CN107390450A - A kind of reflection type inclined camera of polyphaser for airborne vehicle - Google Patents
A kind of reflection type inclined camera of polyphaser for airborne vehicle Download PDFInfo
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- CN107390450A CN107390450A CN201710542315.2A CN201710542315A CN107390450A CN 107390450 A CN107390450 A CN 107390450A CN 201710542315 A CN201710542315 A CN 201710542315A CN 107390450 A CN107390450 A CN 107390450A
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- type eyeglass
- oblique photograph
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- 230000004075 alteration Effects 0.000 abstract description 2
- 230000000007 visual effect Effects 0.000 description 7
- 230000008859 change Effects 0.000 description 5
- 238000013507 mapping Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000012545 processing Methods 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
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
-
- 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
-
- 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
- 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
-
- 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 invention provides a kind of reflection type inclined camera of the polyphaser for airborne vehicle, including:Camera mechanism, it is set on aircraft, including camera, support component, swing type eyeglass, the power part for driving swing type eyeglass, camera are arranged in support component, and swing type eyeglass corresponds to camera setting, and it is swingably arranged in support component;The posture of swing type eyeglass is adjusted by power part, changes the incident ray direction of camera;The number of camera mechanism is at least three groups, and swing type eyeglass is respectively provided in different planes in each camera mechanism.The present invention realized from the earthward shooting of multi-angle in the air, the problem of avoiding the poor image quality that camera rotational band is come, and rotations, shooting figure aberration can not be realized by solving the problems, such as in traditional aeroplane photography that camera is overweight, and the data skew that it is gathered is small, precision height;Drive mechanism is simple, in light weight, and cost is low, and reliability is high, so as to more adapt to aeroplane photography.
Description
Technical field
The present invention relates to a kind of reflection type inclined camera of the polyphaser 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 but 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.
Chinese patent 201220681352.4 discloses a kind of digital aviation oblique photograph measurement apparatus, including support, branch
One lens axis of installation vertically downward lower regards camera to frame between two parties, and the camera ring of four tilts is installed on support,
Four inclined cameras are circumferentially uniformly installed, and its axis is identical with the lower lens axis angle regarding camera, and direction points to four successively
Individual direction, form the vertical/oblique photograph structure for regarding five shooting angle all around and down;Support is rectangle, and its length of side c is
380mm, camera lens are installed on support by mounting hole, and lens axis and support rectangle plane angle β are 45 degree, mounting hole center
It is 182.45mm at a distance of a, the diameter R of mounting hole is 95mm.
Chinese patent 201610240753.9 discloses a kind of machine-carried type multi-angle oblique video camera, including shell, shooting
Window and camera, a shooting window is formed with the lower end center of shell and is provided with one the camera window is intraoral
Individual center camera straight down, the shooting window outer periphery in the center be uniformly formed with it is multiple be obliquely installed take the photograph
As window, multiple intraoral courts for being separately installed with canted shot head, canted shot head and shooting window of camera window being obliquely installed
To consistent.
The defects of above-mentioned technical proposal, is:
1st, installation weight is larger, and complete machine vibrations are obvious;
2nd, camera drive mechanism 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 invention provides a kind of reflection type inclined photography dress of polyphaser for airborne vehicle
Put, it realizes that the light of different angle enters camera by swing type eyeglass, while each camera mechanism is respectively provided with and different inclined
Rake angle, realize the shooting of heading different angle;It realizes that camera group from the earthward shooting of multiple angles in the air, is enriched
The application of product, its shooting efficiency is high, highly reliable, more adapt to aeroplane photography.
To achieve these goals, the invention provides a kind of reflection type inclined photography dress of polyphaser for airborne vehicle
Put, it includes:
Camera mechanism, its set on aircraft, including camera, support component, swing type eyeglass, for driving swing type
The power part of eyeglass, camera are arranged in support component, and swing type eyeglass corresponds to camera setting, and it is swingably arranged on branch
On support component;
The posture of swing type eyeglass is adjusted by power part, changes the incident ray direction of camera;
The number of camera mechanism is at least three groups, and 0 ° of the rotating shaft angulation of swing type eyeglass in adjacent camera mechanism-
90 °, at any time, swing type eyeglass is located in different planes respectively in each camera mechanism.
In the present invention, at any time, swing type eyeglass is respectively provided in different planes in each camera mechanism.
In the present invention, by setting three groups or more than three groups of camera mechanism, realize from earthward multiple angles in the air
Shooting;Wherein, shooting direction corresponding to each camera mechanism is differed, and swing type eyeglass is respectively provided in different planes,
Correspond to the shooting of different zones respectively, in each group of camera mechanism, power part drives swing type eyeglass to swing, and adjusts corresponding phase
The direction of the incident ray of machine, complete the shooting of default shooting angle.
According to another embodiment of the present invention, using the horizontal median axis of oblique photograph device as reference, swing
Formula eyeglass swings for luffing angle.Swing type eyeglass is located at the front of camera, and the pitching of eyeglass is controlled by power part,
Realize the shooting in specified angle direction.
According to another embodiment of the present invention, the number of camera mechanism is three groups, including left side perspective photography
Mechanism, lower-side angle camera mechanism, right side perspective camera mechanism.Each visual angle includes some angle directions, is put by adjusting
The posture of dynamic formula eyeglass, realize the shooting in specified angle direction;Such as each camera mechanism shoots the image of three angle directions,
The shooting at nine visual angles can be achieved, nine visual angles are the column distribution of three row of endian format three.
According to another embodiment of the present invention, the camera in each camera mechanism is arranged side by side, adjacent cameras
The distance between it is identical, camera is fixedly installed in support component.
According to another embodiment of the present invention, camera mechanism also includes rotating shaft, and power part drive shaft is driven
Movable pendulum dynamic formula eyeglass is swung.
According to another embodiment of the present invention, rotating shaft passes through the center of swing type eyeglass, and swing type eyeglass encloses
Certain angle is swung around the shaft.In swing process, its position does not change swing type eyeglass, is being always positioned at camera just
Front, the distortion degree of shooting photograph is substantially reduced, facilitates oblique photograph.
According to another embodiment of the present invention, each power part is steering wheel.
According to another embodiment of the present invention, each camera is horizontal camera, and horizontal camera here is
Refer to optical axis and be less than or equal to 75 ° with horizontal plane angulation.
According to another embodiment of the present invention, oblique photograph device also includes pedestal, base runner or fixation
On aircraft, camera mechanism is arranged on pedestal for installation.
According to another embodiment of the present invention, each support component is fixedly connected with pedestal, entirely shot
Cheng Zhong, the position of camera do not change, and avoid the shooting problem that camera rotational band is come.
The present invention is advantageous in that:By setting multiple photographic units, realize from the earthward bat of multi-angle in the air
Take the photograph, the problem of avoiding the poor image quality that camera rotational band is come, solve in the case that camera is overweight in traditional aeroplane photography,
Camera can not realize rotation, and the problem of shooting figure aberration, the data skew that it is gathered is small, and precision is high;Drive mechanism is simple, weight
Gently, cost is low, and reliability is high, 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 overall structure signal of the reflection type inclined camera of polyphaser for airborne vehicle of embodiment 1
Figure;
Fig. 2 is a kind of overall structure signal of the reflection type inclined camera of polyphaser for airborne vehicle of embodiment 1
Figure, which show first angle;
Fig. 3 is a kind of overall structure signal of the reflection type inclined camera of polyphaser for airborne vehicle of embodiment 1
Figure, which show second angle;
Fig. 4 is a kind of overall structure signal of the reflection type inclined camera of polyphaser for airborne vehicle of embodiment 1
Figure, which show third angle;
Fig. 5 is a kind of overall structure signal of the reflection type inclined camera of polyphaser for airborne vehicle of embodiment 1
Figure, which show fourth angle.
Embodiment
Embodiment 1
A kind of reflection type inclined camera of the polyphaser for airborne vehicle is present embodiments provided, as Figure 1-Figure 5,
It includes the first camera mechanism 1, the second camera mechanism 2, the 3rd camera mechanism 3.
Wherein, the first camera mechanism includes first camera 11, first support bar 12, the first swing type eyeglass 13, the first rudder
Machine 14, one end connection first camera 11 of first support bar 12, the other end connect the first swing type eyeglass 13, first support bar 12
The first support 15 for being used for placing the first swing type eyeglass 13 is provided with, the first swing type eyeglass 13 is installed in rotation on first
On support 15;The first swing type of the drive connection eyeglass 13 of first steering wheel 14, it is arranged in first support 15.With first camera 11
The direction of camera lens face is front visual angle, the image of the corresponding shooting left side perspective of the first camera mechanism 1, as Figure 2-Figure 5, is led to
Crossing the first steering wheel 14 drives the first swing type eyeglass 13 to rotate, and realizes the change of four angle directions in left side, obtains four, left side
The shooting image of angle direction.
Second camera mechanism 2 includes second camera 21, second support bar 22, the second swing type eyeglass 23, the second steering wheel 24,
One end connection second camera 21 of second support bar 22, the other end connect the second swing type eyeglass 23, set in second support bar 22
There is the second support 25 for placing the second swing type eyeglass 23, the second swing type eyeglass 23 is installed in rotation on second support
On 25;The second swing type of the drive connection eyeglass 23 of second steering wheel 24, it is arranged in second support 25.With the camera lens of first camera 1
The direction of face is front visual angle, the image at the second camera mechanism 2 corresponding shooting lower section visual angle, as Figure 2-Figure 5, by the
Two steering wheels 24 drive the second swing type eyeglass 23 to rotate, and realize the change of four angle directions in lower section, obtain four angles in lower section
The shooting image in direction.
3rd camera mechanism 3 includes third camera 31, the 3rd support bar 32, the 3rd swing type eyeglass 33, the 3rd steering wheel 34,
One end connection third camera 31 of 3rd support bar 32, the other end connect the 3rd swing type eyeglass 33, set on the 3rd support bar 32
There is the 3rd support 35 for placing the 3rd swing type eyeglass 33, the 3rd swing type eyeglass 33 is installed in rotation on the 3rd support
On 35;The swing type eyeglass 33 of 3rd steering wheel, 34 drive connection the 3rd, it is arranged on the 3rd support 35.With the camera lens of first camera 1
The direction of face is front visual angle, the image of the corresponding shooting right side perspective of the 3rd camera mechanism 3, as Figure 2-Figure 5, by the
Three steering wheels 34 drive the 3rd swing type eyeglass 33 to rotate, and realize the change of four angle directions in right side, obtain four angles in right side
The shooting image in direction.
Wherein, the first swing type eyeglass 13, are driven by the first steering wheel 14, the second steering wheel 24, the 3rd steering wheel 34 respectively
Two swing type eyeglasses 23, the 3rd swing type eyeglass 33 are swung, and are realized from Fig. 2-Fig. 5 (wherein dashed region display shooting models
Enclose) adjustment, complete from the earthward shooting of multiple angles in the air.
The present embodiment sets three groups of camera mechanisms, changes the incident ray direction of camera by swing type eyeglass, so as to real
Now from the earthward shooting of multiple angles in the air, its is simple and reliable for structure, and camera is fixed, and it is electrically connected without motion, is reduced and is lost
Risk is imitated, reliability is high;Angle accurate positioning, image acquisition rate are high.
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)
- A kind of 1. reflection type inclined camera of polyphaser for airborne vehicle, it is characterised in that the oblique photograph device bag Include:Camera mechanism, it is arranged on the airborne vehicle, including camera, support component, swing type eyeglass, for driving the pendulum The power part of dynamic formula eyeglass, the camera are arranged in the support component, and the swing type eyeglass corresponds to the camera and set Put, it is swingably arranged in the support component;The posture of the swing type eyeglass is adjusted by the power part, changes the incident ray direction of the camera;The number of the camera mechanism is at least three groups, described in the adjacent camera mechanism formed by the rotating shaft of swing type eyeglass 0 ° -90 ° of angle, at any time, swing type eyeglass described in each camera mechanism is respectively in different planes.
- 2. oblique photograph device as claimed in claim 1, it is characterised in that relative to the airborne vehicle, the swing type mirror Piece swings for luffing angle.
- 3. oblique photograph device as claimed in claim 1, it is characterised in that the camera in each camera mechanism is simultaneously Row is set, and the distance between adjacent described camera is identical.
- 4. oblique photograph device as claimed in claim 1, it is characterised in that the rotating shaft is passed through in the swing type eyeglass The heart, the power part drive the swing type eyeglass to surround the shaft swing.
- 5. oblique photograph device as claimed in claim 1, it is characterised in that each power part is steering wheel.
- 6. oblique photograph device as claimed in claim 1, it is characterised in that each camera is horizontal camera.
- 7. the oblique photograph device as described in one of claim 1-6, it is characterised in that the oblique photograph device also includes base Seat, the base runner are arranged on the airborne vehicle, and the camera mechanism is arranged on the pedestal.
- 8. the oblique photograph device as described in one of claim 1-6, it is characterised in that the oblique photograph device also includes base Seat, the pedestal are fixedly mounted on the airborne vehicle, and the camera mechanism is arranged on the pedestal.
- 9. oblique photograph device as claimed in claim 7 or 8, it is characterised in that each support component is fixedly connected with The pedestal.
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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CN107390450A true CN107390450A (en) | 2017-11-24 |
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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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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