CN107329363A - A kind of method of six visual angle oblique photographs of double camera for airborne vehicle - Google Patents
A kind of method of six visual angle oblique photographs of double camera for airborne vehicle Download PDFInfo
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- CN107329363A CN107329363A CN201710542722.3A CN201710542722A CN107329363A CN 107329363 A CN107329363 A CN 107329363A CN 201710542722 A CN201710542722 A CN 201710542722A CN 107329363 A CN107329363 A CN 107329363A
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- 230000000007 visual effect Effects 0.000 title claims abstract description 104
- 238000000034 method Methods 0.000 title claims abstract description 23
- 238000010586 diagram Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- VMXUWOKSQNHOCA-UKTHLTGXSA-N ranitidine Chemical compound [O-][N+](=O)\C=C(/NC)NCCSCC1=CC=C(CN(C)C)O1 VMXUWOKSQNHOCA-UKTHLTGXSA-N 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Classifications
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- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B17/00—Details of cameras or camera bodies; Accessories therefor
- G03B17/02—Bodies
- G03B17/17—Bodies with reflectors arranged in beam forming the photographic image, e.g. for reducing dimensions of camera
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B37/00—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe
- G03B37/04—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe with cameras or projectors providing touching or overlapping fields of view
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
- G01C11/02—Picture taking arrangements specially adapted for photogrammetry or photographic surveying, e.g. controlling overlapping of pictures
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
- G02B7/1821—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors for rotating or oscillating mirrors
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
- G02B7/198—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors with means for adjusting the mirror relative to its support
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
- H04N23/55—Optical parts specially adapted for electronic image sensors; Mounting thereof
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Multimedia (AREA)
- Aviation & Aerospace Engineering (AREA)
- Optics & Photonics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Signal Processing (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
- Stereoscopic And Panoramic Photography (AREA)
Abstract
The invention provides a kind of method of six visual angle oblique photographs of double camera for airborne vehicle, first camera, second camera are fixed on aircraft, including:S1, the front that the first lens set is arranged on to first camera;Second lens set is arranged on to the front of second camera;S2, airborne vehicle reach target location, and the image at the first visual angle is shot by first camera, and the image at the second visual angle is shot by second camera;S3, the first lens set of adjustment, the state of the second lens set, the image at the 3rd visual angle is shot by first camera, the image at the 4th visual angle is shot by second camera;S4, the first lens set, the state of the second lens set are adjusted again, the image at the 5th visual angle is shot by first camera, pass through the image that second camera shoots the 6th visual angle;Complete the image taking at six visual angles in target location;Camera negligible amounts of the present invention, weight of equipment and small volume, cost are relatively low, and operating efficiency is higher.
Description
Technical field
The present invention relates to a kind of method of six visual angle oblique photographs of double camera for airborne vehicle.
Background technology
Airborne inclined photography is the high-new technology of taking photo by plane that international survey field grew up in recent years, and it passes through same
Many different sensors of camera angle are carried on one flying platform, to gather the aerial image of the different sides of atural object.
A kind of more oblique photograph device of current application has 5 camera lenses composition, wherein 1 camera lens it is vertical to
Under, other 4 camera lens respectively forwardly, rear, left and right four direction tilt.When camera works, 5 camera lenses and non-concurrent exposure
Light, but exposed successively according to certain order, exposure interval is generally less than 1 second, and one group of exposure will typically continue several seconds, different
Degree of overlapping sets the different exposure order of generation.Because 5 camera lens have suitable weight, it is unfavorable for flying for airborne vehicle
OK.
The aviation oblique photograph device used at present generally uses multiple built-in cameras, by putting for different angles, real
Existing multiple angle shots, to obtain the panoramic picture on ground.In order to reduce main screw lift and cost, generally using the built-in phase of rotation
Machine realizes multi-angled shooting, to reduce built-in camera quantity.Because the volume and weight of built-in camera itself is larger, meeting during rotation
Cause complete machine vibrations also larger, while also increasing the consumption of electricity, be unfavorable for aeroplane photography.
The defect of above-mentioned technical proposal is:
1st, installation weight is larger, and complete machine vibrations are obvious;
2nd, camera rotational structure is complicated, and precision is low, poor reliability;
3rd, camera rotation period is long, and under the requirement of certain Duplication, shooting efficiency and quality can decline.
The content of the invention
In view of the shortcomings of the prior art, the present invention provides a kind of six visual angle oblique photographs of double camera for airborne vehicle
Method, realizes from the earthward shooting of six direction in the air, enriches the application of product, and its shooting efficiency is high, reliable
Property it is strong, more adapt to aeroplane photography.
To achieve these goals, the invention provides a kind of six visual angle oblique photographs of double camera for airborne vehicle
Method, first camera, second camera are fixed on aircraft, and it includes:
S1, the front that the first lens set is arranged on to first camera;Second lens set is arranged on to the front of second camera;
S2, airborne vehicle reach target location, and first camera shoots the image at the first visual angle, and second camera shoots the second visual angle
Image;
S3, the first lens set of adjustment, the second lens set, first camera shoot the image at the 3rd visual angle, and second camera is shot
The image at the 4th visual angle;
S4, adjust the first lens set, the second lens set again, first camera shoots the image at the 5th visual angle, second camera
Shoot the image at the 6th visual angle;Complete the shooting at six visual angles in target location.
First visual angle, the second visual angle, the 3rd visual angle, the 4th visual angle, the 5th visual angle, the shooting angle not phase at the 6th visual angle
Together.
In the present invention, by the adjustable lens set of installation space angle before camera lens, different angles are obtained
Incident light source, in the case where first camera, second camera are fixed, by adjusting the state of lens set, first camera, the second phase
Machine obtains the incident light source of six different angles, realizes from the earthward shooting of six angles in the air.
Camera negligible amounts of the present invention, reduce the overall weight of equipment and reduce the volume of equipment, reduce production
Manufacturing cost, improves the efficiency of shooting;By setting lens set, make camera in the case of fixation i.e. can be achieved from the air to
The shooting of underground multi-angle, the problem of greatly reducing due to camera rotational band next low precision is more suitable for aviation inclination and taken the photograph
Shadow.
According to another embodiment of the present invention, six visual angles are left front visual angle, lower-left visual angle, left back visual angle, the right side
Preceding visual angle, bottom right visual angle, right back angle.For example, front and rear three row, the layout of the row of left and right two, wherein, left front visual angle and right preceding visual angle
The filmed image in direction overlaps, and the filmed image of lower-left visual angle and bottom right view directions overlaps, left front visual angle
Overlapped with the filmed image of view directions before the right side.
According to another embodiment of the present invention, the first lens set includes the first eyeglass;Second lens set includes the
Two eyeglasses.First eyeglass is along the rotatable certain angle of a certain bar axis, and the second eyeglass is rotatable certain along a certain bar axis
Angle, the first eyeglass, the second eyeglass are in rotary course, and its own position is relatively free of obvious change.
According to another embodiment of the present invention, the first eyeglass can be located to pitch rotation the front of first camera;
Second eyeglass can roll be rotationally located at the front of second camera.First eyeglass is always positioned at first in pitching rotary course
The front of camera, can provide the incident ray at multiple ground visual angles for first camera;Second eyeglass in roll rotation process,
The front of second camera is always positioned at, the incident ray at multiple ground visual angles can be provided for second camera.
According to another embodiment of the present invention, the first eyeglass pitch rotation, second mirror in default first plane
Piece roll in default second plane is rotated, and has certain angle between the first preset plane, the second preset plane.It is preferred that,
Angle is 90 degree.
According to another embodiment of the present invention, the first eyeglass can be located to pitch rotation the front of first camera;
Second eyeglass is located at the front of second camera in which can horizontally rotate.First eyeglass is always positioned at first in pitching rotary course
The front of camera, can provide the incident ray at multiple ground visual angles for first camera;Second eyeglass during horizontally rotating,
The front of second camera is always positioned at, the incident ray at multiple ground visual angles can be provided for second camera.
According to another embodiment of the present invention, by rotating the first eyeglass, the second eyeglass, the first eyeglass of adjustment,
The posture of second eyeglass, makes first camera, second camera obtain the shooting direction at six visual angles.Pass through the first eyeglass, the first phase
Machine and the second eyeglass, the cooperation of second camera, can obtain the incident ray of multiple ground-angles, change traditional aeroplane photography
The pattern directly directly shot using multiple cameras, is conducive to the development of oblique photograph and used.
According to another embodiment of the present invention, the first lens set includes the different eyeglass of three space angles, the
Two lens sets include the different eyeglass of three space angles.By in three eyeglasses and the second lens set of in the first lens set
Three eyeglasses, six shooting direction on ground can be provided for first camera, second camera, and then realize from the air earthward
The shooting of six angles.
According to another embodiment of the present invention, it is just right that the eyeglass in the first lens set is switched to by rotation mode
The position of camera;Eyeglass in second lens set switches to the position of straight-on camera by rotation mode.For example, the first eyeglass
Eyeglass in group, the second lens set is arranged on rotating disk, by rotating rotating disk, realizes the switching between eyeglass, it would be desirable to mirror
Piece switches to the position just to first camera.
According to another embodiment of the present invention, it is just right that the eyeglass in the first lens set is switched to by translation mode
The position of camera;Eyeglass in second lens set switches to the position of straight-on camera by translation mode.For example, the first eyeglass
Eyeglass in group, the second lens set is arranged on sliding block, by driving sliding block to be moved on slide rail, realizes cutting between eyeglass
Change, it would be desirable to eyeglass switch to position just to second camera.
According to another embodiment of the present invention, by the position for switching eyeglass in the first lens set, the second lens set
Put, first camera, second camera is obtained the shooting direction at six visual angles.For example, the first lens set, the second lens set interval are set
Put on same rotating disk, rotate rotating disk to initialization position, now first camera, second camera correspond to left front eyeglass respectively
With right front lens, the shooting of the angle position is carried out;After the completion of shooting, switch the eyeglass just to first camera, second camera, this
When first camera, second camera respectively just to lower-left eyeglass, bottom right eyeglass, carry out the shooting of the angle position;After the completion of shooting,
Switch the eyeglass just to first camera, second camera again, now first camera, second camera are respectively just to left back eyeglass, the right side
Rear lens, carries out the shooting of the angle position.The angle shot of the target location six is completed.
According to another embodiment of the present invention, the first lens set includes an adjustable eyeglass of space angle, the
Two lens sets include the different eyeglass of three space angles.Pass through an adjustable eyeglass of space angle in the first lens set and
Three eyeglasses in two lens sets, can provide six shooting direction on ground for first camera, second camera, so realize from
The earthward shooting of six angles in the air.
In the present invention, by being arranged on the first lens set before first camera, second camera and the second lens set, mesh is carried out
The visual angle of cursor position first, the second visual angle, the 3rd visual angle, the 4th visual angle, the shooting at the 5th visual angle and the 6th visual angle, wherein first regards
Angle, the second visual angle, the 3rd visual angle, the 4th visual angle, the 5th visual angle, the shooting angle at the 6th visual angle are differed, six visual angles point
Not Wei left front, lower-left, it is left back, right before, bottom right, right back to.
The present invention is advantageous in that:Pass through adjustable angle is set before first camera, second camera or multiple skies
Between the different eyeglass of angle, realize from the earthward shooting of six angles in the air, two fixed cameras have reached six cameras
Effect.Compared to traditional aviation oblique photograph mode, contribute to the weight of whole camera, be conducive to the hair of aeroplane photography
Exhibition;First camera, second camera fixed, and it is electrically connected, without motion, reduces failure risk, it is to avoid traditional approach is due to phase
The problem of poor image quality that machine rotational band is come, improve reliability.The change of angle of incident light is realized by eyeglass, shooting
Image is overlapped, it is possible to reduce Duplication of taking photo by plane requirement, increases the interval in course line, operating efficiency is improved, so as to more adapt to
Aeroplane photography.
The present invention is described in further detail below in conjunction with the accompanying drawings.
Brief description of the drawings
Fig. 1 is a kind of device of the method for six visual angle oblique photographs of double camera using for airborne vehicle of embodiment 1
Schematic diagram;
Fig. 2 is a kind of device of the method for six visual angle oblique photographs of double camera using for airborne vehicle of embodiment 2
Schematic diagram.
Embodiment
Embodiment 1
A kind of method of six visual angle oblique photographs of double camera for airborne vehicle is present embodiments provided, it includes as follows
Step:
S1, the front that the first lens set is located to first camera, it includes three different eyeglasses of space angle;By second
Lens set is arranged on the front of second camera, and it includes three different eyeglasses of space angle.
S2, airborne vehicle reach target location, and first camera shoots the image at the first visual angle, and second camera shoots the second visual angle
Image.The first visual angle that now first camera is shot is the image in left front direction, and the second visual angle that second camera is shot is the right side
The image of front direction.
S3, the position by eyeglass in rotation mode the first lens set of switching, first camera shoot the image at the 3rd visual angle,
Switch the position of eyeglass in the second lens set by rotation mode, second camera shoots the image at the 4th visual angle;Now the first phase
The 3rd visual angle that machine is shot is the image of lower left, and the 4th visual angle that second camera is shot is the image of lower right.
S4, the position for switching eyeglass in the first lens set again, first camera shoot the image at the 5th visual angle;Pass through rotation
Mode switches the position of eyeglass in the second lens set, and second camera shoots the image at the 6th visual angle;Now first camera is shot
5th visual angle be left back direction image, second camera shoot the 6th visual angle for right back to image;Complete target position
Put the shooting at six visual angles.
A kind of oblique photograph device for the method for realizing the present embodiment, as shown in figure 1, it includes:Pedestal and it is arranged on base
First camera 1, second camera 2 on seat, rotating disc type angle adjusting mechanism 3, the rudder for driving rotating disk formula angle adjusting mechanism
Machine 4;Wherein, first camera 1, second camera 2 are horizontal camera;Rotating disc type angle adjusting mechanism 3 includes six space angles
Different eyeglass 31, the rotating disk 32 driven by steering wheel 4, some connecting rods 33, eyeglass 31 are consistent with the number of connecting rod 33 and correspondingly
Set, rotating disk 32 is rotatably installed on pedestal, the one end of connecting rod 33 connection eyeglass 31, other end connection rotating disk 32;It is some
Connecting rod 33 is radially arranged on rotating disk 32;First camera 1, second camera 2 are oppositely arranged on the both sides of rotating disk 32;Steering wheel
4 connect rotating disk 32 by drive shaft 41;;
Wherein, the number of eyeglass 31 is 6, and the number of connecting rod 33 is also 6, and it is evenly distributed on rotating disk 32, adjacent
Angular separation between connecting rod 33 is 60 °;It is the first lens set 311, the second lens set 312, the first eyeglass by 6 31 points of eyeglasses
Group 311 includes left front, lower-left, the eyeglass 31 in left back three directions, the second lens set 312 include it is right before, bottom right, it is right after three sides
To eyeglass 32;Wherein left front eyeglass and right front lens are oppositely arranged on the both sides of rotating disk 32;Left back eyeglass and right rear lens phase
Both sides to being arranged on rotating disk 32;Lower-left eyeglass and bottom right eyeglass are oppositely arranged on the both sides of rotating disk 32.
By rotating rotating disk 32, switch the eyeglass 31 just to first camera 1, second camera 2, thus change first camera 1,
The shooting direction of second camera 2.
Embodiment 2
A kind of method of six visual angle oblique photographs of double camera for airborne vehicle is present embodiments provided, it includes as follows
Step:
S1, the front that the first eyeglass is located to first camera, the first eyeglass pitch rotation in the first preset plane;By
Two eyeglasses are arranged on the front of second camera, and the roll in the second preset plane of the second eyeglass is rotated;First preset plane, second
There are certain angle, such as 90 degree between preset plane.
S2, airborne vehicle reach target location, and first camera shoots the image at the first visual angle, and second camera shoots the second visual angle
Image.The first visual angle that now first camera is shot is the image in left front direction, and the second visual angle that second camera is shot is the right side
The image of front direction.
S3, the first eyeglass of rotation, the second eyeglass, the image at the 3rd visual angle is shot by first camera, and second camera is shot
The image at the 4th visual angle;The 3rd visual angle that now first camera is shot is the image of lower left, the 4th of second camera shooting the
Visual angle is the image of lower right.
S4, the first eyeglass, the second eyeglass are rotated again, pass through the image that first camera shoots the 5th visual angle, second camera
Shoot the image at the 6th visual angle;The 5th visual angle that now first camera is shot is the image in left back direction, what second camera was shot
6th visual angle be right back to image;Complete the shooting at six visual angles in target location.
A kind of oblique photograph device for the method for realizing the present embodiment, as shown in Fig. 2 it includes:First photographic unit 5,
Second photographic unit 6 and support 7.
Wherein, the first photographic unit 5 includes first camera 501, the first eyeglass 502 and the first motor 503;First motor
503 are used to drive the first eyeglass 502 to rotate;The front end of first camera 501 is provided with the first camera lens 504;First eyeglass 502 is located at first
The front of camera lens 504;First eyeglass 502 includes first rotating shaft (not shown).
Second photographic unit 6 includes second camera 601, the second eyeglass 602 and the second motor 603;Second motor 603 is used for
The second eyeglass 202 is driven to rotate;The front end of second camera 601 is provided with the second camera lens 604;Second eyeglass 602 is located at the second camera lens 604
Front;Second eyeglass 602 includes the second rotating shaft (not shown);First camera 501 and second camera 601 are horizontal camera;
The axis (not shown) of first camera lens 504 is mutually perpendicular to the axis (not shown) of the second camera lens 604, and positioned at same flat
Face;First rotating shaft is vertical with the second rotating shaft, and is respectively positioned on same plane.
Support 7 includes the first cantilever 701 and the second cantilever 702;First cantilever 701 and the second cantilever 702 intersect vertically, shape
Into " L " shape;First eyeglass 502 is rotatably coupled the free end of the first cantilever 701, and the second eyeglass 602 is rotatably coupled second
The free end of cantilever 702;First rotating shaft is conllinear with the first cantilever 701, and the second rotating shaft is conllinear with the second cantilever 702.
Although the present invention is disclosed above with preferred embodiment, the scope that the present invention is implemented is not limited to.Any
The those of ordinary skill in field, it is when a little improvement can be made, i.e., every according to this hair in the invention scope for not departing from the present invention
Bright done equal improvement, should be the scope of the present invention and is covered.
Claims (9)
1. a kind of method of six visual angle oblique photographs of double camera for airborne vehicle, first camera, second camera are fixed on institute
State on airborne vehicle, it is characterised in that methods described includes:
S1, the front that the first lens set is arranged on to the first camera;Second lens set is arranged on the second camera
Front;
S2, airborne vehicle reach target location, and the image at the first visual angle is shot by the first camera, passes through the second camera
Shoot the image at the second visual angle;
S3, adjustment first lens set, the state of second lens set, pass through the first camera and shoot the 3rd visual angle
Image, the image at the 4th visual angle is shot by the second camera;
S4, first lens set, the state of second lens set are adjusted again, shooting the 5th by the first camera regards
The image at angle, the image at the 6th visual angle is shot by the second camera;Complete the image taking at six visual angles in target location;
First visual angle, second visual angle, the 3rd visual angle, the 4th visual angle, the 5th visual angle, the described 6th
The shooting angle at visual angle is differed.
2. the method as described in claim 1, it is characterised in that six visual angles are left front visual angle, lower-left visual angle, left back regarded
Angle, right preceding visual angle, bottom right visual angle, right back angle.
3. the method as described in claim 1, it is characterised in that first lens set includes the first eyeglass;Second mirror
Piece group includes the second eyeglass.
4. method as claimed in claim 3, it is characterised in that first eyeglass can be located to pitch rotation first phase
The front of machine;Second eyeglass can roll be rotationally located at the front of the second camera.
5. method as claimed in claim 4, it is characterised in that by rotating first eyeglass, second eyeglass, adjustment
The posture of first eyeglass, second eyeglass, makes the first camera, the second camera obtain the shooting at six visual angles
Direction.
6. the method as described in claim 1, it is characterised in that first lens set includes the different mirror of three space angles
Piece, second lens set includes the different eyeglass of three space angles.
7. method as claimed in claim 6, it is characterised in that the eyeglass in first lens set is switched by rotation mode
To the position of straight-on camera;Eyeglass in second lens set switches to the position of straight-on camera by rotation mode.
8. method as claimed in claim 6, it is characterised in that the eyeglass in first lens set is switched by translation mode
To the position of straight-on camera;Eyeglass in second lens set switches to the position of straight-on camera by translation mode.
9. method as claimed in claim 7 or 8, it is characterised in that by switching first lens set, second eyeglass
The position of eyeglass in group, makes the first camera, the second camera obtain the shooting direction at six visual angles.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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CN2017102778590 | 2017-04-25 | ||
CN201710277859 | 2017-04-25 |
Publications (1)
Publication Number | Publication Date |
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CN107329363A true CN107329363A (en) | 2017-11-07 |
Family
ID=60196799
Family Applications (40)
Application Number | Title | Priority Date | Filing Date |
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CN201720809625.1U Expired - Fee Related CN207181921U (en) | 2017-04-25 | 2017-07-05 | A kind of shaft type lens supports for camera multi-angled shooting |
CN201710542036.6A Pending CN107340671A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
CN201720809536.7U Expired - Fee Related CN207360596U (en) | 2017-04-25 | 2017-07-05 | A kind of opposed double camera rotating disc type oblique photograph device for aircraft |
CN201720809495.1U Expired - Fee Related CN207366911U (en) | 2017-04-25 | 2017-07-05 | A kind of reflective twin-lens bi-axial tilt camera for aircraft |
CN201710542723.8A Pending CN107449401A (en) | 2017-04-25 | 2017-07-05 | The implementation method that a kind of multi-angle oblique for airborne vehicle is photographed |
CN201710542576.4A Pending CN107390453A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens bi-axial tilt camera for airborne vehicle |
CN201720809561.5U Expired - Fee Related CN207742455U (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens bi-axial tilt camera for aircraft |
CN201710542329.4A Pending CN107390451A (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
CN201710542703.0A Pending CN107390469A (en) | 2017-04-25 | 2017-07-05 | A kind of polyphaser camera for airborne vehicle |
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CN201720809625.1U Expired - Fee Related CN207181921U (en) | 2017-04-25 | 2017-07-05 | A kind of shaft type lens supports for camera multi-angled shooting |
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CN201710542643.2A Pending CN107560602A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
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CN201710542051.0A Pending CN107561831A (en) | 2017-04-25 | 2017-07-05 | The implementation method that a kind of one camera multi-angle oblique for airborne vehicle is photographed |
CN201720809475.4U Expired - Fee Related CN207106926U (en) | 2017-04-25 | 2017-07-05 | A kind of double camera oblique photograph device for airborne vehicle |
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