CN207631492U - Unmanned vehicle - Google Patents
Unmanned vehicle Download PDFInfo
- Publication number
- CN207631492U CN207631492U CN201721588509.8U CN201721588509U CN207631492U CN 207631492 U CN207631492 U CN 207631492U CN 201721588509 U CN201721588509 U CN 201721588509U CN 207631492 U CN207631492 U CN 207631492U
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- unmanned vehicle
- horn
- spindle motor
- fuselage
- shell
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 20
- 238000013016 damping Methods 0.000 claims description 9
- 230000000712 assembly Effects 0.000 claims description 5
- 238000000429 assembly Methods 0.000 claims description 5
- 238000005516 engineering process Methods 0.000 description 3
- 230000003190 augmentative effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The utility model is related to unmanned vehicle technical fields, provide a kind of unmanned vehicle, including：One end of fuselage, horn, power plant and camera assembly, the horn is installed on the fuselage；The power plant is installed on the other end of the horn far from fuselage, the power for providing the unmanned vehicle flight；The camera assembly is installed on the other end of the horn far from the fuselage, for shooting image.In the above manner, the camera in the camera assembly can be blocked to avoid by undercarriage, propeller and unmanned vehicle horn, so that the unmanned vehicle can carry out pan-shot.
Description
【Technical field】
The utility model is related to unmanned vehicle technical field more particularly to a kind of unmanned vehicles.
【Background technology】
Unmanned vehicle (UAV) is a kind of new concept equipment being in rapidly developing, with maneuverability, reaction
Quickly, unmanned, operation requires low advantage.Unmanned vehicle is by carrying multiclass sensor or picture pick-up device, Ke Yishi
Existing image real-time Transmission, high-risk areas detecting function are the strong supplements of satellite remote sensing and traditional air remote sensing.Currently, nobody
The use scope of aircraft has widened military affairs, scientific research, civilian three big field, specifically in power communication, meteorology, agricultural, sea
Ocean, he explores, photographs, preventing and reducing natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the fields application such as public security anti-terrorism it is very wide.
Current augmented reality (Augmented Rea l ity, AR) and virtual reality (Vi rtua l Rea l ity,
VR) technology development is swift and violent, also higher and higher for the demand of panoramic video shooting, is taken photo by plane using unmanned vehicle, is
Obtain a kind of important way of the panoramic picture of real scene.And in order to accurately obtain the image of multiple angles, work as utilization
When unmanned vehicle carries out panoramic shooting, unmanned vehicle camera mounted needs to avoid undercarriage, propeller and nothing
People's aircraft horn blocks.
In the process of implementing the utility model, the inventor finds that the existing technology has at least the following problems：Existing
In unmanned vehicle, camera is hung on by holder below the fuselage of unmanned vehicle；Due to the camera shooting at the position
Head is blocked by undercarriage, propeller and unmanned vehicle horn, can not carry out panoramic shooting.
【Utility model content】
In order to solve the above-mentioned technical problem, the utility model embodiment provide it is a kind of can realize panoramic shooting nobody fly
Row device.
In order to solve the above technical problems, the utility model embodiment provides following technical scheme：
A kind of unmanned vehicle, including：One end of fuselage, horn, power plant and camera assembly, the horn is installed on
The fuselage；The power plant is installed on the other end of the horn far from the fuselage, for providing the unmanned flight
The power of device flight；The camera assembly is installed on the other end of the horn far from the fuselage, for shooting image.
In some embodiments, the camera assembly is installed on the farthest that the fuselage is away from the horn, and
And the camera assembly is located at side of the power plant far from the fuselage.
In some embodiments, the camera assembly includes holder and photographic device, and the holder carries the camera shooting dress
It sets, the holder is installed on the farthest far from the fuselage on the horn.
In some embodiments, the holder includes：Holder, pitching spindle motor and roll spindle motor, the holder include
Pedestal and two linking arms, the other end face that the pedestal is away from the fuselage with the horn are fixedly connected, two institutes
The one end for stating linking arm is fixedly connected with the pedestal, and the pitching spindle motor is installed on the linking arm far from the pedestal
The other end；The roll spindle motor is rotatablely connected with the pitching spindle motor.
In some embodiments, the pitching spindle motor is installed on one of them described linking arm far from the another of the pedestal
One end；The photographic device includes shell and camera lens module, and the shell is connect with the pitching spindle motor, and with described in two
The other end of another in linking arm is hinged, and the pitching spindle motor is for driving the shell around pitch axes；The cross
Roller motor is installed in the shell, and is connect with the camera lens module, and the roll spindle motor is for driving the camera lens
Module is dynamic around roll shaft rotation relative to the shell.
In some embodiments, the holder includes two pitching spindle motors, each pitching spindle motor installation
In a corresponding other end of the linking arm far from the pedestal；The photographic device includes shell and camera lens module, institute
It states shell to connect with two pitching spindle motors, the pitching spindle motor is for driving the shell around pitch axes；Institute
It states roll spindle motor to be installed in the shell, and is connect with the camera lens module, the roll spindle motor is described for driving
Camera lens module is dynamic around roll shaft rotation relative to the shell.
In some embodiments, the junction of the camera assembly and the horn is provided with damping device, the damping
Device includes the first connecting plate, shock-absorbing ball and the second connecting plate, and the shock-absorbing ball is set to first connecting plate and second and connects
Between fishplate bar；First connecting plate is fixedly connected with the horn, and second connecting plate is fixedly connected with the holder.
In some embodiments, the camera assembly includes photographic device, the photographic device and the horn
Junction is provided with damping device.
In some embodiments, the unmanned vehicle be quadrotor unmanned vehicle, the horn altogether there are four, it is described
There are four camera assembly is total, the camera assembly is corresponded with the horn；The line of four camera assemblies constitutes one
Rectangle.
In some embodiments, one end of four horns is fixedly connected with the fuselage, and adjacent two
Horn is mutually perpendicular to.
Compared with prior art, a kind of unmanned vehicle of the utility model embodiment, including：Fuselage, horn, power
One end of device and camera assembly, the horn is installed on the fuselage；The power plant is installed on the horn far from institute
The other end for stating fuselage, the power for providing the unmanned vehicle flight；It is remote that the camera assembly is installed on the horn
The other end from the fuselage, for shooting image.In the above manner, camera in the camera assembly can to avoid by
To blocking for undercarriage, propeller and unmanned vehicle horn, so that the unmanned vehicle can carry out pan-shot.
【Description of the drawings】
One or more embodiments are illustrated by the picture in corresponding attached drawing, these exemplary theorys
The bright restriction not constituted to embodiment, the element with same reference numbers label is expressed as similar element in attached drawing, removes
Non- to have special statement, composition does not limit the figure in attached drawing.
Fig. 1 is a kind of structural schematic diagram for unmanned vehicle that one embodiment of the utility model provides；
Fig. 2 is the structural schematic diagram of camera assembly in unmanned vehicle shown in FIG. 1；
Fig. 3 is the exploded view of photographic device and roll spindle motor in camera assembly shown in Fig. 2；
Fig. 4 is the upward view of unmanned vehicle shown in FIG. 1.
【Specific implementation mode】
For the ease of understanding the utility model, in the following with reference to the drawings and specific embodiments, the utility model is carried out more detailed
Thin explanation.It should be noted that when element is expressed " being fixed on " another element, it can be directly in another element
Upper or placed in the middle there may be one or more therebetween elements.When an element is expressed " electrical connection " another element, it
It can be directly to another element or may exist one or more elements placed in the middle therebetween.This specification is made
The orientation or positional relationship of the instructions such as term "upper", "lower", "inner", "outside", " bottom " is orientation based on ... shown in the drawings
Or position relationship, be merely for convenience of describing the present invention and simplifying the description, do not indicate or imply the indicated device or
Element must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as the limit to the utility model
System.In addition, term " first ", " second " " third " etc. are used for description purposes only, it is not understood to indicate or imply relatively heavy
The property wanted.
Unless otherwise defined, technical and scientific term all used in this specification and the skill for belonging to the utility model
The normally understood meaning of technical staff in art field is identical.Term used in the description of the utility model is intended merely to
The purpose for describing specific embodiment is not intended to limitation the utility model.Term "and/or" used in this specification includes
Any and all combinations of one or more relevant Listed Items.
In addition, as long as technical characteristic involved in the utility model difference embodiment disclosed below is each other not
Constituting conflict can be combined with each other.
As shown in Figure 1, a kind of unmanned vehicle 100 that the utility model wherein embodiment provides, including：Fuselage 10,
One end of horn 20, power plant 30 and camera assembly 40, the horn 20 is installed on the fuselage 10.The power plant 30
It is installed on the other end of the horn 20 far from the fuselage 10, the power for providing the flight of the unmanned vehicle 100.Institute
It states camera assembly 40 and is installed on the other end of the horn 20 far from the fuselage 10, for shooting image.Above-mentioned unmanned flight
Device 100 can be the unmanned vehicle that rotor unmanned aircraft, fixed-wing unmanned vehicle or fixed-wing are mixed with rotor.Its
In, rotor unmanned aircraft is concretely：Single rotor unmanned vehicle, DCB Specimen unmanned vehicle, three rotor unmanned aircrafts,
Quadrotor unmanned vehicle, six rotor unmanned aircrafts and eight rotor unmanned aircrafts etc..
In the present embodiment, by taking the unmanned vehicle 100 is quadrotor unmanned vehicle as an example, to the unmanned vehicle
100 concrete structure is described in detail.
Specifically, the number of the horn 20 is four, one end of four horns 20 is fixed with the fuselage 10
Connection.The fuselage 10 and horn 20 are substantially in " ten " font, that is, non-conterminous two horns 20 are located at same straight line
On, and two adjacent horns 20 are mutually perpendicular to.
Specifically, the number of the power plant 30 is four, it is separate that the power plant 30 is installed on the horn 20
The other end of the fuselage 10, the power for providing the flight of the unmanned vehicle 100.Four power plants 30 and four
A horn 20 corresponds.The power plant 30 includes motor and propeller, and the motor is fixed on the horn 20
The other end far from the fuselage 10, the motor are connect with the propeller, and the propeller is driven to rotate.
Specifically, as shown in Fig. 2, the camera assembly 40 includes holder 41 and photographic device 42, the holder 41 carries
The photographic device 42 (is taken the photograph with the fixation for realizing photographic device 42 or the posture for arbitrarily adjusting photographic device 42 for example, changing
As the height of device 42, inclination angle and/or direction) and photographic device 42 is made to be stably held in the posture of setting.The camera shooting
Device 42 can be specifically：Camera, video camera, camera etc..The holder 41 can be uniaxial holder, twin shaft holder or three axis clouds
Platform.
The camera assembly 40 and the junction of the horn 20 are provided with damping device (not shown), the damping
Device includes the first connecting plate (not shown), shock-absorbing ball and the second connecting plate (not shown), and the shock-absorbing ball is set to described the
Between one connecting plate and the second connecting plate.First connecting plate is fixedly connected with the horn 20, second connecting plate with
The holder 41 is fixedly connected.
It is understood that in some other embodiment, the camera assembly 40 does not include holder 41, the camera shooting dress
The horn 20 can be installed on by the damping device by setting 42.
In the present embodiment, there are four the camera assembly 40 is total to, the camera assembly 40 is a pair of with the horn 20 1
It answers.It is understood that in some other embodiment, the number of the camera assembly 40 can also be five or five with
On, wherein four camera assemblies 40 are corresponded with the horn 20, remaining camera assembly 40 can be according to the demand of actual conditions
And it is set to any position of unmanned vehicle 100.
As shown in Figures 2 and 3, in the present embodiment, the holder 41 is twin shaft holder.The holder 41 includes：Holder
411, pitching spindle motor 412 and roll spindle motor 413.The holder 411 is substantially U-shaped, including pedestal 4111 and two connections
One end of arm 4112, two linking arms 4112 is fixedly connected with the pedestal 4111, and the pitching spindle motor 412 only has
One, it is installed on the other end of one of them in two linking arms 4112.The roll spindle motor 413 and the pitching
Spindle motor 412 is rotatablely connected.
It is understood that in some other embodiment, the holder 41 includes two pitching spindle motors 412,
Each pitching spindle motor 412 is installed on the other end of a corresponding linking arm 4112.
The photographic device 42 includes shell 421 and camera lens module 422, and the shell 421 is spherical, with the pitching
Spindle motor 412 connects, and hinged with another the other end in two linking arms 4112, and the pitching spindle motor 412 is used
In drive the shell 421 around pitch axes.The roll spindle motor 413 is installed in the shell 421, and with the mirror
Head mould group 422 connects, and the roll spindle motor 413 is for driving the camera lens module 422 relative to the shell 421 around roll
Shaft rotation is dynamic.
As shown in figure 4, in the present embodiment, the line of four camera lens modules 422 constitutes an a rectangle (camera lens mould
Group 422 only with two adjacent 422 lines of camera lens module).Two camera lens moulds being located on two non-conterminous horns 20
The optical axis of group 422 is always positioned in same plane.The optical axis of two adjacent camera lens modules 422 is always positioned at orthogonal two
In a plane.Four camera lens modules 422 can cooperate and cooperate, to take around unmanned vehicle 100 360 degree
Panoramic picture.
The camera assembly 40 is set to the other end of the horn 20, may make camera assembly 40 that can preferably avoid
Undercarriage, propeller, horn and fuselage block so that camera assembly 40 can obtain larger range of scenery or image.This
Outside, four camera assemblies 40 can also jointly shoot same target, due to camera lens module 422 in four camera assemblies 40
Shooting angle it is different, therefore the image that four camera lens modules 422 shoot same target can be used for quickly carrying out above-mentioned target
3D modeling and/or drafting relief map etc..Based on above structure feature, may make the unmanned vehicle 100 engineering survey,
The fields such as mapping and disaster emergency rescue play a significant role.
Specifically, the pedestal 4111 of end face of the horn 20 far from 10 one end of the fuselage and the holder 41 is fixed and is connected
It connects.The camera assembly 40 is installed on the farthest that fuselage 10 is away from the horn 20, at this time the camera assembly 40
In side of the power plant 30 far from the fuselage 10.Photographic device 42 in the camera assembly 40 can to avoid by
Undercarriage (being usually mounted to the underface of the fuselage, farther out apart from camera assembly), propeller and unmanned vehicle machine
Arm blocks, so that the unmanned vehicle 100 can carry out pan-shot (that is, the photographic device 42 can be in all directions
Take 100 oblique upper of the unmanned vehicle, above and below scene).
Finally it should be noted that：Above example is only to illustrate the technical solution of the utility model, rather than its limitations；
Under the thinking of the utility model, it can also be combined between the technical characteristic in above example or different embodiments,
Step can be realized with random order, and there are many other variations of the different aspect of the utility model as described above, be
Simplicity, they do not provide in details；Although the utility model is described in detail with reference to the foregoing embodiments, this
The those of ordinary skill in field should understand that：Its still can with technical scheme described in the above embodiments is modified,
Or equivalent replacement of some of the technical features；And these modifications or replacements, do not make the sheet of corresponding technical solution
Matter is detached from the range of various embodiments of the utility model technical solution.
Claims (10)
1. a kind of unmanned vehicle (100), which is characterized in that including：It fuselage (10), horn (20), power plant (30) and takes the photograph
As component (40), one end of the horn (20) is installed on the fuselage (10)；The power plant (30) is installed on the machine
The other end of the arm (20) far from the fuselage (10), the power for providing the unmanned vehicle (100) flight；The camera shooting
Component (40) is installed on the other end of the horn (20) far from the fuselage (10), for shooting image.
2. unmanned vehicle (100) according to claim 1, which is characterized in that
The camera assembly (40) is installed on the farthest that the fuselage (10) are away from the horn (20), and described takes the photograph
As component (40) is located at side of the power plant (30) far from the fuselage (10).
3. unmanned vehicle (100) according to claim 2, which is characterized in that
The camera assembly (40) includes holder (41) and photographic device (42), and the holder (41) carries the photographic device
(42), the holder (41) is installed on the farthest that the fuselage (10) are away from the horn (20).
4. unmanned vehicle (100) according to claim 3, which is characterized in that
The holder (41) includes：Holder (411), pitching spindle motor (412) and roll spindle motor (413), the holder (411)
Including pedestal (4111) and two linking arms (4112), the pedestal (4111) is away from the fuselage with the horn (20)
(10) the other end face is fixedly connected, and one end of two linking arms (4112) is fixedly connected with the pedestal (4111),
The pitching spindle motor (412) is installed on the other end of the linking arm (4112) far from the pedestal (4111)；The roll
Spindle motor (413) is rotatablely connected with the pitching spindle motor (412).
5. unmanned vehicle (100) according to claim 4, which is characterized in that
It is another far from the pedestal (4111) that the pitching spindle motor (412) is installed on one of them described linking arm (4112)
End；
The photographic device (42) includes shell (421) and camera lens module (422), and the shell (421) is electric with the pitch axis
Machine (412) connects, and hinged with another the other end in two linking arms (4112), the pitching spindle motor (412)
For driving the shell (421) around pitch axes；The roll spindle motor (413) is installed in the shell (421), and
It is connect with the camera lens module (422), the roll spindle motor (413) is for driving the camera lens module (422) relative to institute
It is dynamic around roll shaft rotation to state shell (421).
6. unmanned vehicle (100) according to claim 4, which is characterized in that
The holder (41) includes two pitching spindle motors (412), and each pitching spindle motor (412) is installed on one
The other end of the corresponding linking arm (4112) far from the pedestal (4111)；
The photographic device (42) includes shell (421) and camera lens module (422), the shell (421) and two pitching
Spindle motor (412) connects, and the pitching spindle motor (412) is for driving the shell (421) around pitch axes；The roll
Spindle motor (413) is installed in the shell (421), and is connect with the camera lens module (422), the roll spindle motor
(413) it is used to drive the camera lens module (422) dynamic around roll shaft rotation relative to the shell (421).
7. unmanned vehicle (100) according to claim 3, which is characterized in that
The junction of the camera assembly (40) and the horn (20) is provided with damping device, and the damping device includes first
Connecting plate, shock-absorbing ball and the second connecting plate, the shock-absorbing ball are set between first connecting plate and the second connecting plate；It is described
First connecting plate is fixedly connected with the horn (20), and second connecting plate is fixedly connected with the holder (41).
8. unmanned vehicle (100) according to claim 2, which is characterized in that
The camera assembly (40) includes photographic device (42), and the photographic device (42) and the junction of the horn (20) are set
It is equipped with damping device.
9. according to claim 1 to 8 any one of them unmanned vehicle (100), which is characterized in that
The unmanned vehicle (100) be quadrotor unmanned vehicle, the horn (20) altogether there are four, the camera assembly
(40) there are four altogether, the camera assembly (40) corresponds with the horn (20)；
The line of four camera assemblies (40) constitutes a rectangle.
10. unmanned vehicle (100) according to claim 9, which is characterized in that
One end of four horns (20) is fixedly connected with the fuselage (10), and two adjacent horns (20) are mutual
Vertically.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721588509.8U CN207631492U (en) | 2017-11-22 | 2017-11-22 | Unmanned vehicle |
| PCT/CN2018/106074 WO2019100825A1 (en) | 2017-11-22 | 2018-09-18 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721588509.8U CN207631492U (en) | 2017-11-22 | 2017-11-22 | Unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207631492U true CN207631492U (en) | 2018-07-20 |
Family
ID=62858098
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721588509.8U Active CN207631492U (en) | 2017-11-22 | 2017-11-22 | Unmanned vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN207631492U (en) |
| WO (1) | WO2019100825A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019100825A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2019100821A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN110375716A (en) * | 2019-07-23 | 2019-10-25 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle finds information generating method and unmanned vehicle |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106489266B (en) * | 2014-04-14 | 2019-10-11 | 瓦斯菲·阿希达法特 | Announcer unmanned aerial vehicle |
| CN205265789U (en) * | 2015-12-03 | 2016-05-25 | 广州极飞电子科技有限公司 | A panorama shooting device and unmanned aerial vehicle for unmanned aerial vehicle |
| CN206504072U (en) * | 2016-11-21 | 2017-09-19 | 天津中翔腾航科技股份有限公司 | A kind of varifocal infrared imaging head |
| CN106477028A (en) * | 2016-11-23 | 2017-03-08 | 北京小米移动软件有限公司 | Aircraft and its foot rest structure |
| CN207826581U (en) * | 2017-11-22 | 2018-09-07 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
| CN207631492U (en) * | 2017-11-22 | 2018-07-20 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
-
2017
- 2017-11-22 CN CN201721588509.8U patent/CN207631492U/en active Active
-
2018
- 2018-09-18 WO PCT/CN2018/106074 patent/WO2019100825A1/en active Application Filing
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019100825A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2019100821A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN110375716A (en) * | 2019-07-23 | 2019-10-25 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle finds information generating method and unmanned vehicle |
| CN110375716B (en) * | 2019-07-23 | 2022-01-14 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle searching information generation method and unmanned aerial vehicle |
| US11945583B2 (en) | 2019-07-23 | 2024-04-02 | Autel Robotics Co., Ltd. | Method for generating search information of unmanned aerial vehicle and unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019100825A1 (en) | 2019-05-31 |
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