CN109927924A - Aviation oblique photograph holder - Google Patents
Aviation oblique photograph holder Download PDFInfo
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- CN109927924A CN109927924A CN201910197272.8A CN201910197272A CN109927924A CN 109927924 A CN109927924 A CN 109927924A CN 201910197272 A CN201910197272 A CN 201910197272A CN 109927924 A CN109927924 A CN 109927924A
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- photographic device
- driving structure
- horizontal plane
- phase unit
- rotation
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Abstract
This application discloses a kind of aviation oblique photograph holder, including phase unit and control phase unit at least 150 ° of rotation of driving structure along the horizontal plane；Phase unit includes the axes of rotation skew setting of optical axis and driving structure, and is connected to the first photographic device of driving structure, and be connected to the second photographic device of driving structure.Before phase unit along the horizontal plane rotation, make the angle between the optical axis of the second photographic device and the shaft of driving structure, the angle being adjusted between the optical axis of the first photographic device and the shaft of driving structure is equal.First photographic device and the second photographic device carry out the acquisition of inclination image when driving structure controls the rotation along the horizontal plane of phase unit.It only needs two photographic devices while half rotation, carries out filming image, oblique photograph can be completed, reduce the quantity of photographic device, so that reducing holder manufacturing cost while guaranteeing the operating efficiency of aviation oblique photograph holder and reducing holder volume.
Description
Technical field
This application involves technical field more particularly to a kind of aviation oblique photograph holders of taking photo by plane.
Background technique
It is existing inclination image acquisition, be by the camera of four different directions in independent photographic platform, it is right respectively
Different angle carries out image collection, to realize the acquisition of inclination image.But inclination image collection is being carried out using the prior art
Shi Faxian, since the camera and sensor of carrying are too many, so that holder for aerial photographing there are volumes big, complicated in mechanical structure and quality are big
The shortcomings that, influence aircraft cruise duration.
Summary of the invention
The embodiment of the present application technical problem to be solved is, how in the operation effect for guaranteeing aviation oblique photograph holder
While rate, reduces holder manufacturing cost and reduce holder volume.
To solve the above problems, the embodiment of the present application provides a kind of aviation oblique photograph holder, comprising: the phase for shooting
Unit, for controlling the phase unit at least 150 ° of rotation of driving structure along the horizontal plane；
The phase unit includes the axes of rotation skew setting of optical axis and the driving structure, and is connected to the driving structure
First photographic device, and it is connected to the second photographic device of the driving structure；
First photographic device and second photographic device are respectively used to, and control the camera in the driving structure
When organizing rotation along the horizontal plane, it is based on preset shooting interval, shoots multiple images；
Second photographic device is also used to, in the phase unit not rotation along the horizontal plane, segmentum intercalaris when being based on preset
Optical axis and the shaft of the driving structure are vertically arranged, and shoot image by point.
Further, the shooting interval includes time interval；
First photographic device and second photographic device are respectively used to, and control the camera in the driving structure
When group carries out the rotation of single direction along the horizontal plane, it is based on the time interval, shoots multiple images；
Or,
During the driving structure controls the first direction rotation of the phase unit along the horizontal plane, when being based on described
Between be spaced, shoot multiple images, and after phase unit reset, control the phase unit along the horizontal plane in the driving structure
Second direction rotation during, be based on the time interval, shoot multiple images；Wherein, the first direction and described
Second direction it is oppositely oriented.
Further, the shooting interval includes angle interval；
First photographic device and second photographic device are respectively used to, and control the camera in the driving structure
When group carries out the rotation of single direction along the horizontal plane, it is based on the angle interval, shoots multiple images；
Or,
During the driving structure controls the first direction rotation of the phase unit along the horizontal plane, it is based on the angle
Degree interval shoots multiple images, and after phase unit reset, controls the phase unit along the horizontal plane in the driving structure
Second direction rotation during, be based on the angle interval, shoot multiple images；Wherein, the first direction and described
Second direction it is oppositely oriented.
Further, further includes: rotatable platform, the main shaft of the driving structure are connected to the rotatable platform；
The rotatable platform is connect with the phase unit；
The driving structure is used for, and when meeting preset drive condition, controls rotatable platform rotation along the horizontal plane
At least 150 °, drive the phase unit rotation along the horizontal plane.
Further, the drive condition includes preset coordinate point；
The driving structure is specifically used for, when the aviation oblique photograph holder is located at the preset coordinate point, control
The rotatable platform at least 150 ° of rotation along the horizontal plane, drive the phase unit rotation along the horizontal plane.
Further, the drive condition includes preset duration；
The driving structure is specifically used for, when the runing time of the aviation oblique photograph holder reaches preset duration,
The rotatable platform at least 150 ° of rotation along the horizontal plane are controlled, the phase unit rotation along the horizontal plane is driven.
Further, the angle between the optical axis of first photographic device and the shaft of the driving structure be 35 °~
55°。
It further, further include inclining rotary mechanism；
The inclining rotary mechanism includes bracket and the frame that verts, and the bracket is fixedly connected on the driving structure, described to incline
The side for turning frame is rotationally connected with the bracket, and the frame that verts is socketed on second photographic device.
It further, further include the steering engine that verts for being connected to the driving structure, the main shaft of the steering engine that verts is connected to
Second photographic device.
It further, at least further include pedestal；
The rotatable platform is rotationally connected with the pedestal；
The driving structure is arranged on the pedestal.
Implement the embodiment of the present application, has the following beneficial effects:
A kind of aviation oblique photograph holder provided by the embodiments of the present application, including phase unit and control phase unit are along the horizontal plane
The driving structure that at least 150 ° of rotation；Phase unit includes the axes of rotation skew setting of optical axis and driving structure, and is connected to driving knot
First photographic device of structure, and it is connected to the second photographic device of driving structure.Before phase unit along the horizontal plane rotation, make
Angle between the optical axis of second photographic device and the shaft of driving structure is adjusted to and the optical axis of the first photographic device and driving
Angle between the shaft of structure is equal.First photographic device and the second photographic device are horizontal on driving structure control phase unit edge
When the rotation of face, the acquisition of inclination image is carried out.Compared with prior art, the application only needs two photographic devices in half rotation
Meanwhile filming image is carried out, oblique photograph can be completed, reduce the quantity of photographic device, so that being taken the photograph guaranteeing that aviation tilts
While the operating efficiency of shadow holder, reduces holder manufacturing cost and reduce holder volume.
Detailed description of the invention
Fig. 1 is the perspective view of the explosion for the panorama holder for aerial photographing that one embodiment of the application provides；
Fig. 2 is the perspective view of the explosion for the panorama holder for aerial photographing that another embodiment of the application provides；
Fig. 3 is the schematic layout pattern of the phase unit for the panorama holder for aerial photographing that one embodiment of the application provides；
Fig. 4 is the perspective view of the explosion for the panorama holder for aerial photographing that another embodiment of the application provides；
Fig. 5 is the perspective view of the explosion for the panorama holder for aerial photographing that the further embodiment of the application provides；
Fig. 6 is the elevational schematic view for the panorama holder for aerial photographing that one embodiment of the application provides；
Fig. 7 is the structural schematic diagram of the recessing groove for the panorama holder for aerial photographing that one embodiment of the application provides；
Fig. 8 is the structural schematic diagram of the relief hole for the panorama holder for aerial photographing that one embodiment of the application provides；
Fig. 9 is the structural schematic diagram of the carry part for the panorama holder for aerial photographing that one embodiment of the application provides.
Wherein, 1, driving structure；2, the first photographic device；3, the second photographic device；4, inclining rotary mechanism；5, vert steering engine；
6, pedestal；7, shell；8, carry part；11, rotatable platform；21, bracket；22, vert frame；31, relief hole；32, recessing groove；
41, clamping block.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present application, technical solutions in the embodiments of the present application carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of embodiments of the present application, instead of all the embodiments.It is based on
Embodiment in the application, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall in the protection scope of this application.
It is the perspective view of the explosion of the aviation oblique photograph holder of one embodiment offer of the application referring to Fig. 1, comprising:
For the phase unit of shooting, for controlling phase unit at least 150 ° of rotation of driving structure 1 along the horizontal plane.
Phase unit includes the axes of rotation skew setting of optical axis and driving structure, and is connected to the first camera shooting dress of driving structure 1
2 are set, and is connected to the second photographic device 3 of driving structure.
Wherein, the angle between the optical axis of the first photographic device 2 and the shaft of driving structure 1 is the first angle.
Second photographic device 3 is used for before phase unit along the horizontal plane rotation, by the optical axis of the second photographic device 3 and drive
Angle between the shaft of dynamic structure 1, is adjusted to second angle equal with the first angle.
First photographic device 2 and the second photographic device 3 are respectively used to, and control phase unit along the horizontal plane certainly in driving structure 1
When turning, it is based on preset shooting interval, shoots multiple images.
In the present embodiment, the first photographic device 2 is fixedly connected on driving structure 1, and the second photographic device 3 is movably connected on
Driving structure 1.
In the present embodiment, it the focal length of the optical element (i.e. camera lens) of the first photographic device 2 and the second photographic device 3 or waits
Effect focal length is equal, and the focal length or equivalent focal length of the two are 10mm~35mm, preferably 25mm, in order to image processing arrangement pair
Multiple images are spliced.
In the present embodiment, in order to ensure the counterweight of holder balances, the light of the first photographic device 2 and the second photographic device 3
Axis is coplanar, which is conducive to the image of the first photographic device 2 acquisition and the later period of the image of the second photographic device 3 acquisition spells
It connects.
In the present embodiment, driving structure 1 can be, but not limited to as steering engine.
In the present embodiment, when the holder is mounted on the bottom of aircraft, the axis vertical of driving structure 1 is set in ground
It sets.Before carrying out oblique photograph, the angle between its optical axis and the shaft of driving structure 1 is adjusted to by the second photographic device 3
Second angle equal with the first angle.After the second photographic device 3 completes angle adjustment, driving structure 1 controls phase unit edge
Horizontal plane rotation, the first photographic device 2 and the second photographic device 3 are completed during rotation to aircraft obliquely downward at this time
The full-view image at visual angle acquires, and then completes oblique photograph.
As a preferable examples of the present embodiment, the first photographic device 2 and the preset shooting interval of the second photographic device 3
Including time interval.When the control phase unit of driving structure 1 carries out the rotation of single direction along the horizontal plane, the first photographic device 2
It is based on time interval with the second photographic device 3, shoots multiple images.It is carried out along the horizontal plane or, controlling phase unit in driving structure 1
When the rotation of single direction, the first photographic device 2 and the second photographic device 3 are based on angle interval, shoot multiple images.
By above-mentioned rotating manner, inswept 180 ° of the model of optical axis of the first photographic device 2 and the second photographic device 3 is realized
It encloses.
When driving structure 1 controls the single direction of phase unit along the horizontal plane and rotated around the shaft of driving structure 1, lead to
The time interval for crossing setting N seconds makes the first photographic device 2 and the second photographic device 3 every N seconds progress once photo takings, until phase
Unit completes 180 ° of rotation.
It should be noted that specific interval time can need to be configured according to shooting.The rotation of single direction can be with
It is to the right or to turn left 180 °.
As another preferable examples of the present embodiment, between the first photographic device 2 and the preset shooting of the second photographic device 3
Every including angle interval.
When the control phase unit of driving structure 1 carries out the rotation of single direction along the horizontal plane, the first photographic device 2 and second
Photographic device 3 is based on angle interval, shoots multiple images.
It is primary every 45 ° of shootings when the first photographic device 2 and the second photographic device 3 are shot based on angle interval.
Therefore, when driving structure 1 completes 180 ° of rotations, the first photographic device 2 and one circle of the second photographic device 3 rotation shoot 8 figures altogether
Picture.
It should be noted that time interval and angle interval are the preferable examples of the present embodiment, other art technologies
The setting means of the common shooting interval of personnel is not described here any more.
Further, referring to fig. 2, be the application another embodiment provide panorama holder for aerial photographing explosion signal
Figure.In addition to the structure shown in Fig. 1, further includes: rotatable platform 11.
The main shaft of driving structure 1 is connected to rotatable platform 11.
Rotatable platform 11 is connect with phase unit.
Driving structure 1 is used for, and when meeting preset drive condition, rotation is at least along the horizontal plane for control rotatable platform 11
150 °, drive the rotation along the horizontal plane of phase unit.
In the present embodiment, drive condition can be high to be equipped with the preset flight of the aircraft of the panorama holder for aerial photographing
Degree, position, flight path and flying speed etc..
Due to rotatable platform 11 can at least 150 ° of rotation along the horizontal plane, drive the rotation along the horizontal plane of phase unit, therefore only need
The first photographic device 2 and the second photographic device 3, which is arranged, just can acquire the image at multiple visual angles, avoid as in the prior art in cloud
The photographic goods that multiple shooting different directions are arranged on platform reduce holder cost to control the self weight of holder.
In the present embodiment, the first photographic device 2 and the second photographic device 3 are located at the two of the shaft of rotatable platform 11
Side, and the radial outside of the imaging region of the first photographic device 2 against rotatable platform 11 is arranged, and then avoids the second photographic device 3
It is interfered after verting with the first photographic device 2.
In the present embodiment, as a preferable examples, the drive condition of driving structure 1 includes preset coordinate point.It is navigating
When empty oblique photograph holder is located at the preset coordinate point, driving structure 1 controls at least 150 ° of rotation along the horizontal plane of rotatable platform 11,
Drive the rotation along the horizontal plane of phase unit.By preset coordinate point, realize that the fixed point of holder is taken pictures.
As another preferable examples of the present embodiment, the drive condition of driving structure 1 further includes preset duration.In aviation
The runing time of oblique photograph holder reaches preset duration, or connects the aircraft runing time of the aviation oblique photograph holder and reach
When to preset duration, driving structure 1 controls at least 150 ° of rotation along the horizontal plane of rotatable platform 11, drive phase unit along the horizontal plane from
Turn.By preset duration, realize that the timing of holder is taken pictures.
It should be noted that preset coordinate point and preset duration are the preferable examples of the present embodiment, other this field skills
The common drive condition setting mode of art personnel is not described here any more.
In the present embodiment, the second photographic device 3 is movably connected on rotatable platform 11, the optical axis energy of the second photographic device 3
It is enough to be swung on perpendicular, therefore the second photographic device 3 is relatively rotatable to each other platform 11 and verts, so as to adjust the second camera shooting dress
The angle between 3 optical axis and the shaft of rotatable platform 11 is set, to carry out the image collection at multiple visual angles.
It preferably, is the integrality for guaranteeing image, the first angle is set as 35 °~55 °.Preferably 45 °, i.e., at this time second
Angle is also 45 °, so that the first photographic device 2 and the second photographic device 3 complete the full-view image to aircraft 45 ° of visual angles obliquely downward
Acquisition, it is ensured that the integrality of image.
In the present embodiment, as shown in figure 3, further including inclining rotary mechanism 4.Inclining rotary mechanism 4 includes bracket 21 and the frame that verts
22, bracket 21 is fixedly connected on driving structure 1, and the side for the frame 22 that verts is rotationally connected with bracket 21, the frame 22 that verts socket
On the second photographic device 3.
As shown in figure 3, the frame 22 that verts is socketed in the side of the second photographic device 3, the frame 22 that verts is rotationally connected with branch
The free end of frame 21, the fixing end of bracket 21 are fixedly connected on rotatable platform 11.
It further, referring to fig. 4, is that the explosion of aviation oblique photograph holder that provides of another embodiment of the application is shown
It is intended to.It further include the steering engine 5 that verts for being connected to driving structure 1, the main shaft for the steering engine 5 that verts is connected in addition to the structure shown in Fig. 1-3
Second photographic device 3.
In the present embodiment, the steering engine 5 that verts is set on the stent 21, and the main shaft for the steering engine 4 that verts is connected to the frame 22 that verts.
The steering engine 5 that verts is used for, before meeting drive condition, by the optical axis of the second photographic device 3 and rotatable platform 11
Angle between shaft is adjusted to second angle equal with the first angle.
The driving that the second photographic device is carried out using the steering engine 5 that verts, can make entire aviation oblique photograph holder volume will not
While excessive, achieve the purpose that oblique photograph.
It further, is that the explosion of the aviation oblique photograph holder of another embodiment offer of the application is shown referring to Fig. 5
It is intended to.It further include pedestal 6, shell 7 and carry part 8 in addition to the structure shown in Fig. 1-4.
Rotatable platform 11 is rotationally connected with pedestal 6, and driving structure 1 is arranged on pedestal 6.Shell 7 be located in rotatable platform
On 11, carry part 8 is additionally provided on pedestal 6.
Specifically, as shown in figs 6-8, shell 7 be located on rotatable platform 11, and bracket 21, the frame 22 that verts, vert rudder
Machine 5, the first photographic device 2 and the second photographic device 3 are respectively positioned in shell 7.It is offered on shell 7 for by the first photographic device
2 optical element (i.e. camera lens) is exposed to extraneous relief hole 31 and for by optical element (the i.e. mirror of the second photographic device 3
Head) it is exposed to extraneous recessing groove 32.
Pedestal 4 is equipped with driving structure 1, and the main shaft of driving structure 1 is connected to rotatable platform 11, to drive rotatable platform 11
Opposite base 4 rotates.Carry part 8 is additionally provided on pedestal 4.As shown in figure 9, the outer peripheral surface of carry part 8 is equipped with multiple for connecting
It is connected to the clamping block 41 of aircraft.
In the present embodiment, pedestal 4 and shell 7 can be, but not limited to be made of PC+GF30.
The embodiment of the present application provides a kind of aviation oblique photograph holder, including phase unit and control phase unit along the horizontal plane from
Go to few 150 ° of driving structure；Phase unit includes the axes of rotation skew setting of optical axis and driving structure, and is fixedly connected on driving
First photographic device of structure, and it is movably connected on the second photographic device of driving structure.In the rotation along the horizontal plane of phase unit
Before, make the angle between the optical axis of the second photographic device and the shaft of driving structure, be adjusted to the light with the first photographic device
Angle between axis and the shaft of driving structure is equal, and the first photographic device and the second photographic device are in driving structure control camera
When organizing rotation along the horizontal plane, the acquisition of inclination image is carried out.Compared with prior art, the application only needs two photographic devices revolving
While turning half-turn, filming image is carried out, oblique photograph can be completed, reduce the quantity of photographic device, so that guaranteeing to navigate
While the operating efficiency of empty oblique photograph holder, reduces holder manufacturing cost and reduce holder volume.
In the description of the present application, it should be noted that the orientation or position of the instructions such as term " on ", "lower", "inner", "outside"
Set relationship be based on the orientation or positional relationship shown in the drawings or this application product using when the orientation or position usually put
Relationship is set, description the application is merely for convenience of and simplifies description, rather than the device or element of indication or suggestion meaning are necessary
It with specific orientation, is constructed and operated in a specific orientation, therefore should not be understood as the limitation to the application.
In addition, term " first ", " second ", " third " etc. are only used for distinguishing description, it is not understood to indicate or imply
Relative importance.
In the description of the present application, it is also necessary to which explanation is unless specifically defined or limited otherwise, term " setting ",
" installation ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally connect
It connects；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, can also indirectly connected through an intermediary, it can
To be the connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood with concrete condition
Concrete meaning in this application.The above is the preferred embodiment of the application, it is noted that for the art
For those of ordinary skill, under the premise of not departing from the application principle, several improvements and modifications can also be made, these improvement
Also it is considered as the protection scope of the application with retouching.
Claims (9)
1. a kind of aviation oblique photograph holder characterized by comprising for the phase unit of shooting, for controlling the camera
Organize at least 150 ° of rotation along the horizontal plane of driving structure；
The phase unit includes the axes of rotation skew setting of optical axis and the driving structure, and is connected to the first of the driving structure
Photographic device, and it is connected to the second photographic device of the driving structure；Wherein, the optical axis of first photographic device and institute
Stating the angle between the shaft of driving structure is the first angle；
Second photographic device is used for before the phase unit along the horizontal plane rotation, by the light of second photographic device
Angle between axis and the shaft of the driving structure is adjusted to second angle equal with first angle；
First photographic device and second photographic device are respectively used to, and control phase unit edge in the driving structure
When horizontal plane rotation, it is based on preset shooting interval, shoots multiple images.
2. aviation oblique photograph holder according to claim 1, which is characterized in that the shooting interval includes time interval
With angle interval；
First photographic device and second photographic device are respectively used to, and control phase unit edge in the driving structure
When horizontal plane carries out the rotation of single direction, it is based on the time interval, shoots multiple images；
Or,
When the driving structure controls the phase unit and carries out the rotation of single direction along the horizontal plane, based between the angle
Every shooting multiple images.
3. aviation oblique photograph holder according to claim 1, which is characterized in that further include: rotatable platform, the driving
The main shaft of structure is connected to the rotatable platform；
The rotatable platform is connect with the phase unit；
The driving structure is used for, and when meeting preset drive condition, controlling the rotatable platform, rotation is at least along the horizontal plane
150 °, drive the phase unit rotation along the horizontal plane.
4. aviation oblique photograph holder according to claim 3, which is characterized in that the drive condition includes preset coordinate
Point；
The driving structure is specifically used for, when the aviation oblique photograph holder is located at the preset coordinate point, described in control
Rotatable platform at least 150 ° of rotation along the horizontal plane, drive the phase unit rotation along the horizontal plane.
5. aviation oblique photograph holder according to claim 3, which is characterized in that when the drive condition includes default
It is long；
The driving structure is specifically used for, when the runing time of the aviation oblique photograph holder reaches preset duration, control
The rotatable platform at least 150 ° of rotation along the horizontal plane, drive the phase unit rotation along the horizontal plane.
6. aviation oblique photograph holder according to claim 3, which is characterized in that further include being connected to the driving structure
The steering engine that verts, the main shaft of the steering engine that verts is connected to second photographic device；
The steering engine that verts is used for, before meeting the drive condition, by the optical axis of second photographic device and described turn
Angle between the shaft of moving platform is adjusted to second angle.
7. a kind of aviation oblique photograph holder according to claim 3, which is characterized in that at least further include pedestal；
The rotatable platform is rotationally connected with the pedestal；
The driving structure is arranged on the pedestal.
8. aviation oblique photograph holder described in -7 any one according to claim 1, which is characterized in that first angle is
35 °~55 °.
9. aviation oblique photograph holder described in -7 any one according to claim 1, which is characterized in that further include the machine that verts
Structure；
The inclining rotary mechanism includes bracket and the frame that verts, and the bracket is fixedly connected on the driving structure, the frame that verts
The side of frame is rotationally connected with the bracket, and the frame that verts is socketed on second photographic device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910197272.8A CN109927924A (en) | 2019-03-14 | 2019-03-14 | Aviation oblique photograph holder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910197272.8A CN109927924A (en) | 2019-03-14 | 2019-03-14 | Aviation oblique photograph holder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109927924A true CN109927924A (en) | 2019-06-25 |
Family
ID=66987180
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910197272.8A Pending CN109927924A (en) | 2019-03-14 | 2019-03-14 | Aviation oblique photograph holder |
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| CN (1) | CN109927924A (en) |
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Application publication date: 20190625 |