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 PDF

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Publication number
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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CN
China
Prior art keywords
camera
visual angle
eyeglass
lens set
image
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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.)
Pending
Application number
CN201710542722.3A
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Chinese (zh)
Inventor
徐鹏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GUANGZHOU REDBIRD HELICOPTER REMOTE SENSING TECHNOLOGY Co Ltd
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GUANGZHOU REDBIRD HELICOPTER REMOTE SENSING TECHNOLOGY Co Ltd
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Publication of CN107329363A publication Critical patent/CN107329363A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03BAPPARATUS 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
    • G03B17/00Details of cameras or camera bodies; Accessories therefor
    • G03B17/02Bodies
    • G03B17/17Bodies with reflectors arranged in beam forming the photographic image, e.g. for reducing dimensions of camera
    • GPHYSICS
    • G03PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03BAPPARATUS 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
    • G03B37/00Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe
    • G03B37/04Panoramic 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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C11/00Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
    • G01C11/02Picture taking arrangements specially adapted for photogrammetry or photographic surveying, e.g. controlling overlapping of pictures
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C11/00Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/18Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
    • G02B7/182Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
    • G02B7/1821Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors for rotating or oscillating mirrors
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/18Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
    • G02B7/182Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
    • G02B7/198Mountings, 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
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/50Constructional details
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/50Constructional details
    • H04N23/55Optical parts specially adapted for electronic image sensors; Mounting thereof

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  • 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

A kind of method of six visual angle oblique photographs of double camera for airborne vehicle
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.
CN201710542722.3A 2017-04-25 2017-07-05 A kind of method of six visual angle oblique photographs of double camera for airborne vehicle Pending CN107329363A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN2017102778590 2017-04-25
CN201710277859 2017-04-25

Publications (1)

Publication Number Publication Date
CN107329363A true CN107329363A (en) 2017-11-07

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Family Applications (40)

Application Number Title Priority Date Filing Date
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CN201710551944.1A Pending CN107367887A (en) 2017-04-25 2017-07-05 A kind of one camera rotating disk oblique photograph device for airborne vehicle
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CN107367265A (en) 2017-11-21
CN207113869U (en) 2018-03-16
CN207113871U (en) 2018-03-16
CN107367266A (en) 2017-11-21
CN107390451A (en) 2017-11-24

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