CN107643649A - A kind of implementation method of nine visual angle oblique photographs for airborne vehicle - Google Patents
A kind of implementation method of nine visual angle oblique photographs for airborne vehicle Download PDFInfo
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- CN107643649A CN107643649A CN201710542741.6A CN201710542741A CN107643649A CN 107643649 A CN107643649 A CN 107643649A CN 201710542741 A CN201710542741 A CN 201710542741A CN 107643649 A CN107643649 A CN 107643649A
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- 238000005516 engineering process Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
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- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
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Classifications
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- 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
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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
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- 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
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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
- 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
-
- 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)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Optics & Photonics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Signal Processing (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
- Stereoscopic And Panoramic Photography (AREA)
Abstract
The present invention provides a kind of implementation method of nine visual angle oblique photographs for airborne vehicle, and first camera, second camera, third camera are fixed on aircraft, including:S1, airborne vehicle reach target location, the first lens set are switched into operating position, first camera, second camera, third camera shoot the image of first direction by the first lens set;First direction includes three visual angles;S2, switch the image that the second lens set passes through the second lens set shooting second direction to operating position, first camera, second camera, third camera by eyeglass mechanism;Second direction includes three visual angles;S3, switch the image that the 3rd lens set passes through the 3rd lens set shooting third direction to operating position, first camera, second camera, third camera by eyeglass mechanism;Third direction includes three visual angles;The image ground shaded areas that the present invention obtains is small, and the model accuracy height of generation, texture quality are good, contribute to aeroplane photography.
Description
Technical field
The present invention relates to a kind of implementation method of nine visual angle oblique photographs 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
More different sensors of camera angle are carried on one flying platform, to gather the aerial image of atural object difference side.It is airborne to incline
Tiltedly the vertical photography pattern that tradition is taken photo by plane has been overturned in photography, and the multi-angle oblique image that it is gathered meets the true of human eye vision
The world directly perceived, spatial information is more rich, complete, friendly, is with a wide range of applications.It is however, existing airborne inclined in the world
Generally there is the shortcomings that complex designing, instrument maximizes, involved great expense, operating cost is high in camera chain, and single, close
40 degree of oblique photograph angle design can not adapt to Surveying and Mapping Industry image very well primarily to meet the purpose of landscape covering
The needs of mapping.In recent years, the Technology of low altitude remote sensing based on unmanned plane, unmanned airship has obtained faster development, high performance CCD
The resolution ratio of camera is up to tens million of grades of pixels, using being mounted on unmanned flight's platform, camera angle design and overall cloth
Rational multiple CCD (appliance coupler part, the Charge Coupled Device) cameras of office carry out low latitudes photography can not only be from
The applications such as right Disaster Assessment, military information collection, emergency command, city management provide inexpensive, real-time high definition and tilt image
Data, moreover it is possible to meet Surveying and Mapping Industry mapping and the needs of other three-dimensional spatial informations processing.
The aviation oblique photograph device used at present generally uses multiple built-in cameras, real by putting for different angle
Existing multiple angle shots, to obtain the panoramic picture on ground.In order to reduce main screw lift and cost, phase built in generally use 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 increase the consumption of electricity, be unfavorable for aeroplane photography.
The defects 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 grown, 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 realization side of nine visual angle oblique photographs for airborne vehicle
Method, realizing from the earthward shooting in nine directions in the air, enrich the application of product, its is simple in construction, and reliability is high,
Effectively mitigate the weight of aviation oblique photograph device, more adapt to aeroplane photography.
To achieve these goals, the invention provides a kind of realization side of nine visual angle oblique photographs for airborne vehicle
Method, first camera, second camera, third camera are fixed on aircraft, and method includes:
S1, airborne vehicle reach target location, and the first lens set switched into operating position, first camera, second camera, the
Three cameras shoot the image of first direction by the first lens set;First direction includes three visual angles;
S2, by eyeglass mechanism switch the second lens set to operating position, first camera, second camera, third camera lead to
Cross the image of the second lens set shooting second direction;Second direction includes three visual angles;
S3, by eyeglass mechanism switch the 3rd lens set to operating position, first camera, second camera, third camera lead to
Cross the image of the 3rd lens set shooting third direction;Third direction includes three visual angles;Complete the visual angle of the target location nine
Image taking;
The shooting angle at above-mentioned nine visual angles differs.
In the present invention, by the lens set of the installation space adjustable angle before camera lens is set, the incidence of different angle is obtained
Light source, in the case where first camera, second camera, third camera are fixed, by switching the eyeglass of straight-on camera in lens set,
First camera, second camera, third camera is obtained the incident light source of nine different angles, realize from earthward nine angles in the air
The shooting of degree.
The present invention realizes the shooting from nine angles in the air earthward, the image that three cameras obtain using three cameras
Have the characteristics that ground shaded areas is small, the model accuracy of generation is high, texture quality is good, the aviation oblique photograph be advantageous to.
Operating position is the lens set institute that is used cooperatively with first camera, second camera, third camera in the present invention
Position.Now, the eyeglass in lens set corresponds to first camera, second camera, third camera respectively.
According to another embodiment of the present invention, nine visual angles be left front visual angle, lower-left visual angle, left back visual angle,
Just preceding visual angle, positive downwards angle of visibility, positive back angle, right preceding visual angle, bottom right visual angle, right back angle.Preferably, nine viewing angles arrive
Image does not have lap between each other, can so gather substantial amounts of data, facilitates the use of successive image.
According to another embodiment of the present invention, the first lens set includes the different eyeglass of three space angles;
Second lens set includes the different eyeglass of three space angles;3rd lens set includes the different eyeglass of three space angles.Nine
The space angle of individual above-mentioned eyeglass is different, corresponds to nine angles, such as front and rear three row, the layout of the row of left and right three respectively.
According to another embodiment of the present invention, when each lens set reaches operating position, its three eyeglasses point
Other face first camera, second camera, third camera, now, each camera obtain the incident light source of a special angle, carry out
The shooting of the angle.
According to another embodiment of the present invention, first camera, second camera, third camera, it is arranged side by side.
According to another embodiment of the present invention, eyeglass mechanism includes rotary eyeglass mechanism.
According to another embodiment of the present invention, rotary eyeglass mechanism is rotating disc type eyeglass mechanism;Pass through rotation
Rotatable eyeglass mechanism completes the switching of the first lens set, the second lens set, the 3rd lens set, each camera is obtained difference respectively
Ground shooting direction.
According to another embodiment of the present invention, eyeglass mechanism includes parallel-moving type eyeglass mechanism.
According to another embodiment of the present invention, parallel-moving type eyeglass mechanism is sliding-rail sliding formula eyeglass mechanism;It is logical
Sliding-rail sliding formula eyeglass mechanism is crossed, completes the switching of the first lens set, the second lens set, the 3rd lens set, makes each camera point
Different ground shooting direction is not obtained.
The present invention is advantageous in that:Camera is fixed, and is electrically connected with, and reduces failure risk, simultaneously because eyeglass acts,
Its light weight, vibrations during rotation are small, the shooting effect of complete machine influenceed also small;The only motion of one degree of freedom, transmission knot
Structure is simple, and positioning precision is high.By setting multiple eyeglasses to realize from the earthward shooting of nine angles in the air, area coverage of taking pictures
Greatly, ground shaded areas is small, facilitates image procossing, improves reliability, 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 being shown using device of the implementation method of nine visual angle oblique photographs for airborne vehicle for embodiment 1
It is intended to;
Fig. 2 is a kind of being shown using device of the implementation method of nine visual angle oblique photographs for airborne vehicle for embodiment 1
It is intended to, which show first direction visual angle.
Embodiment
Embodiment 1
Present embodiments provide a kind of implementation method of nine visual angle oblique photographs for airborne vehicle, first camera,
Two cameras, third camera are arranged side by side on aircraft, and it comprises the following steps:
S1, airborne vehicle reach target location, and the different fixed eyeglass of three space angles in the first lens set is cut
Operating position is shifted to, first camera, second camera, third camera shoot the figure of first direction by the eyeglass in the first lens set
Picture;First direction includes three visual angles, such as left front visual angle, lower-left visual angle, left back visual angle.
S2, the different fixed eyeglass of three space angles in the second lens set switched extremely by rotary eyeglass mechanism
Operating position, first camera, second camera, third camera shoot the image of second direction by the second lens set;Second direction
Including three visual angles, such as just preceding visual angle, positive downwards angle of visibility, positive back angle.
S3, the different fixed eyeglass of three space angles in the 3rd lens set switched extremely by rotary eyeglass mechanism
Operating position, first camera, second camera, third camera shoot the image of third direction by the 3rd lens set;Third direction
Including three visual angles, such as right preceding visual angle, bottom right visual angle, right back angle.Complete the image of nine different visual angles in target location
Shooting.
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 11, second camera 12 on seat, third camera 13, eyeglass mechanism 2, steering wheel 3;Wherein, first camera 11, the second phase
Machine 12, third camera 13 are horizontal camera;Eyeglass mechanism 2 includes the first lens set, the second lens set, the 3rd lens set and turned
Disc type eyeglass adjusting part 21, each lens set include the different fixed eyeglass 22 of three space angles;Rotating disc type eyeglass
Adjusting part 21 includes 211, nine connecting rods 212 of rotating disk driven by steering wheel 3, the first lens set, the second lens set, the 3rd mirror
Piece group is disposed on rotating disk 211, and eyeglass 22 is consistent with the number of connecting rod 212 and is correspondingly arranged, and rotating disk 211 is rotatably pacified
On pedestal, the one end of connecting rod 212 connection eyeglass 22, other end connection rotating disk 211;First camera 11, second camera 12,
Three cameras 13 are disposed side by side on the homonymy of rotating disk 211;Steering wheel 3 connects rotating disk 211 by drive shaft 31;Steering wheel 3 passes through driving
Axle 31 connects rotating disk 211;By rotating rotating disk 211, switching face first camera 11, second camera 12, the mirror of third camera 13
Piece 22, so as to realize first camera 11, second camera 12, third camera 13 from the earthward shooting in nine directions in the air.
(dotted portion shows coverage in figure) as shown in Figure 2, it is real by the rotation of the driving rotating disk 211 of steering wheel 3
The shooting of existing nine angles.For example, under original state shooting, the corresponding positive rear lens of first camera 11, second camera 12 corresponds to just
Lower eyeglass, the corresponding positive front lens of third camera 13, after the completion of three direction shootings, steering wheel 3 drives rotating disk 211 to rotate 120 degree,
Left back eyeglass is switched to the position of corresponding first camera 11, lower-left eyeglass is switched to the position of corresponding second camera 12, will
Left front eyeglass switches to the position of corresponding third camera 13, carries out the shooting of three;After the completion of three direction shootings, steering wheel
3 drive rotating disks 211 rotate 120 degree again, then border piece behind the right side is switched to the position of corresponding first camera 11, and bottom right eyeglass is cut
The position of corresponding second camera 12 is shifted to, right front lens is switched to the position of corresponding third camera 13, carries out three directions
Shooting.
Steering wheel 3 drives rotating disk 211 to rotate, and controls the rotational angle of rotating disk 211, makes the face first of eyeglass 22 on rotating disk 211
Camera 11, second camera 12, third camera 13, realize that the light in nine directions is reflected into the second camera of first camera 11 respectively
12nd, third camera 13, obtain respectively left back, lower-left, it is left front, just after, just under, just before, it is right after, bottom right, it is right before nine directions
Photo, realize the shooting of nine angles.
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 implementation method of nine visual angle oblique photographs for airborne vehicle, first camera, second camera, third camera are solid
It is scheduled on the airborne vehicle, it is characterised in that methods described includes:
S1, airborne vehicle reach target location, and the first lens set is switched into operating position, the first camera, second phase
Machine, the third camera shoot the image of first direction by first lens set;The first direction includes three visual angles;
S2, the second lens set switched to operating position by eyeglass mechanism, the first camera, the second camera, described the
Three cameras shoot the image of second direction by second lens set;The second direction includes three visual angles;
S3, pass through the eyeglass mechanism the 3rd lens set of switching to operating position, the first camera, the second camera, institute
State the image that third camera shoots third direction by the 3rd lens set;The third direction includes three visual angles;Complete
The image taking at nine visual angles in target location;
The shooting angle at above-mentioned nine visual angles differs.
2. the method as described in claim 1, it is characterised in that nine visual angles are left front visual angle, lower-left visual angle, left back regarded
Angle, just preceding visual angle, positive downwards angle of visibility, positive back 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, second lens set, the described 3rd
Lens set includes the different eyeglass of three space angles.
4. the method as described in claim 1, it is characterised in that when each lens set reaches the operating position, each eyeglass
First camera, the second camera, the third camera described in three eyeglasses difference face in group.
5. method as claimed in claim 4, it is characterised in that the first camera, the second camera, the third phase
Machine, it is arranged side by side.
6. the method as described in claim 1, it is characterised in that the eyeglass mechanism includes rotary eyeglass mechanism.
7. method as claimed in claim 6, it is characterised in that the rotary eyeglass mechanism is rotating disc type eyeglass mechanism;It is logical
The switching that the rotary eyeglass mechanism completes first lens set, second lens set, the 3rd lens set is crossed, is made
Each camera obtains different ground shooting direction respectively.
8. the method as described in claim 1, it is characterised in that the eyeglass mechanism includes parallel-moving type eyeglass mechanism.
9. method as claimed in claim 8, it is characterised in that the parallel-moving type eyeglass mechanism is sliding-rail sliding formula eyeglass machine
Structure;By the sliding-rail sliding formula eyeglass mechanism, first lens set, second lens set, the 3rd eyeglass are completed
The switching of group, makes each camera obtain different ground shooting direction respectively.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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CN201710277859 | 2017-04-25 | ||
CN2017102778590 | 2017-04-25 |
Publications (1)
Publication Number | Publication Date |
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CN107643649A true CN107643649A (en) | 2018-01-30 |
Family
ID=60196799
Family Applications (40)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
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 |
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 |
CN201710541937.3A Pending CN107340670A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens single-axis tilt camera for airborne vehicle |
CN201720809528.2U Expired - Fee Related CN207181918U (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens single-axis tilt camera for airborne vehicle |
CN201710542576.4A Pending CN107390453A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens bi-axial tilt camera for airborne vehicle |
CN201710541954.7A Pending CN107367263A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph device for airborne vehicle |
CN201710542200.3A Pending CN107367265A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens rotating disk oblique photograph device for airborne vehicle |
CN201710542703.0A Pending CN107390469A (en) | 2017-04-25 | 2017-07-05 | A kind of polyphaser camera for airborne vehicle |
CN201710541936.9A Pending CN107367886A (en) | 2017-04-25 | 2017-07-05 | A kind of rotary single-lens oblique photograph device for airborne vehicle |
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 |
CN201720809656.7U Expired - Fee Related CN207752284U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera turntable oblique photograph device for aircraft |
CN201710542741.6A Pending CN107643649A (en) | 2017-04-25 | 2017-07-05 | A kind of implementation method of nine visual angle oblique photographs for airborne vehicle |
CN201710542558.6A Pending CN107390452A (en) | 2017-04-25 | 2017-07-05 | A kind of reflective twin-lens bi-axial tilt camera for airborne vehicle |
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 |
CN201710542352.3A Pending CN107560601A (en) | 2017-04-25 | 2017-07-05 | A kind of implementation method of the visual angle oblique photograph of one camera five for airborne vehicle |
CN201710542641.3A Pending CN107364585A (en) | 2017-04-25 | 2017-07-05 | A kind of double camera oblique photograph device for airborne vehicle |
CN201720809659.0U Expired - Fee Related CN207181922U (en) | 2017-04-25 | 2017-07-05 | A kind of rotating disc type lens supports for camera multi-angled shooting |
CN201720809538.6U Expired - Fee Related CN207113871U (en) | 2017-04-25 | 2017-07-05 | A kind of reflective single-lens rotating disk oblique photograph device for airborne vehicle |
CN201720809493.2U Expired - Fee Related CN207764534U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for aircraft |
CN201710542628.8A Pending CN107390454A (en) | 2017-04-25 | 2017-07-05 | A kind of shaft type lens supports for camera multi-angled shooting |
CN201720809677.9U Expired - Fee Related CN207360597U (en) | 2017-04-25 | 2017-07-05 | A kind of double camera rotating disc type oblique photograph device 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 |
CN201720809492.8U Expired - Fee Related CN207113870U (en) | 2017-04-25 | 2017-07-05 | A kind of fixed one camera oblique photograph device for airborne vehicle |
CN201710542256.9A Pending CN107367266A (en) | 2017-04-25 | 2017-07-05 | A kind of fixed one camera oblique photograph device for airborne vehicle |
CN201710542722.3A Pending CN107329363A (en) | 2017-04-25 | 2017-07-05 | A kind of method of six visual angle oblique photographs of double camera for airborne vehicle |
CN201710542560.3A Pending CN107685871A (en) | 2017-04-25 | 2017-07-05 | A kind of block form double camera rotating disc type 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 |
CN201710542315.2A Pending CN107390450A (en) | 2017-04-25 | 2017-07-05 | A kind of reflection type inclined camera of polyphaser for airborne vehicle |
CN201710542643.2A Pending CN107560602A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
CN201720809475.4U Expired - Fee Related CN207106926U (en) | 2017-04-25 | 2017-07-05 | A kind of double camera oblique photograph device for airborne vehicle |
CN201710542197.5A Pending CN107340672A (en) | 2017-04-25 | 2017-07-05 | A kind of single-lens oblique photograph device for airborne vehicle |
CN201710542705.XA Pending CN107576312A (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph method at 12 visual angles for airborne vehicle |
CN201720809537.1U Expired - Fee Related CN207113869U (en) | 2017-04-25 | 2017-07-05 | A kind of oblique photograph device for airborne vehicle |
CN201710542036.6A Pending CN107340671A (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
CN201720809623.2U Expired - Fee Related CN207181920U (en) | 2017-04-25 | 2017-07-05 | A kind of one camera oblique photograph device for airborne vehicle |
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CN201710542218.3A Pending CN107380471A (en) | 2017-04-25 | 2017-07-05 | A kind of double camera rotating disc type oblique photograph device for airborne vehicle |
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CN201710542218.3A Pending CN107380471A (en) | 2017-04-25 | 2017-07-05 | A kind of double camera rotating disc type oblique photograph device for airborne vehicle |
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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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CN205931287U (en) * | 2016-08-04 | 2017-02-08 | 数字鹰(泰州)农业科技有限公司 | Unmanned aerial vehicle field of vision expanding unit of making a video recording |
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