CN106017421A - Sweeping-type low altitude photogrammetry device based on small light UAV - Google Patents
Sweeping-type low altitude photogrammetry device based on small light UAV Download PDFInfo
- Publication number
- CN106017421A CN106017421A CN201610385469.0A CN201610385469A CN106017421A CN 106017421 A CN106017421 A CN 106017421A CN 201610385469 A CN201610385469 A CN 201610385469A CN 106017421 A CN106017421 A CN 106017421A
- Authority
- CN
- China
- Prior art keywords
- camera
- small
- gripper shoe
- unmanned plane
- connects
- 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
Links
Classifications
-
- 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
Abstract
A sweeping-type low altitude photogrammetry device based on a small light UAV is provided. A lower central board of the small light UAV is connected to a support plate by damping balls to form a damping platform; damping platform center is vertically connected to a hanging rod; the upper end of the hanging rod is fixedly connected with a driving motor; the driving motor is coaxially connected with a small gear; the small gear is in meshing connection to a big gear; the big gear is connected with one end of a rocker arm, and the other end of the rocker arm is connected to one end of a camera base support plate through rollers; the bottom end of the hanging rod is vertically and movably connected with the center position of the camera base support plate; and the camera base support plate is connected with an airborne camera. The technical effect of the invention is to simplify the structure of the current mainstream tilt camera measurement device, reduce the weight of the device, increase the working time, and reach less restriction by the wind the continuous angle shot.
Description
Technical field
The present invention relates to a kind of photogrammetric apparatus, particularly relate to a kind of sweep type low altitude photogrammetry device based on small-sized unmanned plane.
Background technology
At present, the low altitude photogrammetry device researched and developed both at home and abroad is concentrated mainly on the oblique photograph that vertical photography based on one camera is measured and polyphaser combines and measures.The atural object image information that cannot obtain multi-angle measured by the vertical photography of one camera, and the side-information of such as building, intersection angle is little, constrains the raising of photogrammetric accuracy.And the oblique photograph measuring table structure of polyphaser combination is complicated, camera number is more, and cost is high, and the activity duration is short, has a certain distance with the present invention on the activity duration.Multi-angle photogrammetric is mainly used in the high-precision photogrammetric application such as with three-dimension tidal current.
Existing small-sized unmanned plane multi-angle aerophotogrammetry is concentrated mainly on oblique photograph and measures the realization of system, a kind of numeral aviation oblique photograph measurement apparatus that have China 2013 year authorize close with the research contents of the present invention, the patent No.: ZL201220681352.4, describe a kind of numeral aviation oblique photograph measurement apparatus, this device is installed a lens axis vertically downward lower and is installed on support depending on camera and four inclined camera hoops, its lens axis is a fixed angle with the lower lens axis regarding camera in space, and it is respectively directed to four direction, constitute all around and regard down the vertical/oblique photograph structure of five shooting angle, to realize the function of multi-angled shooting.The Aviation Digital oblique photograph measurement apparatus of utility model patent multi-angle array combination in 2015, the patent No.: ZL201510002994.5, describe the Aviation Digital oblique photograph measurement apparatus of a kind of multi-angle array combination, including photographing unit multi-angle array element, and the camera control unit being connected with this photographing unit multi-angle array element, image store unit, power control unit, multiple photograph unit is included at photographing unit multi-angle array element, each photograph unit includes multiple stage photographing unit, combine a photographing unit in each photograph unit and constitute a shooting array combination, boat can be extended and take the photograph ken angle, improve the quality of outdoor scene threedimensional model.Patent of invention many rotor wing unmanned aerial vehicles oblique photograph system that 2016 authorize, the patent No.: ZL201510668233.3, describe a kind of many rotor wing unmanned aerial vehicles oblique photograph system, including The Cloud Terrace carry assembly, oblique photograph The Cloud Terrace, including roll axle carry, upper backup pad, lower bracing frame, lower bracing frame carry framework, four sides of lower bracing frame arrange inclination installing rack, and photographic attachment is fixedly mounted on inclination installing rack, realizes oblique photograph by polyphaser combination and measures.
Summary of the invention
It is an object of the invention to provide a kind of sweep type low altitude photogrammetry device based on small-sized unmanned plane, concentrate on polyphaser combination oblique photograph measurement apparatus and there is the shortcomings such as structure is complicated, The Cloud Terrace volume is big, device is heavier, camera angle is fixed, camera quantity is many, expensive, the activity duration is short solving existing multi-angle low altitude photogrammetry.Though system is measured in the combination oblique photograph of above-mentioned polyphaser can realize multi-angle earth observation, but needs the camera of up to more than four to shoot simultaneously, image can only be gathered according to support fixed angle.Existing for multi-angle low altitude photogrammetry depend on increase camera quantity complete, the most simple shoots with fixing several angles, and small-sized unmanned aerial vehicle platform is easily affected by air-flow or wind-force, the image that this type of platform obtains is difficult to ensure that prescription, simultaneously, polyphaser combination is added significantly to small-sized unmanned plane weight, and then greatly reduces the stagnant idle job time, affects low altitude photogrammetry efficiency.
The present invention is realized in, it includes shock-absorbing ball, gripper shoe, drive motor, little gear, gear wheel, rocking arm, hanger bar, camera pedestal gripper shoe, roller, Airborne Camera, small-sized unmanned plane, it is characterized in that: the lower central plate of small-sized unmanned plane connects gripper shoe by shock-absorbing ball and forms damped platform, damped platform center vertically connects hanger bar, the upper end of hanger bar fixing connection drives motor, motors is driven to connect little gear, the engagement of little gear connects gear wheel, one end of connecting rocker arm on gear wheel, the other end of rocking arm connects one end of camera pedestal gripper shoe by roller, the bottom Vertical movements of described hanger bar connects the center of camera pedestal gripper shoe, it is connected with Airborne Camera in described camera pedestal gripper shoe.
Described driving motor and Airborne Camera connect lithium battery and the main control unit of small-sized unmanned plane.
The solution have the advantages that: complete multi-angle low altitude photogrammetry based on sweep type photographic imagery, only rely on separate unit digital camera and during small-sized unmanned plane is advanced, swing shooting to obtain several images in certain angle.Compared with other above-mentioned inventions, it first it is that shooting angle is not fixed, it is possible to provide continuous print image in vertical photography to certain angle of inclination;Secondly, simplify the structure of current main-stream oblique photograph measurement apparatus, alleviate installation weight, add the activity duration, and angle shot is little by wind-force restriction continuously, plant maintenance easily and reduces the threshold that the oblique photograph of multi-angle low latitude is measured, and this device performance is stable, cost is cheaper.This aerial device shoots over the ground with on-fixed angle, imaging in the way of sweeping, angle continually varying aerial images in certain angle can be obtained, wide baseline high inclination-angle, the stereogram of high degree of overlapping can be collected, advantageously ensure that photographic image quality and improve small-sized unmanned plane mapping precision;Meanwhile, present configuration is simple, lighter weight, low cost, data acquisition modes idle job time flexible, stagnant length, working performance are high.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the side view of the present invention.
In the drawings, 1, shock-absorbing ball 2, gripper shoe 3, drive motor 4, little gear 5, gear wheel 6, rocking arm 7, hanger bar 8, camera pedestal gripper shoe 9, roller 10, Airborne Camera 11, small-sized unmanned plane 12, lower central plate 13, lithium battery 14, main control unit.
Detailed description of the invention
Such as Fig. 1, shown in Fig. 2, the present invention is realized in, the lower central plate 12 of small-sized unmanned plane 11 connects gripper shoe 2 by shock-absorbing ball 1 and forms damped platform, damped platform center vertically connects hanger bar 7, the upper end of hanger bar 7 fixing connection drives motor 3, drive the coaxially connected little gear 4 of motor 3, the engagement of little gear 4 connects gear wheel 5, one end of connecting rocker arm 6 on gear wheel 5, the other end of rocking arm 6 connects one end of camera pedestal gripper shoe 8 by roller 9, the bottom Vertical movements of described hanger bar 7 connects the center of camera pedestal gripper shoe 8, it is connected with Airborne Camera 10 in described camera pedestal gripper shoe 8, described driving motor 3 and Airborne Camera 10 connect lithium battery 13 and the main control unit 14 of small-sized unmanned plane.During use, by lithium battery 13 to driving motor 3 and Airborne Camera 10 to power, Airborne Camera 10 persistently shoots, and drives motor 3 band motion rocker arm that camera pedestal gripper shoe can be swung, and can efficiently complete the shooting of multi-angle, can realize vertical and oblique photograph.
Claims (2)
1. a sweep type low altitude photogrammetry device based on small-sized unmanned plane, it includes shock-absorbing ball, gripper shoe, drive motor, little gear, gear wheel, rocking arm, hanger bar, camera pedestal gripper shoe, roller, Airborne Camera, small-sized unmanned plane, it is characterized in that: the lower central plate of small-sized unmanned plane connects gripper shoe by shock-absorbing ball and forms damped platform, damped platform center vertically connects hanger bar, the upper end of hanger bar fixing connection drives motor, motors is driven to connect little gear, the engagement of little gear connects gear wheel, one end of connecting rocker arm on gear wheel, the other end of rocking arm connects one end of camera pedestal gripper shoe by roller, the bottom Vertical movements of described hanger bar connects the center of camera pedestal gripper shoe, it is connected with Airborne Camera in described camera pedestal gripper shoe.
A kind of sweep type low altitude photogrammetry device based on small-sized unmanned plane the most according to claim 1, it is characterised in that: described driving motor and Airborne Camera connect lithium battery and the main control unit of small-sized unmanned plane.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610385469.0A CN106017421A (en) | 2016-06-03 | 2016-06-03 | Sweeping-type low altitude photogrammetry device based on small light UAV |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610385469.0A CN106017421A (en) | 2016-06-03 | 2016-06-03 | Sweeping-type low altitude photogrammetry device based on small light UAV |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106017421A true CN106017421A (en) | 2016-10-12 |
Family
ID=57089800
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610385469.0A Pending CN106017421A (en) | 2016-06-03 | 2016-06-03 | Sweeping-type low altitude photogrammetry device based on small light UAV |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106017421A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107367267A (en) * | 2017-07-28 | 2017-11-21 | 长光卫星技术有限公司 | The method that aerial surveying camera and boat based on the imaging of stepping framing type take the photograph imaging |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2705120Y (en) * | 2004-04-16 | 2005-06-22 | 北京万东医疗装备股份有限公司 | X-ray digital pick up device |
US20080215204A1 (en) * | 2006-12-06 | 2008-09-04 | Mercury Computer Systems, Inc. | Methods, apparatus and systems for enhanced synthetic vision and multi-sensor data fusion to improve operational capabilities of unmanned aerial vehicles |
CN204705348U (en) * | 2015-06-24 | 2015-10-14 | 北京数维翔图高新技术有限公司 | A kind of unmanned plane oblique photograph device |
CN204776013U (en) * | 2015-06-04 | 2015-11-18 | 东莞中寰智能航空科技有限公司 | Six unmanned aerial vehicle |
CN105173100A (en) * | 2015-08-04 | 2015-12-23 | 致导科技(北京)有限公司 | Unmanned plane cloud deck and unmanned plane |
CN205664820U (en) * | 2016-06-03 | 2016-10-26 | 东华理工大学 | Formula low latitude photogrammetric survey device is swept to pendulum based on light unmanned aerial vehicle |
-
2016
- 2016-06-03 CN CN201610385469.0A patent/CN106017421A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2705120Y (en) * | 2004-04-16 | 2005-06-22 | 北京万东医疗装备股份有限公司 | X-ray digital pick up device |
US20080215204A1 (en) * | 2006-12-06 | 2008-09-04 | Mercury Computer Systems, Inc. | Methods, apparatus and systems for enhanced synthetic vision and multi-sensor data fusion to improve operational capabilities of unmanned aerial vehicles |
CN204776013U (en) * | 2015-06-04 | 2015-11-18 | 东莞中寰智能航空科技有限公司 | Six unmanned aerial vehicle |
CN204705348U (en) * | 2015-06-24 | 2015-10-14 | 北京数维翔图高新技术有限公司 | A kind of unmanned plane oblique photograph device |
CN105173100A (en) * | 2015-08-04 | 2015-12-23 | 致导科技(北京)有限公司 | Unmanned plane cloud deck and unmanned plane |
CN205664820U (en) * | 2016-06-03 | 2016-10-26 | 东华理工大学 | Formula low latitude photogrammetric survey device is swept to pendulum based on light unmanned aerial vehicle |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107367267A (en) * | 2017-07-28 | 2017-11-21 | 长光卫星技术有限公司 | The method that aerial surveying camera and boat based on the imaging of stepping framing type take the photograph imaging |
CN107367267B (en) * | 2017-07-28 | 2019-08-16 | 长光卫星技术有限公司 | The method that aerial surveying camera and boat based on the imaging of stepping framing type take the photograph imaging |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN207181919U (en) | A kind of rotary single-lens oblique photograph device for airborne vehicle | |
CN210000575U (en) | multifunctional mapping platform based on unmanned aerial vehicle remote sensing | |
CN107167117B (en) | A kind of multi-angle double camera oblique photograph apparatus and system | |
CN205770191U (en) | One is taken photo by plane unmanned plane | |
CN107272720A (en) | A kind of multi-angle oblique camera based on unmanned plane | |
CN205664820U (en) | Formula low latitude photogrammetric survey device is swept to pendulum based on light unmanned aerial vehicle | |
CN110015414A (en) | A kind of unmanned plane multi-angle oblique photographic equipment | |
CN205113735U (en) | Electronic fixed wing uavs of three camera oblique photography | |
CN113716056A (en) | Camera linkage that civil unmanned aerial vehicle was taken photo by plane | |
CN110949682A (en) | Indoor modeling unmanned aerial vehicle and indoor modeling method based on VR photography | |
CN206609424U (en) | Microlight-type variable-angle aviation oblique photograph system | |
CN106017421A (en) | Sweeping-type low altitude photogrammetry device based on small light UAV | |
CN207248166U (en) | Five camera lens oblique photographs measure camera | |
CN109556578A (en) | A kind of unmanned plane spirally sweeping measurement image pickup method | |
CN205594455U (en) | Three -dimensional modeling system of transmission line shaft tower | |
CN202953178U (en) | Minitype electric unmanned helicopter aerial photo system based on proposed triple axel type cloud platform | |
CN208984071U (en) | A kind of aviation oblique photograph system | |
CN208470123U (en) | Unmanned plane, which navigates, flies view finder unit | |
CN211308992U (en) | Efficient three-dimensional modeling cloud platform of oblique photography | |
CN205971881U (en) | Aerial panorama shooting equipment | |
CN113074698B (en) | Intelligent tower inclination detection system based on machine vision | |
CN109018393A (en) | A kind of photogrammetric mounting platform of adjustable unmanned plane | |
CN210890779U (en) | Rotation and sweep oblique photography cloud platform of pendulum combination | |
CN210235341U (en) | Based on unmanned aerial vehicle shoots measuring device | |
CN210338282U (en) | Many rotor unmanned aerial vehicle based on remote sensing system of patrolling and examining |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161012 |
|
RJ01 | Rejection of invention patent application after publication |