CN108541295A - Remote controler - Google Patents
Remote controler Download PDFInfo
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- CN108541295A CN108541295A CN201780006827.5A CN201780006827A CN108541295A CN 108541295 A CN108541295 A CN 108541295A CN 201780006827 A CN201780006827 A CN 201780006827A CN 108541295 A CN108541295 A CN 108541295A
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- China
- Prior art keywords
- fuselage
- rolled round
- remote controler
- round component
- runner
- 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.)
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- 230000033001 locomotion Effects 0.000 claims abstract description 24
- 230000007246 mechanism Effects 0.000 claims description 21
- 238000004891 communication Methods 0.000 claims description 18
- 238000009434 installation Methods 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 8
- 230000036544 posture Effects 0.000 description 7
- 230000008901 benefit Effects 0.000 description 6
- 230000008859 change Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000004044 response Effects 0.000 description 4
- 238000007789 sealing Methods 0.000 description 4
- 230000000007 visual effect Effects 0.000 description 4
- 238000012938 design process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000003550 marker Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 210000004907 gland Anatomy 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 241000288673 Chiroptera Species 0.000 description 1
- 241000282320 Panthera leo Species 0.000 description 1
- 241000276425 Xiphophorus maculatus Species 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000000837 restrainer Substances 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/60—Control of cameras or camera modules
- H04N23/66—Remote control of cameras or camera parts, e.g. by remote control devices
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Mechanical Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Studio Devices (AREA)
- Accessories Of Cameras (AREA)
Abstract
A kind of remote controler, for controlling holder (200), including：Fuselage (110) and the first rolled round component (131)；The first rolled round component (131) is rotatablely connected by shaft (162) and fuselage (110), and the relative position by the way that the first rolled round component (131) and fuselage (110) can be changed relative to the rotation of the fuselage (110) around the shaft (162)；The first rolled round component (131) include the first runner (1311), first runner (1311) being rotated by driving force, to control the movement of the holder (200) at least one axis.By installing the first rolled round component on the fuselage of remote controler, shooting personnel can control the movement of at least one axis of holder by rotating the first runner, improve the precision of cradle head control, and its position and angle between fuselage can be adjusted by rotating the first rolled round component, facilitate the operation of shooting personnel.The present invention also provides a kind of capture apparatus.
Description
Technical field
The present invention relates to a kind of remote controlers, belong to movie and television play capture apparatus technical field.
Background technology
With the development of internet, the movie and television plays such as film, TV play and documentary film quantity just increasing year by year.In movie and television play
Shooting process in, due to the needs of shooting or the limitation of scene, it is often necessary to video camera is manipulated at a distance, because
This, will be equipped with the remote controler that can manipulate the holder for carrying capture apparatus.Existing remote controler is all rocker-type remote controler,
This rocker-type remote controler includes：Fuselage rotatable two rocking bars and is arranged in the day of front fuselage on fuselage
Line.Wherein, the yaw angle and pitch angle of holder can be controlled by controlling or rotating upwardly and downwardly two rocking bars.But it is existing
The rocking bar of this rocker-type remote controler be club, which has certain Hui Zhongli, and operating personnel can not be precisely controlled and shake
The stop position of bar, it is insufficient so as to cause the control accuracy of rocking bar, and also existing rocker-type remote controler cannot be satisfied different bats
The requirement taken the photograph personnel or manipulated for multiposition under different application scene.
Invention content
In order to solve existing in the prior art above-mentioned or other potential problems, the embodiment of the present invention provides a kind of remote control
Device.
According to some embodiments of the present invention, a kind of remote controler is provided, for controlling holder, including：Fuselage and first
Rolled round component；The first rolled round component is rotatablely connected by shaft and fuselage, and by around the relatively described fuselage of the shaft
Rotation can be changed the first rolled round component and fuselage relative position；The first rolled round component includes the first runner, institute
State the first runner being rotated by driving force, to control the movement of at least one axis of the holder.
Technical solution according to the ... of the embodiment of the present invention, by installing the first rolled round component on the fuselage of remote controler, to
In shooting process, shooting personnel can control the movement of at least one axis of holder by rotating the first runner, to control
The posture of holder realizes the control to video camera shooting angle.Since the first runner can rotate random angle under outer power drive
Degree, thus, it is possible to obtain the controlling curve of approximately linear, to improve the precision of cradle head control, and by relative to machine
Body rotate the first rolled round component can obtain multiple manipulation positions, to meet different shooting personnel, different application environment or
The demand of multi-angled shooting.
Description of the drawings
Described in detail below, the above and other objects, features and advantages general of the embodiment of the present invention by referring to accompanying drawing
It becomes more clearly understood from.In the accompanying drawings, by by example and it is unrestricted in a manner of to the present invention multiple embodiments say
It is bright, wherein：
Fig. 1 is the structural schematic diagram for the capture apparatus that one embodiment of the invention provides；
Fig. 2 is the structural schematic diagram of remote controler provided in an embodiment of the present invention；
Fig. 3 is the front view of Fig. 2；
Fig. 4 is the rearview of Fig. 2；
Fig. 5 is the right view of Fig. 2；
Fig. 6 is the vertical view of Fig. 2；
Fig. 7 is the vertical view after the rotation of the first rolled round component in Fig. 2；
Fig. 8 is that the first rolled round component is in the partial sectional view overlooked under visual angle in Fig. 7；
Fig. 9 is sectional view along A-A in Fig. 8；
Figure 10 is that the first rolled round component is in the partial sectional view looked up under visual angle in Fig. 7；
Figure 11 is B-B direction sectional view in Figure 10；
Figure 12 is the structural schematic diagram for the remote controler that another embodiment of the present invention provides；
Figure 13 is the front view of Figure 12；
Figure 14 is the left view of Figure 12；
Figure 15 is the right view of Figure 12；
Figure 16 is the vertical view of Figure 12；
Figure 17 is the explosive view of third rolled round component in Figure 12；
Figure 18 is the structural schematic diagram for the wireless communication device that one embodiment of the invention provides；
Figure 19 is the front view of Figure 18；
Figure 20 is the right view of Figure 18；
Figure 21 is the left view of Figure 18；
Figure 22 is the vertical view of Figure 18.
In figure：
100, remote controler；110, fuselage；120, wireless communication device；121, antenna；123, main body；125, interface；127、
Knob；129, Pin contact；131, the first rolled round component；1311, the first runner；1312, handle；1313, interconnecting piece；1314、
Speed control knob；1315, adjusting knob；1316, switching switch；133, the second rolled round component；1331, the second runner；1332、
Handle；1333, interconnecting piece；1334, speed control knob；1335, adjusting knob；1336, switching switch；135, third rolled round group
Part；1351, third runner；1352, handle；1353, interconnecting piece；1354, speed control knob；1355, adjusting knob；1356、
Switching switch；141, power switch；142, shooting switch；143, home keys；144, focusing button；145, focusing knob；146、
Aperture adjusting knob；147, output interface；148, expansion interface；150, controller；161, guide part；1611, positioning column；162、
Shaft；163, guide groove；164, fixing piece；165, trapezoidal slide block；166, positioning plate；167, screw rod；168, locating slot；169, it locks
Tight knob；170, battery；181, strip；1811, flange；183, link block；1831, card slot；1833, limiting slot；185, it locks
Knob；190, display；191, display battery；200, holder；300, video camera.
Specific implementation mode
Below in conjunction with the accompanying drawings, it elaborates to some embodiments of the present invention.In the absence of conflict, following
Feature in embodiment and embodiment can be combined with each other.
Fig. 1 is the structural schematic diagram of capture apparatus provided in this embodiment.As shown in Figure 1, the capture apparatus of the present embodiment
Including：Remote controler 100, holder 200 and video camera 300.Wherein, holder 200 can be fixed on ground or other determine object
Upper (such as house, trees, rock etc.), can also be mounted in mobile article (such as automobile, rail vehicle or unmanned plane
Deng), in the present embodiment, holder 200 can be the holder of arbitrary structures in the prior art, such as two axle The Cloud Terraces or three axis
Increase steady holder.Video camera 300 is carried by holder 200, and can adjust video camera by the adjustment of 200 posture of holder
300 shooting direction and angle realizes multi-angle, multidirectional shooting, to obtain the image or image element needed for photographer
Material, to facilitate the later stage to carry out editing editor to it to make movie and television play or from media video etc..In the present embodiment, holder
The adjustment of 200 postures is the remote controler 100 by being wirelessly connected with holder 200 to realize, the concrete structure of remote controler 100 will
It is described in detail later.By remote controler 100, shooting personnel can the shooting direction to video camera 300 and bat at a distance
It takes the photograph angle to be controlled, so as to obtain preferably shooting material so that the movie material of post-production has more true
Scene Representation ability.For example, the video camera 300 carried on unmanned plane can be controlled by remote controler 100 to shoot in steep cliff
The real-time performance of the sportsman of the free climbing either predation picture of lion or from sky on wide-long shot grassland on cliff
In take a crane shot grand the fight scene of historical subject matter movie and television play etc..
Fig. 2 is the structural schematic diagram of remote controler provided in this embodiment；Fig. 3 is the front view of Fig. 2；Fig. 4 is the backsight of Fig. 2
Figure；Fig. 5 is the right view of Fig. 2；Fig. 6 is the vertical view of Fig. 2.
As shown in Figures 2 to 6, remote controler 100 includes：Fuselage 110 and the first rolled round component 131.Wherein, the first rolled round group
Part 131 include the first runner 1311, first runner 1311 being rotated by driving force, with control holder 200 to
The movement of a few axis, so as to adjust the posture of holder 200 so that the video camera 300 carried on the holder 200 obtains suitably
Shooting angle and shooting direction.
Specifically, the first runner 1311 can control in the yaw axis, pitch axis and wobble shaft of holder 200 at least
One, with yaw angle, pitch angle and the roll angle of corresponding adjustment holder 200.In operation, by controlling the first runner
1311 rotate around its rotation axis, and fuselage 110 is incuded or received after direction and the angle of the rotation of the first runner 1311
With regard to generating the control information of control 200 at least one axis of holder movement to change the posture of holder 200.When holder 200 receives
At least one of the yaw motor on holder 200, pitching motor, rolling motor will be controlled after the control information to rotate,
To make at least one axis of holder 200 move, and then at least one in the yaw angle of adjustment holder 200, pitch angle, roll angle
Person.For example, when the first runner 1311 is used to control the yaw axis of holder 200, if the first runner 1311 rotates clockwise 5
Degree, the then yaw motor that can control holder 200 rotate to drive yaw axis to move, so that the yaw angle of holder 200 is also corresponding
5 degree of rotation.In another example when the first runner 1311 is used to control the yaw axis of holder 200 and pitch axis moves, it can be the
The pitching motor that holder 200 is controlled when one runner 1311 rotates clockwise rotates to drive pitch axis to move, in the first runner
1311 yaw motors that holder 200 is controlled when rotating counterclockwise rotate to drive yaw axis to move.It is of course also possible to pass through setting
Switching switchs to realize control of first runner 1311 to yaw axis and pitch axis.For another example when the first runner 1311 is for controlling
When yaw axis, pitch axis or the wobble shaft of holder 200 processed move, the first runner 1311 can be switched by the way that switching push button is arranged
The axis of the holder 200 controlled.
It should be noted that the first runner that the fuselage 110 of remote controler 100 will directly can also be received or be sensed
1311 rotation direction and angle and the controller 150 for being sent to holder 200, control is generated by the controller 150 of holder 200
Yaw motor, pitching motor or the control information of rolling motor rotation of holder 200.Certainly, in reality to remote controler 100
In setting up procedure, 1311 rotational angle of the first runner or rotation direction can also be used as control 200 running parameter of holder
Condition.
In the present embodiment, due to control holder 200 axial-movement be by way of rotating the first runner 1311 come
It realizes, there is no the rocking bars of existing rocker-type remote controler to have Hui Zhongli, can not accurately control lacking for rocking bar stop position
It falls into, the control to 200 approximately linear of holder can be obtained, to improve the control accuracy of remote controler 100, stablized and high
The shooting material of quality.Also, the posture of holder 200 is adjusted using the first runner 1311, to control the bat of video camera 300
Taking the photograph the mode of operation of angle and shooting direction, also shooting custom long-term with shooting personnel is close, to lead to shooting personnel
For the discomfort of mode of operation, the time that shooting personnel adapt to remote controler 100 is reduced, the efficiency of shooting is improved.
In order to describe simplicity, for controlling the yaw angle of holder 200 by the first rolled round component 131 below, shaken to first
The structure of wheel assembly 131 is described in detail, it is understood that, it is described below and is equally applicable to 200 pitch axis of holder
With the control of wobble shaft.
As shown in Figures 2 to 6, the first rolled round component 131 is mounted on the left side of fuselage 110, to facilitate shooting personnel to use
Left hand rotates the first runner 1311 to control the yaw angle of holder 200.It is apparent that the first rolled round component 131 can also basis
Need other suitable positions mounted on fuselage 110.It further, can be more when rotating the first runner 1311 in order to shoot personnel
Good grasping, is optionally equipped with handle 1312 in the outside (left side in Fig. 2) of the first runner 1311.In this way, shooting personnel
The first runner 1311 can be rotated by grasping member 1312, it is convenient and labor-saving.It is appreciated that the handle 1312 can
It omits, and first runner 1311. is rotated by holding the outer profile of the first runner 1311
With continued reference to Fig. 2 to Fig. 6, the first runner 1311 is connected to the left side of fuselage 110 by interconnecting piece 1313.It is optional
Ground, interconnecting piece 1313 are the structure with 1311 one of the first runner, such as the medial surface that interconnecting piece 1313 is the first runner 1311
It is formed by convex block.The through-hole that shaft opens up on the axis hole and convex block at 1311 center of the first runner is fixed on fuselage 110
Left side wall on.The gland for being screwed in roller end is provided in the outside of the first runner 1311, it, can be with by the limitation of gland
The first runner 1311 is avoided to be fallen from shaft.Again optionally, interconnecting piece 1313 and the first runner 1311 are separate structure, such as
Interconnecting piece 1313 is a rectangular block.Shaft is fixed on after the axis hole at 1311 center of the first runner on the side wall of link block,
To which the first runner 1311 can be rotated around shaft to control the yaw angle of holder 200.
In embodiments of the present invention, pass through with fuselage 110 with the interconnecting piece 1313 of 1311 split settings of the first runner
Shaft 162 is rotatablely connected, as shown in Figure 7, wherein Fig. 7 is the vertical view after the rotation of the first rolled round component in Fig. 2.Shaft 162 can
To be fixed on fuselage 110 or interconnecting piece 1313, alternatively, shaft 162 is located at hinge center, the both ends of hinge are respectively with first
Rolled round component 131 and interconnecting piece 1313 are fixed.
The remote controler 100 of the present embodiment connects the first rolled round component 131 and fuselage 110 by shaft 162, so as to
It is suitable to obtain to adjust its relative position or relative angle with fuselage 110 by rotating the first rolled round component 131
Operating clearance and work angle facilitate the first runner of shooting personnel control 1311 to rotate or operate selectivity and are shaken mounted on first
Wheel assembly 131, fuselage 110 or the function button on both.Based on aforementioned it is found that remote controler 100 provided in this embodiment,
Its position and angle between fuselage 110 can be adjusted by rotating the first rolled round component 131, facilitate shooting personnel's
Operation, including but not limited to adapts to the operating habit of different operating positions and angle requirement, different personnel, and adapts to certain
The application environment etc. of special screne (such as narrow space).
It should be noted that in order to lock the first rolled round component 131 and fuselage 110, need not turn to avoid the two
It is subjected to displacement when dynamic, arbitrary locking mode can be taken to lock the two.For example, when shaft 162 is mounted on fuselage 110
When, it can realize the first rolled round component by the way that the stiction between the first rolled round component 131 and shaft 162 is rationally arranged
Locking between 131 and shaft 162；It similarly, can be by reasonable when shaft 162 is mounted on the first rolled round component 131
Stiction between fuselage 110 and shaft 162 is set to realize locking.
Optionally, remote controler 100 is provided with the locking machine for locking or loosening fuselage 110 and the first rolled round component 131
Structure, the retaining mechanism include locking piece.Various structures may be used in locking piece.In the present embodiment, the locking piece is screw rod
167, screw rod 167 passes through the threaded hole opened up on fuselage 110 or the first rolled round component 131, supports in the first rolled round component 131
Or on fuselage.In this way, fuselage 110 and the first rolled round component 131 can be locked by way of tightening screw rod 167.This
Outside, locking piece can also be lock, and the movable part and fixed part of the lock are separately mounted to the first rolled round component 131 and machine
On body 110, vice versa, to realize the locking to the first rolled round component 131 and fuselage 110.For another example, locking piece is chock, when
After first rolled round component 131 turns to required angle, which is inserted into the first rolled round component 131 and fuselage 110
Between, to realize the locking of fuselage 110 and the first rolled round component 131.For another example, locking piece is pin, in fuselage 110 or first
Multiple pin holes are provided on rolled round component 131, so as to insert pin after the first rolled round component 131 turns to proper angle
Enter the locking that the first rolled round component 131 and fuselage 110 is realized in pin hole.
Fig. 8 is that the first rolled round component is in the partial sectional view overlooked under visual angle in Fig. 7；Fig. 9 be in Fig. 8 A-A to section view
Figure；Figure 10 is that the first rolled round component is in the partial sectional view looked up under visual angle in Fig. 7；
Figure 11 is B-B direction sectional view in Figure 10.
As shown in Figure 7 to 10, optionally, for convenience to the relative rotation of the first rolled round component 131 and fuselage 110 into
Row is oriented to, and guiding mechanism is additionally provided between fuselage 110 and interconnecting piece 1313.The guiding mechanism includes being arranged in the first rolled round
Guide groove 163 on component 131, and it is slidably installed in the sliding block connecting in the guide groove 163 and with fuselage.For example, in interconnecting piece
Guide part 161 is arranged in 1313 inside, and guide groove 163 is opened up on guide part 161；Correspondingly, the setting in guide groove 163
The sliding block that can be slided in guide groove 163, the sliding block can be connected to fuselage by connecting rod or other structures form
110.In this way, when driving 162 rotation around the shaft of the first rolled round component 131, sliding block can slide in guide groove 163, from
And realize guiding role.In the present embodiment, the sliding block is connected to fuselage 110 by locking piece 167.In another example in fuselage 110
Left side wall on above-mentioned guide part 161 is installed, and the sliding block being slidably installed in guide groove 163 is fixed on the suitable of interconnecting piece 1313
Position.In addition it is also possible to which the directly setting slide bar that is connect with the first rolled round component 131 substitutes above-mentioned cunning in guide groove 163
Block.In the present embodiment, above-mentioned guide part 161 includes but not limited to platy structure, block structure and frame structure.
The shape of guide groove 163 is not specifically limited, and those skilled in the art can be designed according to actual needs.Example
Such as, guide groove 163 is using shaft as the arc groove in the center of circle, so as to what is moved with the relatively described fuselage 110 of the first rolled round component 131
Movement locus matches.Depth direction along guide groove 163 can be designed to dovetail groove as shown in Figure 9.When guide groove 163
, can be accordingly by slider designs at the trapezoidal slide block 165 coordinated with the dovetail groove when cross section is designed to dovetail groove, this
Sample, so that it may to realize that locking or release first are shaken by changing the size in the gap between trapezoidal slide block 165 and dovetail groove
The effect of wheel assembly 131.
Further, in order to realize the adjustment to trapezoidal slide block 165 and dovetail groove gap to lock fuselage 110 and the first rolled round
Locking piece can be arranged to screw rod 167, and trapezoidal slide block 165 and the connecting pin of screw rod 167 are fixed by component 131.Below will
By taking guide groove 163 is arranged on the first rolled round component as an example, to the matching relationship of screw rod 167 and fuselage 110 and trapezoidal slide block 165
It is introduced, certainly, following matching relationships can also be arranged in guide groove 163 in machine directly or through being applied after simple replacement
In remote controler on body 110.
It is provided with external screw thread on screw rod 167, phase is provided in the through-hole of fuselage 110 for the free end of screw rod 167
The internal thread of cooperation.Trapezoidal slide block 165 can be pushed to be moved in the axial direction of screw rod 167 by rotary screw 167 in this way,
To realize the effect of the fit clearance between adjustment trapezoidal slide block 165 and dovetail groove, and then the first rolled round component 131 is locked
On fuselage 110.Optionally, in order to facilitate rotary screw 167, locking piece further includes being installed mounted on the free end of screw rod 167
Locking knob 169.In assembly, which can be fixed on to the free end of screw rod 167 by screw.When need
When locking or discharging the first rolled round component 131, it is only necessary to the locking knob 169 that the free end of rotary screw 167 is installed
Screw rod 167 can be driven to move axially, to drive trapezoidal slide block 165 also to be moved axially along screw rod 167, and then adjusted trapezoidal
Fit clearance between sliding block 165 and dovetail groove realizes the purpose of locking or the first rolled round component of release 131 and fuselage 110.
Optionally, boss can be formed in lead to the hole site, to facilitate the movement of locking knob 169.
Optionally, fuselage 110 further includes fixing piece 164, and the free end of screw rod 167 passes through what is opened up on fixing piece 164 to lead to
Hole.For example, fuselage 110 includes the fixing piece 164 for being set to left side, at this point it is possible to which shaft 162 is mounted on fixing piece 164.
(such as upper right corner) vertically offers axis hole on interconnecting piece 1313, and shaft 162 is threaded through in the axis hole, to realize the first rolled round
The rotation connection of component 131 and fuselage 110.As a kind of interchangeable mode, shaft 162 can also be mounted on interconnecting piece
On 1313, while axle sleeve being installed on fixing piece 164, and axle sleeve is set in and realizes the first rolled round component 131 in shaft 162
With the rotation connection of fuselage 110.Similarly, fixing piece 164 can also be mounted on the first rolled round component 131, screw rod 167
Free end passes through the through-hole opened up on fixing piece to extend to outside the first rolled round component 131.
The specific constructive form of fixing piece 164 is not especially limited in the present embodiment, and those skilled in the art can select
Any appropriate structure is selected as fixing piece.For example, fixing piece 164 can be two intervals being arranged on fuselage 110
The guide part 161 of the fixed plate of certain distance, the first rolled round component 131 is housed between the two fixed plates or first shakes
When being rotated relative to fuselage 110, at least part of guide part 161 can expose wheel assembly 131 between two fixed plates.
Obvious, the first rolled round component 131 may also comprise two spaced guide plates, and correspondingly, fuselage 110 includes fixing piece,
And it can award between two guide plates of the first rolled round of honor component 131.
Optionally, as shown in Figure 10 and Figure 11, other position restrainers are additionally provided between fuselage 110 and interconnecting piece 1313
Structure, for limiting the angular range that the first rolled round component 131 is rotated relative to fuselage 110.In some optionally embodiment,
Position-limit mechanism is the flexible piece that both ends are connect with fuselage and the first rolled round component respectively, such as rope or chain.Other can
In selection of land embodiment, position-limit mechanism includes：Locating slot and the positioning column being plugged in locating slot.For example, locating slot is arranged
On fuselage 110, positioning column is arranged on the first rolled round component 131, and vice versa.Specifically, it can be set on fuselage 110
Positioning plate 166 is set, such as the positioning plate 166 is set on the left side wall of fuselage.It further, can also be by positioning plate 166 and upper
It states two fixed plates to be arranged in parallel, or one of fixed plate is used directly as positioning plate.Further, in order to operate
It is convenient, positioning plate 166 can be arranged in the lower section of fixed plate, or using underlying fixed plate as positioning plate.Positioning
The locating slot 168 for limiting the first rolled round component 131 maximum rotation angle and minimum rotation angle is offered on plate 166.It leads
Surface of the part 161 towards positioning plate 166 is provided with positioning column 1611, which is inserted into locating slot 168.In reality
In the design process of border, shape, position or the length of locating slot 168 can be arranged as required to obtain the first rolled round component
131 different size of rotatable angle ranges.By the way that position-limit mechanism is arranged, the first rolled round component 131 can be made to turn in maximum
It is dynamic to be moved between angle and minimum rotation angle, to facilitate different shooting personnel to use remote controler 100.
Further, as shown in Fig. 2 to Fig. 6, following one or more are optionally provided on interconnecting piece 1313：
For controlling the speed control knob 1314 of 200 yaw axis of holder, being revolved for controlling the adjusting of 200 yaw axis response speed of holder
Button 1315, the open-close on-off for enabling or closing the first rolled round component 131 or the first runner 1311 and for switching
The switching switch 1316 of left/right hand operation.In the present embodiment, speed control knob 1314, adjusting knob 1315, open-close on-off
It is not construed as limiting with the specific installation position of switching switch 1316, it is suitable that those skilled in the art can select according to actual demand
Position is designed.For example, above-mentioned speed control knob 1314, adjusting knob 1315, open-close on-off and switching can be switched
1316 are arranged in the top surface of interconnecting piece 1313 to facilitate shooting personnel to use.In addition, in specific setting, it can be by open-close on-off
And switching switch 1316 is arranged between speed control knob 1314 and adjusting knob 1315.Optionally, in specific design process
In, open-close on-off and switching switch 1316 can be integrated, to reduce the quantity of switch.For example, as shown in Fig. 2, can
Open-close on-off and switching switch 1316 are integrated into a deflector rod switch.In operation, driving lever is pushed and intermediate then deactivates the
One rolled round component 131 or the first runner 1311；Driving lever is pushed into left side, then enables the first rolled round component 131 or first turn
Wheel 1311, and shoot personnel and manipulate the first runner 1311 using left hand；Driving lever is pushed into right side, then enables the first rolled round component
131 or first runner 1311, and shoot personnel and manipulate the first runner 1311 using the right hand.It is of course also possible to select other
Suitable integrated switch realizes open-close on-off and switches the function of switch 1316.
In present embodiment, the adjusting knob 1315 is specifically used for adjusting response speed when holder starts；Switching is opened
The 1316 left/right hand operation correspondences for being specifically used for switching remote controler 100 with holder are closed, the user of different use habits is facilitated
Switching uses；Speed control knob 1314 is specifically used for controlling the controlled quentity controlled variable of the controller 100 and the cloud platform rotation amount
Correspondence.
In addition, in order to intuitively show the rotation angle of the first runner 1311, it can in shaft or interconnecting piece 1313
Selection of land fixes angled marker disc, and pointer is fixed on the first runner 1311.In this way, when the first runner 1311 turns around shaft
When dynamic, the pointer being fixed on the first runner 1311 also just follows the first runner 1311 to rotate, thus just by angle marker disc
The rotational angle of the first runner 1311 can intuitively be read.It is of course also possible to which corresponding in angle marker disc identify when the
When one runner 1311 turns to certain angle, the yaw angle of holder 200, for example, when the first runner 1311 rotates 30 degree, holder
200 yaw angle rotates 1 degree.
With continued reference to Fig. 2 to Fig. 7, remote controler 100 also optionally includes the second rolled round component 133.Second rolled round component 133
The second runner 1331 including the movement of 200 at least one axis of holder can be controlled.First rolled round component 131 and the second rolled round component
133 can integrate, or the two can also be arranged at intervals on to the outer edge of fuselage 110, for example, the first rolled round component
131 are arranged in the left side of fuselage 110, and the second rolled round component 133 is then arranged in the fuselage 110 opposite with the first rolled round component 131
Right side.By the way that the second rolled round component 133 is arranged, realizes and holder is controlled by the first runner 1311 and the second runner 1331
The control to more than 200 a axis of holder may be implemented in the movement of 200 at least two axis, improves the adjustment effect of 200 posture of holder
Rate.
In general, the second runner 1331 and the first runner 1311 are set as controlling the different axis of holder 200, but this
Embodiment is not excluded for the scheme of the second runner 1331 and the first runner 1311 control 200 same axis of holder.For example, when first turn
When wheel 1311 is used for controlling yaw angle of the movement of the yaw axis of holder 200 to adjust holder 200, the second rolled round component 133 is used
Come control holder 200 pitch axis movement to adjust the pitch angle or roll angle of holder 200, vice versa.Below with
One rolled round component 131 controls the movement of yaw axis, to the second rolled round group for the movement of the second rolled round component 133 control pitch axis
Part 133 is introduced.
Handle 1332 can also be set on second runner 1331 of the second rolled round component 133.Similarly, the second rolled round component
133 can also be arranged interconnecting piece 1333, also, can also selectively be arranged on interconnecting piece 1333 following a kind of or more
Kind：Speed control knob 1334 for controlling 200 pitch axis of holder, the tune for controlling 200 pitch axis response speed of holder
Save knob 1335, the open-close on-off for enabling or closing the second rolled round component 133 or the second runner 1331 and for cutting
Change the switching switch 1336 of left/right hand operation.
Further, it may be a fixed connection or be rotatablely connected between the second rolled round component 133 and fuselage 110.For example, the
One rolled round component 131 and the second rolled round component 133 are fixedly connected with fuselage 110, and certain this mode that is fixedly connected can be
It is dismountable or non-removable.In another example the first rolled round component 131 is rotatablely connected with fuselage 110 by shaft 162, the
Two rolled round components 133 are fixedly connected with fuselage 110, and vice versa.In this way, by rotating the first rolled round rotated with fuselage 110
Between component 131 or the second rolled round component 133 can adjust between the first rolled round component 131 and the second rolled round component 133
Away to facilitate different shooting personnel to manipulate remote controler 100.
Figure 12 is the structural schematic diagram of another remote controler provided in this embodiment；Figure 13 is the front view of Figure 12；Figure 14
For the left view of Figure 12；Figure 15 is the right view of Figure 12；Figure 16 is the vertical view of Figure 12；Figure 17 is third rolled round component in Figure 12
Explosive view.
As shown in Figure 12 to Figure 17, the remote controler 100 of the present embodiment further includes the third rolled round group being mounted on fuselage 110
Part 135, the third rolled round component 135 include rotatable third runner 1351, by driving the third runner 1351 to rotate, together
Sample can control the movement of 200 at least one axis of holder.It, can be 1311, second turns by the first runner when actual disposition
Wheel 1331 and third runner 1351 are arranged respectively to the axis movement for controlling holder 200, such as the first runner 1311 is used
Come control holder 200 yaw axis movement to adjust the yaw angle of holder 200, the second runner 1331 is used for controlling holder 200
Pitch axis movement to adjust pitch angle, third runner 1351 is used for controlling the movement of the wobble shaft of holder 200 to adjust cloud
The roll angle of platform 200 will be introduced the other structures of third rolled round component 135 with the above-mentioned example that is set as below.
Handle 1352 can also be set on the third runner 1351 of third rolled round component 135.Similarly, third rolled round component
135 can also be arranged interconnecting piece 1353, also, can also selectively be arranged on interconnecting piece 1353 following a kind of or more
Kind：Speed control knob 1354 for controlling 200 wobble shaft of holder, the tune for controlling 200 wobble shaft response speed of holder
Save knob 1355, the open-close on-off for enabling or closing third rolled round component 135 or third runner 1351 and for cutting
Change the switching switch 1356 of left/right hand operation.
Further, can also be to be fixedly connected or be rotatablely connected between third rolled round component 135 and fuselage 110.For example,
First rolled round component 131, the second rolled round component 133 and third rolled round component 135 are fixedly connected with fuselage 110, certainly this
It can be dismountable or non-removable that kind, which is fixedly connected with mode,.In another example the first rolled round component 131 and fuselage 110 are logical
The rotation connection of shaft 162 is crossed, the second rolled round component 133 is fixedly connected with fuselage 110, and third rolled round component 135 can with fuselage 110
Dismantling connection.Optionally, third rolled round component 135 is detachably connected by quick-disassembly structure and fuselage 110, so as to
Third rolled round component 135 is quickly installed as needed or disassembles third rolled round component 135 from fuselage 110, is reached
To the purpose of 100 function of Quick Extended remote controler.
Refering to fig. 12 to Figure 17, in some optionally embodiment, quick-disassembly structure includes：The strip formed on interconnecting piece
181 and fuselage 110 on formed can in some optionally embodiment for being clamped the card slot 1831 of the strip 181
Card slot 1831 is designed to dovetail groove.Card slot 1831 can be directly opened on the side wall of fuselage 110, or can also be as
A link block 183 being fixed on 110 side wall of fuselage is separately provided shown in Figure 17, card slot 1831 is then opened in the company
It connects on block 183.Optionally, limiting slot 1833 is further opened on the inner wall of card slot 1831, an end of the limiting slot 1833
Closing, is formed with the flange 1811 being connected in limiting slot 1833 on strip 181.For example, in fig. 17, at 1831 bottom of card slot
The limiting slot 1833 of upper end opening, lower end closed is offered on wall.Pass through the restriction of flange 1811 and limiting slot 1833, Ke Yiwei
Quick-disassembly structure provides additional clamping force, avoids strip 181 and 1831 clamping force of card slot deficiency and is detached from.Again optionally, corresponding
The end set of the flange 1811 of the opening end position of limiting slot 1833 has locking knob 185.For example, in fig. 17, in flange
Locking knob 185 is arranged in 1811 upper end, and in assembly, the bottom end of strip 181 is inserted into from the upper end of card slot 1831, and makes flange
Strip 181, is inserted into card slot 1831, then rotates locking rotating by the opening of 1811 bottom end alignment limiting slot 1833 from top to bottom
Button 185 reduces the gap of knob bottom and 183 top of link block, since the side wall of locking knob 185 has been more than limiting slot 1833,
Therefore, link block 183 and third rolled round component 135 can be locked after screwing locking knob 185.
In other optionally embodiment, quick-disassembly structure includes the strip 181, Yi Ji being arranged on fuselage 110
The card slot 1831 for being clamped strip 181 opened up on the interconnecting piece of three rolled round components 135.In addition, strip 181 and card slot 1831
Partial structurtes can be identical as partial structurtes described in the preceding paragraph, details are not described herein.
It is appreciated that the first rolled round component 131, the second rolled round component 133 can also use above-mentioned quick-disassembly structure and fuselage
110 connections.
Further, remote controler 100 also further includes optionally focusing rolled round, which includes being used for controlling holder 200
On focus tracking adjustment video camera 300 on physical lens stop focusing runner.Certainly, remote controler 100 can also include more shaking
Wheel, those skilled in the art can be set according to actual needs the function of suitable rolled round number and each rolled round.
It is appreciated that the first rolled round component 131, the second rolled round component 133, third rolled round component 135 and described
Focusing rolled round is not limited to address the mode presented in figure with the position relationship of the fuselage 110.
As shown in Fig. 2-16, wireless communication device 120 is mounted on fuselage 110, and such holder 200 can pass through the nothing
Line communication device 120 is established with fuselage 110 and is communicated to connect, and the control information of coming is transmitted to receive fuselage 110.Wireless communication dress
Any appropriate wireless communication device 120, such as WiFi module, bluetooth module etc. can be used by setting 120.It is wireless in specific assembly
When communication device 120, wireless communication device 120 can be directly assembled in fuselage 110, to form one with fuselage 110
Structure, naturally it is also possible to by wireless communication device 120 by way of interface or connecting line with fuselage 110 be connected to one
It rises, to facilitate the wireless receiving ability for improving remote controler 100 in some scenarios.For example, in some optionally embodiment,
Wireless communication device 120 is detachably connected to the trailing flank of fuselage 110, in this way, would not when the personnel of shooting manipulate runner
It is influenced by wireless communication device 120.It, can be by wireless communication device when needing in the car to be remotely controlled holder 200
120 remove from fuselage 110 and are then placed on roof, to improve the ability that remote controler 100 receives signal.
Figure 18 to Figure 22 gives a kind of quick disassembled wireless communication device 120, wherein Figure 18 is 121 component of antenna
Structural schematic diagram；Figure 19 is the front view of Figure 18；Figure 20 is the right view of Figure 18；Figure 21 is the left view of Figure 18；Figure 22 is figure
18 vertical view.
Refering to fig. 18 to Figure 22, which includes：Main body 123 and the day in main body 123
Line 121.Plug is provided in main body 123, and either socket is provided with matched socket or plug on fuselage 110, this
Wireless communication device 120 can be quickly installed on fuselage 110 by sample, or quickly be removed from fuselage 110.Optionally,
As shown in figure 20, Pin contact 129 is set in main body 123.Further, the outer peripheral edge of Pin contact 129 is designed with protrusion, in machine
It is designed with guide groove on the socket inner walls of body 110, with the correct installation of convenient plug and socket.Further, in plug and socket
It is inside provided with sealing structure, for example, the bottom in socket is formed with seal groove, is designed in the end of plug and is contained in the sealing
Sealing strip in slot；In another example being arranged with sealing ring in plug or socket.In addition, being also optionally provided in main body 123
Interface 125, to when disassembling wireless communication device 120 from fuselage 110, be connected by being inserted into interface 125
The mode of wiring links together itself and fuselage 110.Some control wireless communications optionally, in main body 123 can be also set again
The function knob 127 of function.
With continued reference to Fig. 2, Fig. 7 and Figure 12, the shape of fuselage 110 can select suitable shape, example according to specific needs
Such as, rectangle box body or cube box body can be selected as fuselage 110, in another example, fuselage 110 is it is also an option that such as Figure 12
Shown in irregular shape box body structure, with three or three or more rolled rounds of installation.It is appreciated that being equipped in fuselage 110
The electronic devices such as circuit board, sensor, are no longer described in detail herein, and those skilled in the art can be according to actual needs to fuselage
The type and connection type of electronic device are configured in 110.
Optionally, battery 170 is installed on fuselage 110.For example, when the first rolled round component 131 and the second rolled round component
133 set up separately at the left side and right side of fuselage 110, and battery 170 may be mounted at the leading flank of fuselage 110.Some can
In selection of land embodiment, accommodating case can be set on fuselage 110, then battery 170 is mounted in the accommodating case.Accommodating case
Concrete structure and set-up mode can design according to actual needs, be not specifically limited herein.For example, accommodating case can be by
The front side wall of fuselage 110 is recessed；In another example accommodating case is the component seperated with fuselage 110, it is fixed on fuselage 110.
Further, battery 170 is contained in by elastic mechanism in accommodating case, by the elastic reaction of elastic mechanism, is applied when to battery 170
Accommodating case can be popped up battery 170 or be locked in accommodating case by adding when thrust.For example, elastic mechanism is mounted on battery
The spring of 170 directions of motion.When needing to install battery 170, push 170 compressed spring of battery battery 170 to be fully advanced
In accommodating case, and the limited wall for being received box opening setting blocks, and prevents battery 170 from dropping out；When needing to take out battery 170,
170 compressed spring of battery is pushed again, battery 170 is made to be detached from conflict state with limited wall, then makes battery 170 toward perpendicular to spring
Direction displacement, so that it may so that battery 170 is popped up by the elastic force of spring from accommodating chamber.
As shown in Fig. 2 to 12, controller 150, such as GCU controllers are also optionally installed on fuselage 110, to side
Just shooting personnel set or change to the parameter of holder 200.For example, shooting personnel can input in controller 150
Correspondence between the yaw axis of each rolled round and holder 200, pitch axis and wobble shaft, that is to say, in controller
The correspondence control of the first rolled round component 131 is inputted in 150 is which of yaw axis, pitch axis and wobble shaft of holder 200
Or which.Certainly, this correspondence can also be preset by manufacturer or retailer.In another example shooting personnel can
Specifically rotation is more for some axis of the holder 200 of correspondence control when inputting the first runner 1,311 one circle of rotation by controller 150
Few degree.When being designed, any suitable position in fuselage 110 can be arranged in controller 150, for example, controller 150 can be with
It is arranged between the first rolled round component 131 and the second rolled round component 133, in another example, show that controller 150 can be set in Fig. 2
It sets in the top surface of fuselage 110, to facilitate shooting personnel to input corresponding control parameter.In some optionally embodiment, control
Device 150 processed is removably mounted on fuselage 110, can facilitate the replacement to controller 150 in this way.In addition, controller 150 can
To include display screen.
Also be optionally provided on fuselage 110 power switch 141, shooting switch 142, photographing switch, focusing button 144,
It is a kind of or more in focusing knob 145, aperture adjusting knob 146, home keys 143, output interface 147, expansion interface 148
Kind.In general, any suitable location in fuselage 110 can be arranged in above structure, can be with for example, as shown in Fig. 6 to Figure 16
Output interface 147 and expansion interface 147 are arranged and connect other external equipments, other portions in the trailing flank of fuselage 110 to facilitate
Part can be then arranged in the top surface of fuselage 110 to facilitate shooting personnel to operate.In a kind of optional embodiment, it can will control
Device 150 processed is arranged on the longitudinal axis of fuselage 110, and shooting switch 142 and home keys 143 are arranged in the left side of controller 150,
Power switch 141, focusing button 144, focusing knob 145 and aperture adjusting knob 146 are arranged on the right side of controller 150.
It should be appreciated that the aperture adjusting knob 146 being arranged on fuselage 110 can be used for adjusting electric aperture, the physics of video camera 200
One or more in aperture, but when remote controler 100 is provided with above-mentioned focusing rolled round, then aperture adjusting knob 146 can be with
It is only used for adjusting the electric aperture of video camera.
Finally, property is also an option that on fuselage 110 display 190 is set, it thus can be real on remote controler 100
When play or the shooting picture that is returned by video camera 300 of playback.In actual design process, display 190 can be independent
The display of configuration can also be the mobile electronic devices such as mobile phone or tablet computer.It can between display 190 and fuselage 110
To be linked together by wireless or wired mode, to realize the transmission of data.Specifically, in some optionally embodiments
In, angle-adjusting bracket is installed on fuselage 110, display 190 is carried on the angle-adjusting bracket, to realize fuselage
110 and display 190 mechanical connection.Various structures may be used in angle-adjusting bracket, for example, it may be link mechanism.It is logical
The adjustment at the angle of inclination between display 190 and fuselage 110 may be implemented in over-angle adjusting bracket, to facilitate shooting personnel
The content played on viewing display 190.In addition, display 190 can use on fuselage 110 battery 170 that carries or
Individual battery can be set.
Finally, although being described in the context of these embodiments associated with certain embodiments of the present technology
Advantage, but other embodiment can also include such advantage, and simultaneously the present invention is all described in detail in not all embodiments
All advantages, by the technical characteristic in embodiment objective the advantages of bringing be regarded as the present invention and be different from the prior art
Advantage all belongs to the scope of protection of the present invention.
Claims (35)
1. a kind of remote controler, for controlling holder, which is characterized in that including：Fuselage and the first rolled round component；
The first rolled round component is rotatablely connected by shaft and fuselage, and passes through the rotation around the shaft relative to the fuselage
The relative position of the first rolled round component and fuselage can be changed；
The first rolled round component include the first runner, first runner being rotated by driving force, with control
The movement of at least one axis of holder.
2. remote controler according to claim 1, which is characterized in that be provided with and lead between the first rolled round component and fuselage
To mechanism, for being oriented to when the first rolled round component is rotated relative to the fuselage.
3. remote controler according to claim 2, which is characterized in that
The guiding mechanism includes：Guide groove on the first rolled round component is set, and is slidably installed in the guide groove
And the sliding block being connect with the fuselage；Alternatively,
The guiding mechanism includes：Guide groove on the fuselage is set, and be slidably installed in the guide groove and with it is described
The sliding block of first rolled round component connection.
4. remote controler according to claim 3, which is characterized in that the guide groove is using the shaft as the arc in the center of circle
Slot.
5. remote controler according to claim 4, which is characterized in that the guide groove be dovetail groove, the sliding block for institute
State the trapezoidal slide block of dovetail groove cooperation.
6. remote controler according to claim 5, the remote controler further includes retaining mechanism, and the retaining mechanism includes locking
Part, the locking piece are locked or are loosened with the first rolled round component, and the fuselage and the first rolled round component are locked
Or loosen.
7. remote controler according to claim 6, which is characterized in that the locking piece is screw rod, is provided on the screw rod
Screw thread；The connecting pin of the screw rod is fixed with the trapezoidal slide block, and the screw rod passes through institute away from the free end of the connecting pin
State the threaded hole opened up on fuselage or the first rolled round component.
8. remote controler according to claim 7, which is characterized in that the retaining mechanism further includes locking knob, the lock
Tight knob is installed on the free end of the screw rod.
9. remote controler according to claim 7, which is characterized in that the fuselage or the first rolled round component are including fixing
The free end of part, the screw rod passes through the through-hole opened up on the fixing piece to extend to the fuselage or the first rolled round component
Outside.
10. remote controler according to claim 9, which is characterized in that the shaft is mounted on the fixing piece.
11. remote controler according to claim 9, the fixing piece is two one spacings of interval being arranged on the fuselage
From fixed plate, the guide part of the first rolled round component is contained between described two fixed plates or rotationally from described
Expose at least partly in fixed plate.
12. remote controler according to claim 7, which is characterized in that when the screw rod in axial direction rotates, can drive
The trapezoidal slide block is moved along the axial direction of screw rod, to lock or unlock the first rolled round component and fuselage.
13. according to claim 1-5 any one of them remote controlers, which is characterized in that further include retaining mechanism, the locking machine
Structure includes locking piece, is used for first rolled round after the first rolled round component rotates predetermined angle relative to the fuselage
Component and fuselage locking.
14. remote controler according to claim 13, which is characterized in that the locking piece is lock,
The movable part and fixed part of the lock are separately mounted on the first rolled round component and fuselage.
15. remote controler according to claim 13, which is characterized in that the locking member is chock, and the chock can be
It is inserted under the action of driving force between the first rolled round component and fuselage.
16. according to claim 1-12 any one of them remote controlers, which is characterized in that the first rolled round component and the machine
Position-limit mechanism is additionally provided between body, the angular range rotated relative to the fuselage for limiting the first rolled round component.
17. remote controler according to claim 16, which is characterized in that the position-limit mechanism includes：It locating slot and is plugged in
Positioning column in the locating slot.
18. remote controler according to claim 17, which is characterized in that the locating slot is arranged to be determined what the fuselage was installed
On the plate of position, the positioning column is arranged on the first rolled round component.
19. remote controler according to claim 17, which is characterized in that the locating slot is the arc centered on the shaft
Shape slot.
20. remote controler according to claim 16, which is characterized in that the position-limit mechanism is described in both ends are connected to
Flexible piece on fuselage and the first rolled round component.
21. according to claim 1-12 any one of them remote controlers, which is characterized in that the remote controler further includes the second rolled round
Component, the second rolled round component include the second runner, first runner and the second runner for controlling the holder at least
The movement of two axis.
22. remote controler according to claim 21, which is characterized in that first runner is for controlling the inclined of the holder
The movement of boat axis, second runner are used to control the movement of the pitch axis of the holder.
23. remote controler according to claim 21, which is characterized in that the second rolled round component is fixed with the fuselage to be connected
It connects, alternatively, the second rolled round component is rotatablely connected by shaft and the fuselage.
24. according to claim 1-12 any one of them remote controlers, which is characterized in that be provided with power supply on the fuselage and open
It closes.
25. remote controler according to claim 24, which is characterized in that be provided with focusing button, focusing rotation on the fuselage
One or more of button, aperture adjusting knob, shooting switch, photographing switch.
26. according to claim 1-12 any one of them remote controlers, which is characterized in that be equipped on the fuselage for setting
The controller of holder parameter.
27. remote controler according to claim 26, which is characterized in that the controller is detachably mounted to the fuselage
Top surface.
28. according to claim 1-12 any one of them remote controlers, which is characterized in that be equipped with battery on the fuselage.
29. remote controler according to claim 28, which is characterized in that the installation that the battery can be popped up by elastic mechanism
On the fuselage.
30. according to claim 1-12 any one of them remote controlers, which is characterized in that be connected with display on the fuselage.
31. remote controler according to claim 30, which is characterized in that the display by angle-adjusting bracket with it is described
Fuselage connects, and the angle-adjusting bracket is for adjusting angle of inclination of the display relative to fuselage.
32. according to claim 1-12 any one of them remote controlers, which is characterized in that the remote controler further includes and the machine
The wireless communication device that body is detachably connected.
33. remote controler according to claim 32, which is characterized in that the wireless communication device is detachably connected to institute
State the trailing flank of fuselage.
34. remote controler according to claim 1, which is characterized in that be provided with handle on first runner.
35. remote controler according to claim 1, which is characterized in that the shaft be mounted on the first rolled round component or
On person's fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110236746.2A CN113012417B (en) | 2017-08-04 | 2017-08-04 | Remote controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2017/096115 WO2019024118A1 (en) | 2017-08-04 | 2017-08-04 | Remote controller |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110236746.2A Division CN113012417B (en) | 2017-08-04 | 2017-08-04 | Remote controller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108541295A true CN108541295A (en) | 2018-09-14 |
| CN108541295B CN108541295B (en) | 2021-03-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780006827.5A Expired - Fee Related CN108541295B (en) | 2017-08-04 | 2017-08-04 | Remote controller |
| CN202110236746.2A Active CN113012417B (en) | 2017-08-04 | 2017-08-04 | Remote controller |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110236746.2A Active CN113012417B (en) | 2017-08-04 | 2017-08-04 | Remote controller |
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| Country | Link |
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| CN (2) | CN108541295B (en) |
| WO (1) | WO2019024118A1 (en) |
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| WO2019144408A1 (en) * | 2018-01-29 | 2019-08-01 | 深圳市大疆创新科技有限公司 | Remote control |
| CN110809734A (en) * | 2018-11-15 | 2020-02-18 | 深圳市大疆创新科技有限公司 | Camera lens adjusting method and device, control equipment and control system |
| CN113422905A (en) * | 2021-06-22 | 2021-09-21 | 浙江博采传媒有限公司 | Automatic control method and system for movement locus of focus follower |
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- 2017-08-04 CN CN201780006827.5A patent/CN108541295B/en not_active Expired - Fee Related
- 2017-08-04 CN CN202110236746.2A patent/CN113012417B/en active Active
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| WO2019144408A1 (en) * | 2018-01-29 | 2019-08-01 | 深圳市大疆创新科技有限公司 | Remote control |
| CN110325782A (en) * | 2018-01-29 | 2019-10-11 | 深圳市大疆创新科技有限公司 | Remote controler |
| CN110325782B (en) * | 2018-01-29 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Remote controller |
| CN110809734A (en) * | 2018-11-15 | 2020-02-18 | 深圳市大疆创新科技有限公司 | Camera lens adjusting method and device, control equipment and control system |
| CN113422905A (en) * | 2021-06-22 | 2021-09-21 | 浙江博采传媒有限公司 | Automatic control method and system for movement locus of focus follower |
| CN113422905B (en) * | 2021-06-22 | 2022-09-16 | 浙江博采传媒有限公司 | Automatic control method and system for movement locus of focus follower |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113012417A (en) | 2021-06-22 |
| CN113012417B (en) | 2022-04-15 |
| WO2019024118A1 (en) | 2019-02-07 |
| CN108541295B (en) | 2021-03-23 |
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