CN207978026U - Lens assembly, damping module and the aircraft for installing lens assembly - Google Patents
Lens assembly, damping module and the aircraft for installing lens assembly Download PDFInfo
- Publication number
- CN207978026U CN207978026U CN201721370834.7U CN201721370834U CN207978026U CN 207978026 U CN207978026 U CN 207978026U CN 201721370834 U CN201721370834 U CN 201721370834U CN 207978026 U CN207978026 U CN 207978026U
- Authority
- CN
- China
- Prior art keywords
- shock
- camera lens
- lens
- absorbing
- lens assembly
- 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.)
- Active
Links
Landscapes
- Accessories Of Cameras (AREA)
Abstract
The utility model is related to a kind of lens assemblies, including：Camera lens；Connected with camera lens, for determine lens location and buffer camera lens vibrations damping module.The lens assembly, damping module is directly connected to camera lens and determines lens location, buffering camera lens vibrations, the device for using holder fixed lens component in traditional technology has been banned, has ensured camera lens steady shot while saving cost of the aircraft for taking photo by plane or providing virtual reality visual angle.
Description
Technical field
The utility model is related to lens assembly field, more particularly to used on a kind of aircraft lens assembly, damping
Module and the aircraft for installing lens assembly.
Background technology
With the development of micro-electromechanical technology, aircraft applications are more and more extensive.Aircraft can be used for taking photo by plane, provide virtually
The fields such as Realistic Visual Angle or the small quality article of transport.
It, will to make aircraft generally utilize cradle head device for taking photo by plane or providing virtual reality visual angle field, traditional technology
The holder for being fixed with taking lens is installed on aircraft, and taking lens is carried to achieve the purpose that aircraft is stablized.It is realizing
During traditional technology, it is found by the applicant that：
Cradle head device is at high price, will increase cost using cradle head device establishing shot camera lens.
Utility model content
Based on this, it is necessary to which the problem of increasing aircraft cost for cradle head device provides and use on a kind of aircraft
Lens assembly, damping module and the aircraft for installing lens assembly.
A kind of lens assembly, including：Camera lens；It is connected with camera lens, for determining lens location and buffering subtracting for camera lens vibrations
Shake module.
Above-mentioned lens assembly, damping module are directly connected to lens assembly, have banned holder fixed lens group in traditional technology
The device of part saves cost of the aircraft for taking photo by plane or providing virtual reality visual angle.
The lens assembly in one of the embodiments, further includes：Rotary drive；The rotary drive with
Camera lens connects, and for driving the rotation of lens.
The lens assembly in one of the embodiments, further includes：Component end；The component end passes through institute
It states damping module and connects the camera lens, and for determining the lens location；The rotary drive is fixed on the assembly end
Head.
The lens assembly, the damping module are made of more than two shock-absorbing arms in one of the embodiments,；
Described shock-absorbing arms one end connects the component end, and the shock-absorbing arms other end connects the camera lens.
The lens assembly in one of the embodiments, the shock-absorbing arms of the damping module is respectively from different spaces
Coordinate axially connects the camera lens and the component end, so that the camera lens realizes damping effect in various dimensions.
The lens assembly, the shock-absorbing arms include in one of the embodiments,：Shock-absorbing ball；The damping ball
It is flexible.
The lens assembly, the shock-absorbing arms further include in one of the embodiments,：Spring；The spring with subtract
Ball is shaken to be connected；Shock-absorbing arms is collectively formed with shock-absorbing ball in the spring.
One diameter of the lens assembly in one of the embodiments, the spring axis and shock-absorbing ball is same
On one straight line, so that shock-absorbing arms deforms upon in an axial direction when working.
A kind of damping module, it is matched with camera lens, for the vibrations to camera lens into row buffering, including：More than two skies
Between coordinate axial direction shock-absorbing arms.
Above-mentioned damping module is coupled with camera lens, includes the shock-absorbing arms of more than two space coordinate axial directions, make aircraft
It carries in camera lens flight course, camera lens vibrations can be reduced in different directions, be conducive to camera lens stabilization.
A kind of aircraft, which is characterized in that be equipped with lens assembly；The lens assembly includes：Camera lens；Connect with camera lens
Connect, for determine lens location and buffer camera lens vibrations damping module.
Above-mentioned aircraft, is equipped with including camera lens and for determining lens location and buffering the damping modules of camera lens vibrations,
So that aircraft, which carries when virtual reality visual angle is taken photo by plane or provided to camera lens, does not need cradle head device fixed lens, reduce winged
The cost of manufacture of row device；And the damping module of the aircraft can axially realize damping in multiple spaces, ensure aircraft work
The stability of camera lens in the process.
Description of the drawings
Fig. 1 is the sectional structure chart of lens assembly provided by the embodiments of the present application；
Fig. 2 is the side view of lens assembly provided by the embodiments of the present application.
Fig. 3 is the vertical view of lens assembly provided by the embodiments of the present application.
Fig. 4 is the upward view of lens assembly provided by the embodiments of the present application.
Wherein,
100 lens assemblies
110 component ends
120 camera lenses
130 steering engines
140 shock-absorbing arms
141 shock-absorbing balls
142 springs
Specific implementation mode
To keep the above objects, features, and advantages of the utility model more obvious and easy to understand, below in conjunction with the accompanying drawings to this
The specific implementation mode of utility model is described in detail.Elaborate many details in order to abundant in the following description
Understand the utility model.But the utility model can be much to implement different from other manner described here, this field
Technical staff can do similar improvement without prejudice to the utility model connotation, therefore the utility model is not by following public affairs
The limitation for the specific embodiment opened.
The embodiments of the present invention are described below in detail, examples of the embodiments are shown in the accompanying drawings, wherein from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining the present invention, and is not considered as limiting the invention.
In the description of the present invention, it is to be understood that, term " longitudinal direction ", " transverse direction ", "upper", "lower", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown, is merely for convenience of description of the present invention and simplification of the description, and does not indicate or imply the indicated dress
It sets or element must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as the limit to the present invention
System.
In the description of the present invention, unless otherwise specified and limited, it should be noted that term " installation ", " connected ",
" connection " shall be understood in a broad sense, for example, it may be mechanical connection or electrical connection, can also be the connection inside two elements, it can
, can also indirectly connected through an intermediary, for the ordinary skill in the art to be to be connected directly, it can basis
Concrete condition understands the concrete meaning of above-mentioned term.
As shown in Figure 1, a kind of lens assembly 100, including：Camera lens 120 and camera lens 120 connect, for determining camera lens 120
Position and the damping module for buffering the vibrations of camera lens 120.
Specifically, aforementioned camera lens 120 is generally positioned at aircraft, for taking photo by plane or providing the technologies such as virtual reality visual angle neck
Field.
Aforementioned damping module is made of more than two shock-absorbing arms 140.140 connection lens 120 of shock-absorbing arms, can be used for determining
Position of the camera lens 120 relative to aircraft.Shock-absorbing arms 140 has elasticity, can buffer camera lens 120 in the aircraft course of work and shake
It is dynamic.
More specifically, the connection relation of aforementioned camera lens 120 and aircraft is by being made of more than two shock-absorbing arms 140
Damping module composition.Multiple shock-absorbing arms 140 of aforementioned damping module are respectively from different spaces reference axis to connecting the camera lens
120, so that camera lens 120 can realize vibrations buffering in various dimensions in the aircraft course of work.
Above-mentioned lens assembly 100, damping module are directly connected to lens assembly 100, have banned holder in traditional technology and have fixed
The device of lens assembly 100 saves cost of the aircraft for taking photo by plane or providing virtual reality visual angle.
Further, aforementioned lens assembly 100 further includes：Component end 110.
Specifically, component end 110 is directly connected to aircraft.Damping module connection component end 110 and camera lens 120.Group
Part end 110 is by connecting damping module connection lens 120, and the position for determining camera lens 120 and damping module.
More specifically, component end 110 is directly fixedly connected on aircraft, damping module is by more than two shock-absorbing arms
140 are constituted.140 one end connection component end 110 of shock-absorbing arms, other end connection lens 120.By the connection of shock-absorbing arms 140, with
Determine position of the camera lens 120 relative to component end 110.
As shown in Figures 2 to 4, in one embodiment, lens assembly 100 above-mentioned further includes：Rotary drive.
Specifically, rotary drive is fixedly connected on component end 110, other end connection lens 120, for driving camera lens
120 rotations.
More specifically, rotary drive connection lens 120, and be fixed on component end 110, it is worked in for aircraft
Take photo by plane or provide rotating lens 120 during the field of virtual reality visual angle.
Further, in the preferred embodiment of the application, aforementioned rotary drive is steering engine 130.Steering engine 130 is used
Camera lens 120 is driven to rotate when aircraft works, to realize multi-angled shooting.
Further, in specific embodiment provided by the present application, in order to complete rotation of the steering engine 130 to camera lens 120
Control, aircraft should be provided with function module (not shown).Function module includes the work of control flaps machine 130 so that camera lens
120 rotations.
In one embodiment, aforementioned shock-absorbing arms 140 includes：Shock-absorbing ball 141.
Specifically, shock-absorbing arms 140 includes shock-absorbing ball 141, and shock-absorbing ball 141 has elasticity.Aircraft carries aforementioned lens group
When part 100 works, the shock-absorbing ball 141 of shock-absorbing arms 140 has the function of elasticity, it can be achieved that buffering camera lens 120 shakes.
In one embodiment, aforementioned shock-absorbing arms 140 further includes：Spring 142.
Specifically, shock-absorbing arms 140 further includes spring 142, and shock-absorbing arms 140 is collectively formed in spring 142 and shock-absorbing ball 141, with
Shock-absorbing arms 140 is set preferably to realize shock-absorbing function when camera lens 120 shakes.
More specifically, aforementioned shock-absorbing ball 141 and spring 142 are collectively formed shock-absorbing arms 140, and the axle center of spring 142 and subtract
Shake a diameter of ball 141 on the same line.140 one end connection lens 120 of shock-absorbing arms, other end connection component end 110,
When so that camera lens 120 shaking, the deformation of shock-absorbing arms 140 generates in an axial direction.
Optionally, the quantity of the aforementioned shock-absorbing ball 141 for constituting shock-absorbing arms 140 and spring 142 is unlimited, subtracts as long as it can meet
Shake function.
In the preferred embodiment of the application, shock-absorbing arms 140 is made of two springs 142 and a shock-absorbing ball 141.
On the same line, and two springs 142 respectively have one end and subtract for the axle center of two springs 142 and a diameter of shock-absorbing ball 141
It shakes ball 141 to be connected, to constitute shock-absorbing arms 140.In 140 course of work of shock-absorbing arms, spring 142 be not connected with shock-absorbing ball 141 two
One end connection component end 110, other end connection lens 120 is held to be shaken to reach 120 position of determining camera lens and buffer camera lens 120
Dynamic function.
Further, aforementioned shock-absorbing arms 140 can also be made of a shock-absorbing ball 141 and a damping spring 142.Spring
On the same line, 142 one end of spring connects shock-absorbing ball 141 for 142 axle center and a diameter of shock-absorbing ball 141.Spring 142 is not
One end connection component end 110 being connected with shock-absorbing ball 141.Shock-absorbing ball 141 and 142 axle center of spring are conllinear diametrically, do not connect
The endpoint connection lens 120 for connecing spring 142, to reach 120 position of determining camera lens and buffer the function of the vibrations of camera lens 120.
Further, the aforementioned shock-absorbing ball 141 and spring 142 for constituting shock-absorbing arms 140, meets its quantity and is more than or equal to
One can be realized shock-absorbing function.
A kind of damping module, it is matched with camera lens 120, for the vibrations to camera lens 120 into row buffering, including：Two with
On space coordinate axial direction shock-absorbing arms 140.
Specifically, damping module is coupled with camera lens 120, includes the shock-absorbing arms 140 of more than two space coordinates axial direction, can
For the vibrations to camera lens 120 into row buffering.Camera lens 120 may be implemented in the shock-absorbing arms 140 of more than two space coordinate axial directions
Vibrations buffering on various dimensions.
More specifically, aforementioned shock-absorbing arms 140 includes shock-absorbing ball 141 and spring 142.Constitute the damping of a shock-absorbing arms 140
On the same line, and spring 142 is connected with shock-absorbing ball 141 for one diameter of ball 141 and the axle center of spring 142.A plurality of damping
Arm 140 connection component end 110 and camera lens 120 in different coordinate axially directions, to realize various dimensions damping effect.
Further, the quantity of the aforementioned shock-absorbing ball 141 for constituting shock-absorbing arms 140 and spring 142 is not fixed, can be expired
Foot buffering 120 vibration function of camera lens.I.e. shock-absorbing ball 141 and 142 quantity of spring and be more than or equal to one.
Above-mentioned damping module is coupled with camera lens 120, includes the shock-absorbing arms 140 of more than two space coordinate axial directions, make
Aircraft carries in 120 flight course of camera lens, can reduce the vibrations of camera lens 120 in different directions, it is steady to be conducive to camera lens 120
It is fixed.
A kind of aircraft is equipped with lens assembly 100；Lens assembly 100 includes：Camera lens 120；It connects, uses with camera lens 120
In determine 120 position of camera lens and buffer camera lens 120 vibrations damping module.
Specifically, camera lens 120 is fixed on aircraft, for shooting.
Damping module is connect with camera lens 120 and aircraft, for determining 120 position of camera lens, and buffers the vibrations of camera lens 120.
Further, aforementioned aircraft further includes the component to match with the damping module of lens assembly 100, camera lens 120
End 110 and for drive camera lens 120 rotate rotary drive.
More specifically, component end 110 is fixed on aircraft.Damping module connects aircraft and camera lens 120.Rotation is driven
Moving part one end connects taking lens 120, and the other end is fixed on aircraft or component end 110, for driving camera lens 120 to revolve
Turn, realizes multi-angled shooting.
Still further, above-mentioned damping module, is coupled with camera lens 120, include that more than two space coordinates are axial
Shock-absorbing arms 140 makes aircraft carry in 120 flight course of camera lens, can reduce the vibrations of camera lens 120 in different directions, favorably
Stablize in camera lens 120.Aforementioned shock-absorbing arms 140 includes shock-absorbing ball 141 and spring 142.Constitute the shock-absorbing ball of a shock-absorbing arms 140
On the same line, and spring 142 is connected with shock-absorbing ball 141 for 141 diameter and the axle center of spring 142.A plurality of shock-absorbing arms
140 in different coordinate axially directions connection component end 110 and camera lens 120, to realize various dimensions damping effect.
In one specifically embodiment, above-mentioned lens assembly 100, including：Camera lens 120 is connected with camera lens 120, uses
In determine 120 position of camera lens and buffer camera lens 120 vibrations damping module.Damping module includes that eight different spaces coordinates are axial
Shock-absorbing arms 140.Each shock-absorbing arms 140 is made of two springs 142 and a shock-absorbing ball 141.Constitute every shock-absorbing arms 140
Two springs 142 and a shock-absorbing ball 141 are coaxially connected.Damping module is fastened on carry-on component end 110.Group
Connection lens 120, the rotary drive for driving camera lens 120 to rotate are fixed on part end 110.Rotary drive is steering engine
130。
Eight 140 distribution situations of shock-absorbing arms of above-mentioned damping module are：Four shock-absorbing arms 140 are located at 120 top of camera lens, incline
Oblique connection lens 120 and component end 110, are used for fixed lens 120, and buffer 120 upward direction of camera lens or obliquely upward to
Vibrations.Other four shock-absorbing arms 140 are located at 120 lower section of camera lens, connection lens 120 and component end 110 are tilted, for fixing
Camera lens 120, and buffer camera lens 120 in downward direction or oliquely downward to vibrations.The vibrations of camera lens 120 in the horizontal can also pass through
The collective effect of the shock-absorbing arms 140 of tilted upward placement is into row buffering.Therefore realize that 120 various dimensions of camera lens shake pooling feature.
In a specific embodiment, above-mentioned damping module is coupled with camera lens 120, for the vibrations of camera lens 120 into
Row buffering comprising：The shock-absorbing arms 140 of eight space coordinate axial directions.The shock-absorbing arms 140 of each space coordinate axial direction is respectively by two
A spring 142 and a shock-absorbing ball 141 are constituted.Each spring 142 and a 141 coaxial connection of shock-absorbing ball.Eight shock-absorbing arms 140
Distribution situation be：Four shock-absorbing arms 140 are located at 120 top of camera lens, tilt connection lens 120 and component end 110, can be used for
Buffer 120 upward direction of camera lens or obliquely upward to vibrations.Four shock-absorbing arms 140 are located at 120 lower section of camera lens, tilt connection mirror
First 120 and component end 110, can be used for buffering camera lens 120 in downward direction or oliquely downward to vibrations.Meanwhile camera lens 120 exists
The vibrations of lateral all directions, the collective effect for the shock-absorbing arms 140 that can also be disposed by tilted upward is into row buffering.Therefore it realizes
120 various dimensions of camera lens shake pooling feature.
In a specific embodiment, a kind of aircraft is equipped with above-mentioned lens assembly 100.Lens assembly 100 includes
Camera lens 120 is connect with camera lens 120, for fixed lens 120 and buffer camera lens 120 vibrations damping module.Lens assembly 100
Further include the component end 110 for determining 120 position of camera lens and the steering engine 130 for driving rotating lens 120.
In order to realize that aircraft carries the function that lens assembly 100 flies and shoots, aircraft removes and is equipped with above-mentioned camera lens
Outside component 100, function module should be also installed.The function module on the one hand flight for controlling aircraft, is on the other hand used for
Complete driving of the aircraft by steering engine 130 to camera lens 120.
In order to complete control of the function module to the flight control of aircraft and to steering engine 130, the function module of aircraft
Should include data transmission unit, Power Management Unit, processing unit and storage unit.
Data transmission unit may include wireless transceiver, antenna.Wireless transceiver can use wireless communication wave band
Electromagnetic wave carries out data transmission, and the WIFI electromagnetic waves of Conventional band can also be used to carry out data transmission.Specifically for example, using
4G communication signals or 2.4Ghz WIFI signals.On the one hand data transmission unit can receive user to aircraft flight and steering engine
The control instruction that 130 control camera lenses 120 rotate, on the other hand can be by 120 shooting angle of the flight parameter of aircraft and camera lens
User is fed back to, so that user is more accurately controlled aircraft flight and the shooting of camera lens 120.Certainly, data transmission unit may be used also
With by the parameter feedback involved in concrete application function to user.
Power Management Unit can manage the power supply of aircraft carrying.It is specific for example, power supply electric energy residual volume it is timely
Feedback, the occupation mode etc. of power supply electric energy.
Processing unit is usually expressed as processing chip.Storage unit can usually show as calculator memory or caching.Sequence
Rowization instruction set can usually be stored in storage unit.Processing unit executes serializing instruction set to realize the work(of functional module group
Energy.The various methods such as control method, data transmission method, the method for managing power supply of aircraft flight are usually by way of programming
Formation sequence instruction set, is stored in storage unit.
Each technical characteristic of embodiment described above can be combined arbitrarily, to keep description succinct, not to above-mentioned reality
It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, it is all considered to be the range of this specification record.
Above-described embodiments merely represent several embodiments of the utility model, the description thereof is more specific and detailed,
But therefore it can not be interpreted as the limitation to utility model patent range.It should be pointed out that for the common skill of this field
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
The scope of protection of the utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (9)
1. a kind of lens assembly, which is characterized in that including：
Camera lens；
Connected with camera lens, for determine lens location and buffer camera lens vibrations damping module；
Rotary drive；
The rotary drive is connect with camera lens, and for driving the rotation of lens.
2. lens assembly according to claim 1, which is characterized in that further include：
Component end；
The component end connects the camera lens by the damping module, and for determining the lens location；
The rotary drive is fixed on the component end.
3. lens assembly according to claim 2, which is characterized in that the damping module is by more than two shock-absorbing arms groups
At；
Described shock-absorbing arms one end connects the component end, and the shock-absorbing arms other end connects the camera lens.
4. lens assembly according to claim 3, which is characterized in that the shock-absorbing arms of the damping module is respectively from different skies
Between coordinate axially connect the camera lens and the component end so that the camera lens realizes damping effect in various dimensions.
5. lens assembly according to claim 4, which is characterized in that the shock-absorbing arms includes:
Shock-absorbing ball；
The shock-absorbing ball has elasticity.
6. lens assembly according to claim 5, which is characterized in that the shock-absorbing arms further includes：
Spring；
The spring is connected with shock-absorbing ball；Shock-absorbing arms is collectively formed with shock-absorbing ball in the spring.
7. lens assembly according to claim 6, which is characterized in that a diameter of the spring axis and shock-absorbing ball exists
On same straight line, so that shock-absorbing arms deforms upon in an axial direction when working.
8. a kind of damping module, matched with camera lens, for the vibrations to camera lens into row buffering, which is characterized in that including：
The shock-absorbing arms of more than two space coordinate axial directions.
9. a kind of aircraft, which is characterized in that be equipped with lens assembly；
The lens assembly includes：
Camera lens；
Connected with camera lens, for determine lens location and buffer camera lens vibrations damping module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721370834.7U CN207978026U (en) | 2017-10-23 | 2017-10-23 | Lens assembly, damping module and the aircraft for installing lens assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721370834.7U CN207978026U (en) | 2017-10-23 | 2017-10-23 | Lens assembly, damping module and the aircraft for installing lens assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207978026U true CN207978026U (en) | 2018-10-16 |
Family
ID=63771000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721370834.7U Active CN207978026U (en) | 2017-10-23 | 2017-10-23 | Lens assembly, damping module and the aircraft for installing lens assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207978026U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021098410A1 (en) * | 2019-11-18 | 2021-05-27 | 北京石头世纪科技股份有限公司 | Camera device and cleaning robot |
-
2017
- 2017-10-23 CN CN201721370834.7U patent/CN207978026U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021098410A1 (en) * | 2019-11-18 | 2021-05-27 | 北京石头世纪科技股份有限公司 | Camera device and cleaning robot |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11787540B2 (en) | Unmanned flight systems and control systems thereof | |
| EP3419894B1 (en) | Foldable multi-rotor aerial vehicle | |
| CN207634925U (en) | A kind of holder and the camera assembly with this holder | |
| CN107097966B (en) | A kind of holder and unmanned vehicle | |
| CN204297112U (en) | A kind of omnidirectional motor increases steady The Cloud Terrace | |
| CN111867932A (en) | Unmanned aerial vehicle comprising omnidirectional depth sensing and obstacle avoidance air system and operation method thereof | |
| CN105667775A (en) | Mobile phone App based remotely-controllable miniature aerial-photographing four-rotor aircraft and control method thereof | |
| CN207978026U (en) | Lens assembly, damping module and the aircraft for installing lens assembly | |
| CN207773419U (en) | Unmanned plane | |
| CN106275478A (en) | A kind of slide rail type three-axis stabilization The Cloud Terrace | |
| CN109589580A (en) | The intelligent tennis ball image training robot and training method of view-based access control model identification and Omni-mobile | |
| US11785119B2 (en) | Cloud-based microservices system | |
| CN108268121A (en) | Control method, control device and the control system of unmanned vehicle | |
| CN106428595A (en) | Built-in image stabilization cradle head for miniature unmanned aerial vehicle | |
| CN105589469A (en) | Quadcopter using Wi-Fi in manipulation and video transmission | |
| US11254444B2 (en) | Gimbal, photographing apparatus having same, and unmanned aerial vehicle | |
| CN209351613U (en) | A kind of concealed three axis holder of O-E Payload for UAV | |
| CN206609424U (en) | Microlight-type variable-angle aviation oblique photograph system | |
| CN207670655U (en) | A kind of auto-folder three-axis stability augmentation camera shooting quadrotor drone | |
| US20200106853A1 (en) | Efficient cloud-based data transfers with a wearable computing device | |
| CN108698692A (en) | Flight instrumentation without wing | |
| CN207631490U (en) | Holder, picture shooting assembly and unmanned vehicle | |
| CN110271685A (en) | A kind of unmanned plane of taking photo by plane based on ARM and FPGA | |
| CN114671021A (en) | Unmanned aerial vehicle based on gesture control | |
| CN211220674U (en) | Wide-view-angle robot |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |