial vehicle monitoring device of claim 1, wherein: the width of mounting panel (33) outer wall and the width looks adaptation of storage storehouse (34) bottom, mounting panel (33) upper surface is close to front end department and still is equipped with handle (330), surveillance camera head (331) are through screw and mounting panel (33) fixed connection, surveillance case (3) lower surface still is equipped with gasbag circle (6), gasbag circle (6) are cyclic annularly, just gasbag circle (6) are fixed with surveillance case (3) bonding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210958195.5A CN115285367A (en) | 2022-08-11 | 2022-08-11 | Triphibian unmanned aerial vehicle monitoring devices of land, water and air |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210958195.5A CN115285367A (en) | 2022-08-11 | 2022-08-11 | Triphibian unmanned aerial vehicle monitoring devices of land, water and air |
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| CN115285367A true CN115285367A (en) | 2022-11-04 |
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| CN202210958195.5A Pending CN115285367A (en) | 2022-08-11 | 2022-08-11 | Triphibian unmanned aerial vehicle monitoring devices of land, water and air |
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| CN215245581U (en) * | 2021-04-06 | 2021-12-21 | 国核电力规划设计研究院有限公司 | Photovoltaic board dust detection device based on many rotor unmanned aerial vehicle |
| CN215475797U (en) * | 2021-07-26 | 2022-01-11 | 海南中农航服科技有限公司 | Unmanned aerial vehicle that takes photo by plane of many cameras |
| CN216140182U (en) * | 2021-08-31 | 2022-03-29 | 云南顺时空间科技有限公司 | Unmanned aerial vehicle aerial survey system |
| CN216509045U (en) * | 2022-01-26 | 2022-05-13 | 山东拓普地理信息工程有限公司 | Can improve unmanned aerial vehicle mapping device of survey and drawing influence stability |
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2022
- 2022-08-11 CN CN202210958195.5A patent/CN115285367A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US20140312165A1 (en) * | 2013-03-15 | 2014-10-23 | Armen Mkrtchyan | Methods, apparatus and systems for aerial assessment of ground surfaces |
| US20160355257A1 (en) * | 2015-06-05 | 2016-12-08 | Dana R. CHAPPELL | Unmanned aerial rescue system |
| CN109178305A (en) * | 2018-09-11 | 2019-01-11 | 武汉云衡智能科技有限公司 | A kind of amphibious unmanned plane of hydrologic monitoring and hydrologic monitoring method |
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| CN216509045U (en) * | 2022-01-26 | 2022-05-13 | 山东拓普地理信息工程有限公司 | Can improve unmanned aerial vehicle mapping device of survey and drawing influence stability |
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