CN107685871A - A kind of block form double camera rotating disc type oblique photograph device for airborne vehicle - Google Patents

A kind of block form double camera rotating disc type oblique photograph device for airborne vehicle Download PDF

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Publication number
CN107685871A
CN107685871A CN201710542560.3A CN201710542560A CN107685871A CN 107685871 A CN107685871 A CN 107685871A CN 201710542560 A CN201710542560 A CN 201710542560A CN 107685871 A CN107685871 A CN 107685871A
Authority
CN
China
Prior art keywords
camera
eyeglass
disc type
rotating disc
rotating disk
Prior art date
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
CN201710542560.3A
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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
Original Assignee
GUANGZHOU REDBIRD HELICOPTER REMOTE SENSING TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by GUANGZHOU REDBIRD HELICOPTER REMOTE SENSING TECHNOLOGY Co Ltd filed Critical GUANGZHOU REDBIRD HELICOPTER REMOTE SENSING TECHNOLOGY Co Ltd
Publication of CN107685871A publication Critical patent/CN107685871A/en
Pending legal-status Critical Current

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Classifications

    • 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
    • G—PHYSICS
    • G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
    • G03B17/00—Details of cameras or camera bodies; Accessories therefor
    • G03B17/02—Bodies
    • G03B17/17—Bodies with reflectors arranged in beam forming the photographic image, e.g. for reducing dimensions of camera
    • G—PHYSICS
    • G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
    • G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
    • G03B37/00—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe
    • G03B37/04—Panoramic or wide-screen photography; Photographing extended surfaces, e.g. for surveying; Photographing internal surfaces, e.g. of pipe with cameras or projectors providing touching or overlapping fields of view
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
    • G01C11/02—Picture taking arrangements specially adapted for photogrammetry or photographic surveying, e.g. controlling overlapping of pictures
    • 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 block form double camera rotating disc type oblique photograph device for airborne vehicle, including：First camera, second camera, rotating disc type angle adjusting mechanism, the power part for driving rotating disk formula angle adjusting mechanism；Rotating disc type angle adjusting mechanism includes the different eyeglass of some space angles, the rotating disk by power part driving, some connecting rods, eyeglass is consistent with connecting rod number and is correspondingly arranged, rotating disk is rotatably installed on airborne vehicle, connecting rod one end connection eyeglass, other end connection rotating disk；First camera is installed on aircraft, and second camera is installed on aircraft；First camera, second camera are disposed in parallel in the homonymy of rotating disk；Power part is installed on aircraft；By rotating rotating disk, switching first camera, the eyeglass of second camera, so as to change first camera, the shooting direction of second camera.The present invention is simple in construction, and shooting effect is good；Camera is fixed, and reduces failure risk, and reliability is high.

Description

A kind of block form double camera rotating disc type oblique photograph device for airborne vehicle
Technical field
The present invention relates to a kind of block form double camera rotating disc type oblique photograph device 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.Or in order to reduce main screw lift and cost, using phase built in rotation Machine realizes multi-angled shooting, to reduce the quantity of built-in camera；In order to reduce main screw lift and cost, built in generally use rotates Camera realizes multi-angled shooting, to reduce built-in camera quantity.Because the volume and weight of built-in camera itself is larger, during rotation Complete machine vibrations can be caused 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 block form double camera rotating disc type inclination for airborne vehicle and taken the photograph Image device, realize from the earthward shooting of any direction in the air, enrich the application of product, its is simple in construction, reliably Property it is high, effectively mitigate the weight of aviation oblique photograph device, more adapt to aeroplane photography.
To achieve these goals, tilt and take the photograph the invention provides a kind of block form double camera rotating disc type for airborne vehicle Image device, it includes：
First camera, second camera, rotating disc type angle adjusting mechanism, the power for driving rotating disk formula angle adjusting mechanism Part；
If rotating disc type angle adjusting mechanism include the different eyeglass of some space angles, by power part driving rotating disk, Involvement extension bar, eyeglass is consistent with connecting rod number and is correspondingly arranged, and rotating disk is rotatably installed on airborne vehicle, connecting rod one end Connect eyeglass, other end connection rotating disk；
First camera is installed on aircraft, and second camera is installed on aircraft；First camera, second camera are set side by side Put the homonymy in rotating disk；
Power part is installed on aircraft；
By rotating rotating disk, switching first camera, the eyeglass of second camera, so as to change first camera, second camera Shooting direction.
In the present invention, by setting the different eyeglass of some space angles before camera lens, entering for different angle is obtained Light source is penetrated, in the case where camera is fixed, the eyeglass different by switching space angle, the direction of change camera entrance light source, Further realize from the earthward shooting of multiple angles in the air.
By one group of double camera for being arranged on rotating disk homonymy in the present invention, reduce the shooting time of target location, increase The overlapping area of shooting photo, it is possible to reduce the requirement for Duplication of taking photo by plane, increase the interval in course line, improve operating efficiency, from And more add and aeroplane photography.
In the present invention, using the direction of one of camera lens as front.
According to another embodiment of the present invention, eyeglass number is 6, by setting 6 eyeglasses to realize from aerial The earthward shooting in 6 directions.
According to another embodiment of the present invention, six eyeglasses include left lens group, right lens group, lower side mirror Piece group, left lens group include the eyeglass of left front, left back both direction, right lens group include it is right before, right latter two direction Eyeglass, downside lens set include lower-left, the eyeglass of bottom right both direction.
According to another embodiment of the present invention, left front eyeglass, left back eyeglass in left lens group correspond to respectively First camera, second camera；Right front lens, right rear lens in right lens group correspond to first camera, second camera respectively；Under Lower-left eyeglass, bottom right eyeglass in the lens set of side correspond to first camera, second camera respectively.
According to another embodiment of the present invention, left lens group, right lens group, downside lens set are uniformly arranged On rotating disk.In the present invention, when camera is shot, while there is one group of two eyeglass to be located at operating position, wherein operating position, refer to mirror Position when piece and camera be used cooperatively where eyeglass, ensure that first camera, second camera can be shot simultaneously, mirror The angle in piece space is different, and first camera, the photo of second camera shooting are different, substantially increase operating efficiency.
According to another embodiment of the present invention, left lens group, right lens group, downside lens set pass through bag The connecting portion for including connecting rod is arranged on rotating disk, and connecting portion number is 3, and the angular separation between abutting connection is 120 °.
According to another embodiment of the present invention, steering wheel is by driving axis connection rotating disk；Steering wheel drives drive rod to drive Turn disk rotates, and then realizes the switching of eyeglass；In whole shooting process, due to rotating rotating disk and eyeglass, its light weight, rotate When vibrations it is small, the shooting effect of complete machine is influenceed also small, whole transmission process only has the motion of one degree of freedom, drive mechanism Simply, positioning precision is high.
According to another embodiment of the present invention, camera is horizontal camera, horizontal camera here refer to optical axis with Horizontal plane angulation is less than or equal to 75 °.
According to another embodiment of the present invention, rotating disc type oblique photograph device also includes pedestal, and pedestal is arranged on On airborne vehicle, first camera, second camera, power part are fixedly mounted on pedestal, and rotating disk is rotatably installed on pedestal. First camera, second camera, power part are corresponded in pedestal and is provided with support base, it is removably connected and airborne vehicle, wherein also Provided with other parts, such as controlling organization in Aerial photography.
The present invention shooting process be：When reaching target location, shot by first camera, second camera, it is complete Into after the angle shot, by steering wheel, drive rotating disk to rotate 120 degree, switch to the eyeglass of other different conditions, carry out other angles The shooting of degree；Multiple rotary rotating disk, complete the multi-angled shooting of target location.
In the present invention, rotating disk rotates the shooting that can complete the position twice, for example, under original state, downside lens set In operating position, first camera corresponds to lower-left eyeglass, and second camera corresponds to bottom right eyeglass, after the completion of the angle shot, steering wheel Drive rotating disk to rotate 120 degree, left lens group is switched into operating position, now, left front eyeglass switches to corresponding first camera Position, left back eyeglass switches to the position of corresponding second camera, carries out the shooting of the angle；After the completion of shooting, steering wheel drives Rotating disk rotates 120 degree again, right lens group is switched into operating position, border piece switches to the position for corresponding to first camera behind the right side Put, right front lens is switched to the position of corresponding second camera, carries out the shooting of angle.
The present invention is advantageous in that：Multi-angled shooting is realized by rotating eyeglass, two built-in cameras realize six The shooting effect of built-in camera.Layout vertical compared to conventional bevel camera is set, the effective weight for mitigating whole device, favorably In aeroplane photography；Simultaneously because rotate rotating disk and eyeglass, its light weight, vibrations during rotation are small, to the shooting effect shadow of complete machine Sound is also small.Built-in camera position is fixed, and it is electrically connected without motion, reduces failure risk, and reliability is high.Only one degree of freedom Motion, drive mechanism is simple, and positioning precision is high.The photo of built-in camera shooting is overlapped, it is possible to reduce Duplication of taking photo by plane It is required that increasing 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 overall knot of block form double camera rotating disc type oblique photograph device for airborne vehicle of embodiment 1 Structure schematic diagram；
Fig. 2 is a kind of schematic diagram of block form double camera rotating disc type oblique photograph device for airborne vehicle of embodiment 1, Which show lower-left, the shooting state of lower right；
Fig. 3 is a kind of schematic diagram of block form double camera rotating disc type oblique photograph device for airborne vehicle of embodiment 1, Which show the shooting state in left front, left back direction；
Fig. 4 is a kind of schematic diagram of block form double camera rotating disc type oblique photograph device for airborne vehicle of embodiment 1, Which show before the right side, right back to shooting state.
Embodiment
Embodiment 1
Present embodiments provide a kind of block form double camera rotating disc type oblique photograph device for airborne vehicle, such as Fig. 1-4 It is shown, including：Pedestal and the first camera 1 being arranged on pedestal, second camera 2, rotating disc type angle adjusting mechanism 3, steering wheel 4； Wherein, first camera 1, second camera 2 are horizontal camera；Rotating disc type angle adjusting mechanism 3 includes six space angle differences Eyeglass 31,32, six connecting rods 33 of rotating disk for being driven by steering wheel 4, eyeglass 31 is consistent with the number of connecting rod 33 and is correspondingly arranged, Rotating disk 32 is rotatably installed on pedestal, the one end of connecting rod 33 connection eyeglass 31, other end connection rotating disk 32；First camera 1, Second camera 2 is arranged on the homonymy of rotating disk 32；Steering wheel 4 connects rotating disk 32 by drive shaft 41；Steering wheel 4 is connected by drive shaft 41 Rotating disk 32；By rotating rotating disk 32, switching face first camera 1, the eyeglass 31 of second camera 2, so as to change first camera 1, The shooting direction of second camera 2.
Wherein, the number of eyeglass 31 is 6, and it includes left lens group 311, right lens group 312, downside lens set 313, it is uniformly arranged on rotating disk 32 by connecting portion 321, and connecting portion 321 is provided with two connecting rods 33；Connecting portion 321 counts Mesh is 3, and the angular separation between abutting connection 321 is 120 °；Left lens group 311 includes left front, left back both direction Eyeglass, right lens group 312 include it is right before, the eyeglass in latter two right direction, downside lens set 313 includes lower-left, bottom right two The eyeglass in direction.Left front eyeglass, left back eyeglass in left lens group 311 correspond to first camera 1, second camera 2 respectively；Right side Right front lens, right rear lens in lens set 312 correspond to first camera 1, second camera 2 respectively；A left side in downside lens set 313 Lower eyeglass, bottom right eyeglass correspond to first camera 1, second camera 2 respectively.
(dashed region shows coverage in figure) as in Figure 2-4, it is real by the rotation of the driving rotating disk 32 of steering wheel 4 Existing transformation of the shooting state from Fig. 2-Fig. 4.For example, as shown in Fig. 2 original state shooting under, the corresponding lower-left mirror of first camera 1 Piece, the corresponding bottom right eyeglass of second camera 2, after the completion of the angle shot, steering wheel 4 drives rotating disk 32 to rotate 120 degree, as shown in figure 3, Left front eyeglass is switched to the position of corresponding first camera 1, right front lens is switched to the position of corresponding second camera 2, carried out The shooting of the angle；After the completion of shooting, steering wheel drives rotating disk to rotate 120 degree again, as shown in figure 4, again switching left back border piece To the position of corresponding first camera 1, right rear lens is switched to the position of corresponding second camera 2, carries out the shooting of the angle.
Steering wheel 4 drives lens slewing disc 32 to horizontally rotate, and controls the rotational angle of rotating disk 32, makes eyeglass face on rotating disk 32 the One camera 1 and second camera 2, realize that the light of six direction is reflected into first camera 1 and second camera 2 respectively, obtain respectively Take left front, lower-left, it is left back, right before, bottom right, it is right after six direction photo, realize the shooting of multi-angle.
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 1. block form double camera rotating disc type oblique photograph device for airborne vehicle, it is characterised in that the oblique photograph Device includes：First camera, second camera, rotating disc type angle adjusting mechanism, for driving the rotating disc type angle adjusting mechanism Power part；
    The rotating disc type angle adjusting mechanism includes the different eyeglass of some space angles, turned by what the power part drove Disk, some connecting rods, the eyeglass is consistent with the connecting rod number and is correspondingly arranged, and the rotating disk is rotatably installed in institute State on airborne vehicle, described connecting rod one end connects the eyeglass, and the other end connects the rotating disk；
    The first camera is arranged on the airborne vehicle, and the second camera is arranged on the airborne vehicle；First phase Machine, the second camera are disposed in parallel in the homonymy of the rotating disk；
    The power part is arranged on the airborne vehicle；
    By rotating the rotating disk, switch the first camera, the eyeglass of the second camera, so as to change first phase The shooting direction of machine, the second camera.
  2. 2. rotating disc type oblique photograph device as claimed in claim 1, it is characterised in that the eyeglass number is 6.
  3. 3. rotating disc type oblique photograph device as claimed in claim 2, it is characterised in that six eyeglasses are divided into left lens Group, right lens group, downside lens set, the left lens group include the eyeglass of left front, left back both direction, the right side mirror Piece group include it is right before, the eyeglass in latter two right direction, the downside lens set includes lower-left, the eyeglass of bottom right both direction.
  4. 4. rotating disc type oblique photograph device as claimed in claim 3, it is characterised in that the left side in the left lens group Front lens, the left back eyeglass correspond to the first camera, the second camera respectively；The right side in the right lens group Front lens, the right rear lens correspond to the first camera, the second camera respectively；The left side in the downside lens set Lower eyeglass, the bottom right eyeglass correspond to the first camera, the second camera respectively.
  5. 5. rotating disc type oblique photograph device as claimed in claim 4, it is characterised in that the left lens group, the right side Lens set, the downside lens set are uniformly arranged on the rotating disk.
  6. 6. rotating disc type oblique photograph device as claimed in claim 5, it is characterised in that the rotating disk is provided with connecting portion, institute State connecting portion and be provided with two connecting rods；The left lens group, the right lens group, the downside lens set are arranged at On the connecting portion, the connecting portion number is 3, and the angular separation between the adjacent connecting portion is 120 °.
  7. 7. rotating disc type oblique photograph device as claimed in claim 1, it is characterised in that the power part is steering wheel, described Steering wheel is by driving rotating disk described in axis connection.
  8. 8. rotating disc type oblique photograph device as claimed in claim 1, it is characterised in that the camera is horizontal camera.
  9. 9. the rotating disc type oblique photograph device as described in one of claim 1-8, it is characterised in that the rotating disc type oblique photograph Device also includes pedestal, and the pedestal is arranged on the airborne vehicle, the first camera, the second camera, the power Part is fixedly mounted on the pedestal, and the rotating disk is rotatably installed on the pedestal.
CN201710542560.3A 2017-04-25 2017-07-05 A kind of block form double camera rotating disc type oblique photograph device for airborne vehicle Pending CN107685871A (en)

Applications Claiming Priority (2)

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

Publications (1)

Publication Number Publication Date
CN107685871A true CN107685871A (en) 2018-02-13

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
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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
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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
CN201720809565.3U Expired - Fee Related CN207181919U (en) 2017-04-25 2017-07-05 A kind of rotary single-lens oblique photograph device for airborne vehicle
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CN201720809625.1U Expired - Fee Related CN207181921U (en) 2017-04-25 2017-07-05 A kind of shaft type lens supports for camera multi-angled shooting

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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
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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
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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
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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
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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

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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
CN201720809565.3U Expired - Fee Related CN207181919U (en) 2017-04-25 2017-07-05 A kind of rotary single-lens oblique photograph device for airborne vehicle
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
CN201710542577.9A Pending CN107499525A (en) 2017-04-25 2017-07-05 A kind of opposed double camera rotating disc type oblique photograph device for airborne vehicle
CN201710551944.1A Pending CN107367887A (en) 2017-04-25 2017-07-05 A kind of one camera rotating disk oblique photograph device for airborne vehicle
CN201720809625.1U Expired - Fee Related CN207181921U (en) 2017-04-25 2017-07-05 A kind of shaft type lens supports for camera multi-angled shooting

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