CN201235938Y - Machine-carried visible light image apparatus - Google Patents
Machine-carried visible light image apparatus Download PDFInfo
- Publication number
- CN201235938Y CN201235938Y CNU200820068273XU CN200820068273U CN201235938Y CN 201235938 Y CN201235938 Y CN 201235938Y CN U200820068273X U CNU200820068273X U CN U200820068273XU CN 200820068273 U CN200820068273 U CN 200820068273U CN 201235938 Y CN201235938 Y CN 201235938Y
- Authority
- CN
- China
- Prior art keywords
- airtight
- vibration isolation
- gondola
- camera
- axis
- 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.)
- Expired - Fee Related
Links
- 238000002955 isolation Methods 0.000 claims abstract description 17
- 230000003287 optical effect Effects 0.000 claims abstract description 15
- 238000005259 measurement Methods 0.000 claims description 6
- 239000006096 absorbing agent Substances 0.000 claims description 4
- 230000035939 shock Effects 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 abstract 2
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
Images
Landscapes
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The utility model relates to a machine load visible light image device which comprises a vibration isolation bracket connected with an aeroplane, wherein a rolling stand suspending cabin is arranged under the vibration isolation bracket. The visible light image device is characterized in that the rolling stand suspending cabin comprises an orientation servo device connected with the vibration isolation bracket, a pitching servo device is arranged on a rotating frame of the orientation servo device which is connected with an airtight suspending cabin, a television camera and a digital camera are arranged in the airtight suspending cabin, and the lens optical shaft of the television camera and the lens optical shaft of the digital camera point to the same direction and are corresponding to a perspective window arranged in the airtight suspending cabin. The utility model has the function of distant video recording, can remotely confirms object details by the digital camera so as to take photos and obtain evidence very clearly, can collect images and take photos for objects on the ground and in the air in an omnidirectional and multidirectional way, synchronously realizes video recording and high-resolution digital photo taking, and has function of object automatic follow, high automatization degree and convenient operation.
Description
Technical field
The utility model relates to a kind of airborne visible image device, belongs to the airborne photoelectric field, is specially adapted under the airborne circumstance ground, sea, aerial target be monitored, record a video and takes pictures.
Background technology
Airborne device for image can be in a wider context scouted, supervision, automatic tracking, is recorded a video and take pictures target, had the aircraft pod device for image that adopts tele camera and thermal infrared imager in the prior art, and the visible light aircraft pod camera head of single tele camera, though these devices have the video record function, but because the resolution of tele camera or thermal infrared imager is lower, be difficult to be implemented in remote affirmation of going up target detail, its functions of use is also perfect not to the utmost.
Summary of the invention
Technical problem to be solved in the utility model is to provide a kind of resolution height, the airborne visible image device that in-use performance is more perfect at the deficiency of above-mentioned prior art existence.
The utility model is that the technical scheme that problem adopted of the above-mentioned proposition of solution is: include and aircraft bonded assembly vibration isolation support, the turntable gondola is installed in vibration isolation support below, its difference is that described turntable gondola comprises the bearing servo device that links to each other with the vibration isolation support, the pitching actuating device is installed on the pivoted frame of bearing servo device, the pitching actuating device connects an airtight gondola, tele camera and digital camera are housed in airtight gondola, the camera lens optical axis of tele camera and the camera lens optical axis of digital camera point to identical, and the see-through window of offering with airtight gondola is corresponding.
Press such scheme, the camera lens optical axis direction of the camera lens optical axis of described tele camera and digital camera and the rotor shaft direction of pitching actuating device are perpendicular.
Press such scheme, described vibration isolation support comprises permanent seat, mounting shock absorber on the permanent seat, controlling party to guidepost be connected bearing.
Press such scheme, described bearing servo device comprises azimuth axis and the pivoted frame that links with it, azimuth axis and orientation torque motor and angle measurement element phase configuration, and install the conducting slip ring of transmission of electric signals.
Press such scheme, described pitching actuating device comprises the pitch axis that correspondence is installed in the pivoted frame both sides and links with airtight gondola, the pitch axis configuration pitching moment motor of a side, the pitch axis configuration pitching angle measurement element of opposite side.The axis direction of the azimuth axis of the axis direction of pitch axis and bearing servo device is perpendicular.
The beneficial effects of the utility model are: 1, tele camera be provided with simultaneously with digital camera and camera lens optical axis consistent, make this device not only have remote video record function, and can on remote, confirm target detail by digital photographing, realize the high-resolution evidence obtaining of taking pictures, make the functions of use of airborne visible image device more become perfect; 2, behind the input control signal, airtight gondola is turned to flexibly, can be comprehensive multidirectional made a video recording and take a picture in ground and aerial target, realize that video record and fine resolution digital photographing carry out synchronously, and has automatic tracking function to target, the degree of automation height uses easy to operate.
Description of drawings
The overall structure block diagram of an embodiment of Fig. 1 the utility model.
Vibration isolation support block diagram among embodiment of Fig. 2 the utility model.
An embodiment intermediate station of Fig. 3 the utility model gondola block diagram.
The positive view of an embodiment intermediate station of Fig. 4 the utility model gondola.
The specific embodiment
Further specify the utility model embodiment below in conjunction with accompanying drawing, include and aircraft bonded assembly vibration isolation support 1, described vibration isolation support 1 comprises and aircraft rack bonded assembly permanent seat 7, mounting shock absorber 3 on the permanent seat, and configuration guidepost 6, the upper end of guidepost 6 is equipped with linear bearing 5, the upper end of linear bearing 5, bumper 3 be connected bearing 4 and link to each other.Turntable gondola 2 is installed in vibration isolation support 1 below, and described turntable gondola 2 comprises the bearing servo device 9 that links to each other with the vibration isolation support, and pitching actuating device 8 is installed on the pivoted frame of bearing servo device, and the pitching actuating device connects an airtight gondola 10; The pivoted frame 17 that described bearing servo device 9 comprises azimuth axis 21 and links with it, azimuth axis 21 and orientation torque motor 18 and angle measurement element 19 phase configuration, and install the conducting slip ring 20 of transmission of electric signals, conducting slip ring 20 is used for Dynamic Signal and transmits.Described pitching actuating device 8 comprises that correspondence is installed in pivoted frame 17 both sides and the pitch axis configuration pitching moment motor 25 of pitch axis 15, one sides that link with airtight gondola 10, the pitch axis configuration pitching angle measurement element 16 of opposite side.Axis 22 directions of axis 24 directions of pitch axis and the azimuth axis of bearing servo device are perpendicular.The pitching actuating device links by pitch axis 15 and airtight gondola 10, controls the pitching rotation of airtight gondola 10, rotates displacement with the azimuth rotation of bearing servo device simultaneously, finishes the gyroscopic movement of two mutually perpendicular directions.Airtight gondola 10 is spherical in shape, offer two see-through window 11, in airtight gondola 10, tele camera 13 and digital camera 12 are housed by frame 23, the camera lens optical axis 14 of tele camera and the camera lens optical axis of digital camera 26 point to identical, and the see-through window of offering with airtight gondola 11 is corresponding, and shaft axis 24 directions of camera lens optical axis 26 directions of the camera lens optical axis 14 of described tele camera and digital camera and pitching actuating device are perpendicular.Described digital camera adopts the single anti-digital camera of fine resolution, has 1,000 ten thousand above pixels, and camera lens be a change multiple proportions long focal lengh lenses greatly, and both wide angle shot target overall picture closely can be grown burnt photographic subjects details again at a distance.
Claims (6)
1. airborne visible image device, include and aircraft bonded assembly vibration isolation support, the turntable gondola is installed in vibration isolation support below, it is characterized in that described turntable gondola comprises the bearing servo device that links to each other with the vibration isolation support, the pitching actuating device is installed on the pivoted frame of bearing servo device, the pitching actuating device connects an airtight gondola, tele camera and digital camera are housed in airtight gondola, the camera lens optical axis of tele camera and the camera lens optical axis of digital camera point to identical, and the see-through window of offering with airtight gondola is corresponding.
2. airborne visible image device according to claim 1 is characterized in that the rotor shaft direction of the camera lens optical axis direction of the camera lens optical axis of described tele camera and digital camera and pitching actuating device is perpendicular.
3. airborne visible image device according to claim 1 and 2 is characterized in that described vibration isolation support comprises permanent seat, mounting shock absorber on the permanent seat, controlling party to guidepost be connected bearing.
4. airborne visible image device according to claim 1 and 2, it is characterized in that described bearing servo device comprises azimuth axis and the pivoted frame that links with it, azimuth axis and orientation torque motor and angle measurement element phase configuration, and install the conducting slip ring of transmission of electric signals.
5. airborne visible image device according to claim 1 and 2, it is characterized in that described pitching actuating device comprises the pitch axis that correspondence is installed in the pivoted frame both sides and links with airtight gondola, the pitch axis configuration pitching moment motor of one side, the pitch axis configuration pitching angle measurement element of opposite side.The axis direction of the azimuth axis of the axis direction of pitch axis and bearing servo device is perpendicular.
6. airborne visible image device according to claim 3, it is characterized in that described vibration isolation support comprises and aircraft rack bonded assembly permanent seat, mounting shock absorber on the permanent seat, and configuration guidepost, the upper end of guidepost is equipped with linear bearing, the upper end of linear bearing, bumper be connected bearing and link to each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU200820068273XU CN201235938Y (en) | 2008-07-04 | 2008-07-04 | Machine-carried visible light image apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU200820068273XU CN201235938Y (en) | 2008-07-04 | 2008-07-04 | Machine-carried visible light image apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201235938Y true CN201235938Y (en) | 2009-05-13 |
Family
ID=40648676
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU200820068273XU Expired - Fee Related CN201235938Y (en) | 2008-07-04 | 2008-07-04 | Machine-carried visible light image apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201235938Y (en) |
Cited By (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101860684A (en) * | 2010-06-21 | 2010-10-13 | 福建福光数码科技有限公司 | Airborne turret with in-built CCD camera and forward looking infrared device and control system thereof |
| CN102610008A (en) * | 2012-03-31 | 2012-07-25 | 中国船舶重工集团公司第七一七研究所 | Ship borne light video searching and rescuing device |
| CN102717894A (en) * | 2012-06-14 | 2012-10-10 | 北京中陆航星科技有限公司 | Fixing structure of external onboard photoelectric pod on fixed-wing aircraft |
| CN102975856A (en) * | 2012-12-07 | 2013-03-20 | 天津大学 | Aviation nacelle equipment cabin |
| CN103395497A (en) * | 2013-08-14 | 2013-11-20 | 武汉华中天经光电系统有限公司 | Small-sized shooting gondola for unmanned aerial vehicle |
| CN103471472A (en) * | 2013-08-30 | 2013-12-25 | 昂海松 | Aerial anti-terrorist unit for firing mini-rocket to propel special ammunition |
| CN103523239A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | Installation structure of helicopter earth observation device |
| CN103616673A (en) * | 2013-12-03 | 2014-03-05 | 中国船舶重工集团公司第七一七研究所 | Tracking and pointing device for laser orientation interference |
| CN104058099A (en) * | 2014-06-30 | 2014-09-24 | 武汉华中天经光电系统有限公司 | Unmanned plane electro-optical pod |
| CN104776298A (en) * | 2015-05-06 | 2015-07-15 | 北京和普威视光电技术有限公司 | Electric direction positioning platform |
| CN104828256A (en) * | 2015-04-21 | 2015-08-12 | 杨珊珊 | An intelligent multi-mode flight shooting device and its flight control method |
| CN106005460A (en) * | 2016-07-28 | 2016-10-12 | 上海航天控制技术研究所 | Three-axis stable electro-optical pod for unmanned aerial vehicle |
| CN106161905A (en) * | 2016-08-31 | 2016-11-23 | 易瓦特科技股份公司 | It is applied to the double Shell mechanism of photoelectric nacelle |
| CN106275474A (en) * | 2016-08-31 | 2017-01-04 | 易瓦特科技股份公司 | There is the unmanned plane of photoelectric nacelle |
| CN106275475A (en) * | 2016-08-31 | 2017-01-04 | 易瓦特科技股份公司 | Airborne vehicle for information gathering |
| CN106275476A (en) * | 2016-08-31 | 2017-01-04 | 易瓦特科技股份公司 | It is applied to the arrangement for deflecting of photoelectric nacelle |
| CN106335648A (en) * | 2016-08-31 | 2017-01-18 | 易瓦特科技股份公司 | Unmanned aerial vehicle with image collection function |
| CN106341582A (en) * | 2016-08-31 | 2017-01-18 | 易瓦特科技股份公司 | Image acquisition equipment |
| CN106347696A (en) * | 2016-09-29 | 2017-01-25 | 武汉华中天经通视科技有限公司 | Light and small photoelectric pod |
| CN106394917A (en) * | 2016-08-31 | 2017-02-15 | 易瓦特科技股份公司 | Pod for multi-angle information collection |
| CN106394916A (en) * | 2016-08-31 | 2017-02-15 | 易瓦特科技股份公司 | Device for rotating collection |
| CN106742005A (en) * | 2016-11-21 | 2017-05-31 | 国网山东省电力公司电力科学研究院 | A kind of power-line patrolling photoelectric nacelle and depopulated helicopter |
| CN106742006A (en) * | 2016-08-31 | 2017-05-31 | 易瓦特科技股份公司 | Unmanned vehicle |
| CN108001696A (en) * | 2017-11-29 | 2018-05-08 | 中国航空工业集团公司洛阳电光设备研究所 | A kind of airborne compact photoelectric nacelle |
| CN108248880A (en) * | 2016-12-28 | 2018-07-06 | 北京卓翼智能科技有限公司 | For being tethered at two axis photoelectric nacelles of unmanned plane |
| CN109436344A (en) * | 2018-11-16 | 2019-03-08 | 航宇救生装备有限公司 | Airborne photography gondola based on parachute ballistic trajectory |
| CN112034893A (en) * | 2019-05-18 | 2020-12-04 | 九江精密测试技术研究所 | T-shaped structure searching and turning platform |
| CN112278301A (en) * | 2020-09-17 | 2021-01-29 | 河北汉光重工有限责任公司 | Two-shaft four-frame mechanism photoelectric pod with passive vibration isolation |
| CN114233799A (en) * | 2021-12-24 | 2022-03-25 | 中国科学院长春光学精密机械与物理研究所 | Machine carries two frame photoelectricity stabilized platform vibration isolation structures |
| WO2024158362A1 (en) * | 2023-01-27 | 2024-08-02 | Aselsan Elektroni̇k Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇ | An aerodynamic pod for aircrafts |
-
2008
- 2008-07-04 CN CNU200820068273XU patent/CN201235938Y/en not_active Expired - Fee Related
Cited By (41)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101860684A (en) * | 2010-06-21 | 2010-10-13 | 福建福光数码科技有限公司 | Airborne turret with in-built CCD camera and forward looking infrared device and control system thereof |
| CN102610008A (en) * | 2012-03-31 | 2012-07-25 | 中国船舶重工集团公司第七一七研究所 | Ship borne light video searching and rescuing device |
| CN102717894A (en) * | 2012-06-14 | 2012-10-10 | 北京中陆航星科技有限公司 | Fixing structure of external onboard photoelectric pod on fixed-wing aircraft |
| CN103523239A (en) * | 2012-07-06 | 2014-01-22 | 哈尔滨飞机工业集团有限责任公司 | Installation structure of helicopter earth observation device |
| CN103523239B (en) * | 2012-07-06 | 2015-12-02 | 哈尔滨飞机工业集团有限责任公司 | Installation structure of helicopter earth observation device |
| CN102975856A (en) * | 2012-12-07 | 2013-03-20 | 天津大学 | Aviation nacelle equipment cabin |
| CN103395497A (en) * | 2013-08-14 | 2013-11-20 | 武汉华中天经光电系统有限公司 | Small-sized shooting gondola for unmanned aerial vehicle |
| CN103395497B (en) * | 2013-08-14 | 2016-06-08 | 武汉华中天经光电系统有限公司 | A kind of small-sized shoot with video-corder gondola without man-machine |
| CN103471472B (en) * | 2013-08-30 | 2015-09-16 | 昂海松 | A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet |
| CN103471472A (en) * | 2013-08-30 | 2013-12-25 | 昂海松 | Aerial anti-terrorist unit for firing mini-rocket to propel special ammunition |
| CN103616673A (en) * | 2013-12-03 | 2014-03-05 | 中国船舶重工集团公司第七一七研究所 | Tracking and pointing device for laser orientation interference |
| CN103616673B (en) * | 2013-12-03 | 2016-01-20 | 中国船舶重工集团公司第七一七研究所 | A kind of track sight for laser orientation interference |
| CN104058099A (en) * | 2014-06-30 | 2014-09-24 | 武汉华中天经光电系统有限公司 | Unmanned plane electro-optical pod |
| CN104828256A (en) * | 2015-04-21 | 2015-08-12 | 杨珊珊 | An intelligent multi-mode flight shooting device and its flight control method |
| CN104828256B (en) * | 2015-04-21 | 2016-09-28 | 杨珊珊 | An intelligent multi-mode flight shooting device and its flight control method |
| CN104776298A (en) * | 2015-05-06 | 2015-07-15 | 北京和普威视光电技术有限公司 | Electric direction positioning platform |
| CN106005460A (en) * | 2016-07-28 | 2016-10-12 | 上海航天控制技术研究所 | Three-axis stable electro-optical pod for unmanned aerial vehicle |
| CN106005460B (en) * | 2016-07-28 | 2018-01-30 | 上海航天控制技术研究所 | A kind of unmanned plane three-axis stabilization photoelectric nacelle |
| CN106275476A (en) * | 2016-08-31 | 2017-01-04 | 易瓦特科技股份公司 | It is applied to the arrangement for deflecting of photoelectric nacelle |
| CN106394916A (en) * | 2016-08-31 | 2017-02-15 | 易瓦特科技股份公司 | Device for rotating collection |
| CN106275474A (en) * | 2016-08-31 | 2017-01-04 | 易瓦特科技股份公司 | There is the unmanned plane of photoelectric nacelle |
| CN106335648A (en) * | 2016-08-31 | 2017-01-18 | 易瓦特科技股份公司 | Unmanned aerial vehicle with image collection function |
| CN106341582A (en) * | 2016-08-31 | 2017-01-18 | 易瓦特科技股份公司 | Image acquisition equipment |
| CN106275475B (en) * | 2016-08-31 | 2019-01-15 | 易瓦特科技股份公司 | Aircraft for information collection |
| CN106394917A (en) * | 2016-08-31 | 2017-02-15 | 易瓦特科技股份公司 | Pod for multi-angle information collection |
| CN106275476B (en) * | 2016-08-31 | 2019-01-15 | 易瓦特科技股份公司 | Arrangement for deflecting applied to photoelectric nacelle |
| CN106275475A (en) * | 2016-08-31 | 2017-01-04 | 易瓦特科技股份公司 | Airborne vehicle for information gathering |
| CN106742006A (en) * | 2016-08-31 | 2017-05-31 | 易瓦特科技股份公司 | Unmanned vehicle |
| CN106161905A (en) * | 2016-08-31 | 2016-11-23 | 易瓦特科技股份公司 | It is applied to the double Shell mechanism of photoelectric nacelle |
| CN106347696A (en) * | 2016-09-29 | 2017-01-25 | 武汉华中天经通视科技有限公司 | Light and small photoelectric pod |
| CN106742005A (en) * | 2016-11-21 | 2017-05-31 | 国网山东省电力公司电力科学研究院 | A kind of power-line patrolling photoelectric nacelle and depopulated helicopter |
| CN108248880A (en) * | 2016-12-28 | 2018-07-06 | 北京卓翼智能科技有限公司 | For being tethered at two axis photoelectric nacelles of unmanned plane |
| CN108001696A (en) * | 2017-11-29 | 2018-05-08 | 中国航空工业集团公司洛阳电光设备研究所 | A kind of airborne compact photoelectric nacelle |
| CN109436344A (en) * | 2018-11-16 | 2019-03-08 | 航宇救生装备有限公司 | Airborne photography gondola based on parachute ballistic trajectory |
| CN109436344B (en) * | 2018-11-16 | 2022-04-22 | 航宇救生装备有限公司 | Airborne photography pod based on parachute ballistic trajectory |
| CN112034893A (en) * | 2019-05-18 | 2020-12-04 | 九江精密测试技术研究所 | T-shaped structure searching and turning platform |
| CN112278301A (en) * | 2020-09-17 | 2021-01-29 | 河北汉光重工有限责任公司 | Two-shaft four-frame mechanism photoelectric pod with passive vibration isolation |
| CN114233799A (en) * | 2021-12-24 | 2022-03-25 | 中国科学院长春光学精密机械与物理研究所 | Machine carries two frame photoelectricity stabilized platform vibration isolation structures |
| CN114233799B (en) * | 2021-12-24 | 2023-12-08 | 中国科学院长春光学精密机械与物理研究所 | Vibration isolation structure of airborne two-frame photoelectric stabilized platform |
| WO2024158362A1 (en) * | 2023-01-27 | 2024-08-02 | Aselsan Elektroni̇k Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇ | An aerodynamic pod for aircrafts |
| US12371188B2 (en) | 2023-01-27 | 2025-07-29 | Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi | Aerodynamic pod for aircrafts |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201235938Y (en) | Machine-carried visible light image apparatus | |
| CN212332992U (en) | Multifunctional three-light nacelle and system based on unmanned aerial vehicle carrying and unmanned aerial vehicle | |
| JP7048011B2 (en) | Imaging device | |
| CA2903259C (en) | All weather camera system and methods for control thereof | |
| US20130162761A1 (en) | Rotary image generator | |
| WO2010116370A1 (en) | Camera systems having multiple image sensors combined with a single axis mechanical gimbal | |
| CN210526874U (en) | Airborne three-light photoelectric pod system | |
| CN104058099A (en) | Unmanned plane electro-optical pod | |
| CN104796672A (en) | Emergency monitoring cloud platform device for unmanned aerial vehicle and operating method of emergency monitoring cloud platform device for unmanned aerial vehicle | |
| CN108495048A (en) | Dual camera image capture device based on cradle head control | |
| CN106347693B (en) | A kind of miniature gondola of changeable type unmanned plane | |
| CN110871898A (en) | A temperature measuring type photoelectric pod | |
| CN204272255U (en) | Vertical panoramic camera system | |
| CN206878992U (en) | A kind of vehicle-mounted panoramic video camera of linkage | |
| CN106742005A (en) | A kind of power-line patrolling photoelectric nacelle and depopulated helicopter | |
| CN101311818A (en) | Electronic navigation positioning panoramic view video camera | |
| CN211001903U (en) | Camera adjusting device that unmanned aerial vehicle observed and controlled | |
| CN108248815B (en) | Method and device for acquiring high-precision remote sensing data | |
| CN110493516A (en) | A kind of friction speed image motion compensation device and system | |
| CN108124127B (en) | Panoramic scanning monitoring system | |
| CN111741216A (en) | A method for capturing images from unmanned aerial vehicles | |
| CN204952261U (en) | Remote control aircraft of taking photo by plane | |
| CN204305216U (en) | A kind of full-view video image control tower | |
| CN205212943U (en) | Unmanned aerial vehicle overhead imaging system | |
| CN102833529A (en) | Multispectral monitoring system with distance measurement and image stabilization functions |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090513 Termination date: 20130704 |