CN201517925U - Unmanned aerial vehicle remote sensing detector - Google Patents
Unmanned aerial vehicle remote sensing detector Download PDFInfo
- Publication number
- CN201517925U CN201517925U CN2009202183228U CN200920218322U CN201517925U CN 201517925 U CN201517925 U CN 201517925U CN 2009202183228 U CN2009202183228 U CN 2009202183228U CN 200920218322 U CN200920218322 U CN 200920218322U CN 201517925 U CN201517925 U CN 201517925U
- Authority
- CN
- China
- Prior art keywords
- remote sensing
- module
- aerial vehicle
- unmanned aerial
- vehicle remote
- 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 - Lifetime
Links
Images
Abstract
The utility model relates to an unmanned aerial vehicle remote sensing detector, which at least comprises a satellite positioning module, an inertial navigator and a data recording module. Accordingly, the unmanned aerial vehicle remote sensing detector completely records flying state, shooting angle and shooting time for obtaining information of navigation shooting state to help operation of subsequent study and analysis of shooting results, facilitates processing of subsequent images (such as image montage), and further provides relatively accurate ground image information.
Description
Technical field
The utility model is about a kind of unmanned aerial vehicle remote sensing detector, is meant a kind of for the unmanned aerial vehicle remote sensing detector of carrying out empty bat or location tasks especially.
Background technology
When being engaged in the sky bat task of so-called shooting on the spot in the past, carry out to lease large-scale flight carrier (as aircraft or helicopter) mostly, except the huge funds of needs cost remove to pay POL expense and lease the expense, relevant Camera crews must undertake the risk of flight safety, the carrier technology is very ripe even if fly now, but still can't absolutely guarantee passenger's safety.
Therefore, just there is the related personnel to develop a kind of filming instrument is arranged on the large-scale flight carrier (as position of ventral below), angle according to the angle of flight carrier sporting flying and inclination comes corresponding control filming instrument camera lens to be photographed allows filming instrument can take required geography information voluntarily.
Yet, along with small-sized unmanned flight carrier technology is more and more ripe, existing replacement tradition gradually needs the trend of the performed task of large-scale flight carrier of pilot driver, because except the cost that can reduce aerial mission, utilize unmanned flight carrier to enter dangerous spatial domain, also can avoid personnel's injures and deaths.
But because the volume of unmanned flight carrier is less, the influence of environment (as interference in air flow) when being easy to be subjected to flying, the situation that deviation is arranged when causing unmanned flight carrier to navigate by water aloft, and such phenomenon has produced a little flaw for utilizing the unmanned vehicle to carry out empty bat task, because, have only under the most stable flight situation, best photographic effects is just arranged, can provide follow-up study to analyze operation with the most accurate geographical image information.
Therefore, external environmental factor be difficult to overcome in artificial mode and the inborn shortcoming of miniature self-service flight carrier under, design a preferable unmanned flight carrier filming instrument, obtain the image information with the best achievement in cinematography effect, be to carry out the target that the relevant manufacturer of empty bat task makes great efforts research and development always.
The utility model content
The inventor is actively to set about going in for the study because the unmanned flight of above-mentioned tradition carrier reduces the shortcoming of taking quality of achievement because of being vulnerable to environmental interference, through constantly test and effort, develops the utility model finally.
It is a kind of for the unmanned aerial vehicle remote sensing detector of carrying out empty bat or location tasks that the fundamental purpose of the utility model is to provide, see through the information that obtains the navigation shooting state, help follow-up study and analyze the operation of shooting results, can obtain more accurate and preferable geographical image information.
In order to reach above-mentioned utility model purpose, the unmanned aerial vehicle remote sensing detector of the utility model, it comprises:
One power module, required electric power when being used to provide this unmanned aerial vehicle remote sensing detector running;
One satellite positioning module, it has an antenna at least and is connected in this power module, this antenna see through to receive outside global satellite system (Global Positioning System, GPS) in the signal that sent of satellite obtain the present longitude of this unmanned aerial vehicle remote sensing detector, latitude, sea level on the average and accurate satellite time;
One remote sensing module, it is connected in this power module and sees through the image information that remote sensing (RemoteSensing) technology obtains ground;
One inertial navigator, it is connected in this power module, and come the outer orientation attitude information of this remote sensing module of synchronous measure when surveying according to the satellite time that this satellite positioning module received, wherein, this outer orientation attitude information includes magnetic azimuth angle value, luffing angle value and lift-over angle value respectively; And
One data recording (Data Log) module, it is connected to this power module, this satellite positioning module, this remote sensing module and this inertial navigator, and it sees through the image information that the reception satellite time that this satellite positioning module transmitted comes longitude, latitude, sea level on the average, accurate satellite time, outer orientation attitude information and the ground of this unmanned aerial vehicle remote sensing detector of synchronous recording when operation.
Based on general small-sized unmanned flight carrier, the influence of environment (as interference in air flow) when being easy to be subjected to flying, the situation that deviation is arranged when causing unmanned flight carrier to navigate by water aloft, therefore, the unmanned aerial vehicle remote sensing detector of the utility model is provided with a satellite positioning module and an inertial navigator especially, and carry out synchronization job according to satellite time, come complete record state of flight, shooting angle and shooting time, in order to the processing (as image joint) of follow-up image, and then provide and have ground image information more accurately.
Description of drawings
Fig. 1 is the unmanned aerial vehicle remote sensing detector carriage composition of the utility model.
Fig. 2 is the process flow diagram of one of the utility model embodiment.
[primary clustering symbol description]
1 unmanned aerial vehicle remote sensing detector, 14 data recording modules
10 power modules, 20 steps A
11 satellite positioning module, 21 step B
110 antennas, 22 step C
12 remote sensing modules, 23 step D
13 inertial navigators
Embodiment
Please refer to shown in Figure 1, the unmanned aerial vehicle remote sensing detector 1 of the utility model, it comprises:
One power module 10, required electric power when being used to provide this unmanned aerial vehicle remote sensing detector 1 running;
One satellite positioning module 11, it has an antenna 110 at least and is connected in this power module 10, and this antenna 110 sees through and receives satellite sent in the outside global satellite system signal and obtain this unmanned aerial vehicle remote sensing detector 1 present longitude, latitude, sea level on the average and accurate satellite time;
One remote sensing module 12, it is connected in this power module 10 and sees through the image information that the remote sensing technology obtains ground;
One inertial navigator 13, it is connected in this power module 10, and comes the outer orientation attitude information of this remote sensing module 12 of synchronous measure when surveying according to the satellite time that this satellite positioning module 11 is received; And
One data recording (Data Log) module 14, it is connected to this power module 10, this satellite positioning module 11, this remote sensing module 12 and this inertial navigator 13, and its satellite time that is transmitted through this satellite positioning module 11 of reception comes longitude, latitude, sea level on the average, accurate satellite time, outer orientation attitude information, the image information on ground and the time of taking pictures of this unmanned aerial vehicle remote sensing detector 1 of synchronous recording when operation.
Wherein, this remote sensing module 12 can be a camera, an infrared imaging machine or a radar bidimensional image and becomes camera.
Wherein, this outer orientation attitude information includes magnetic azimuth angle value, luffing angle value and lift-over angle value respectively.
Please refer to Figure 1 and Figure 2, the operation workflow when clapping in flight is empty for the unmanned aerial vehicle remote sensing detector 1 that more can understand the utility model, the spy carries out the explanation of flow process with an embodiment, and it includes:
Steps A 20: power-on, required electric power when allowing this power module 10 that 1 running of this unmanned aerial vehicle remote sensing detector is provided starts this satellite positioning module 11, this remote sensing module 12, this inertial navigator 13 and this data recording module 14;
Step B21: this satellite positioning module 11 receives the signal of outside satellite, with longitude, latitude, sea level on the average and the accurate satellite time of obtaining this unmanned aerial vehicle remote sensing detector 1;
Step C22: this inertial navigator 13 and this data recording module 14 receive this satellite time respectively and come the outer orientation attitude information of this remote sensing module 12 of synchronous measure when surveying; And
Step D23: this data recording module 14 these unmanned aerial vehicle remote sensing detectors 1 of record longitude, latitude, sea level on the average, accurate satellite time, outer orientation attitude information, the image information on ground and time of taking pictures when operation.
Comprehensively above-mentioned, the unmanned aerial vehicle remote sensing detector of the utility model is provided with a satellite positioning module and an inertial navigator especially, and see through satellite time and carry out synchronization job, come complete record state of flight, shooting angle and shooting time, in order to the processing (as image joint) of follow-up image, and then provide and have ground image information more accurately.
The above only is the preferred embodiment of the utility model, when the scope that can not limit the utility model enforcement with this; All simple equivalent of being done according to the utility model claim and utility model description change and modify, and all should still belong in the scope that this novel patent contains.
Claims (3)
1. unmanned aerial vehicle remote sensing detector is characterized in that it comprises:
One power module, required electric power when being used to provide this unmanned aerial vehicle remote sensing detector running;
One satellite positioning module, it has an antenna at least and is connected in this power module, and this antenna sees through the signal that satellite sent in the global satellite system that receives the outside and obtains the present longitude of this unmanned aerial vehicle remote sensing detector, latitude, sea level on the average and accurate satellite time;
One remote sensing module, it is connected in this power module and sees through the image information that the remote sensing technology obtains ground;
One inertial navigator, it is connected in this power module, and comes the outer orientation attitude information of this remote sensing module of synchronous measure when surveying according to the satellite time that this satellite positioning module received; And
One data recording module, it is connected to this power module, this satellite positioning module, this remote sensing module and this inertial navigator, and it sees through the reception satellite time that this satellite positioning module transmitted and comes longitude, latitude, sea level on the average, accurate satellite time, outer orientation attitude information, the image information on ground and the time of taking pictures of this unmanned aerial vehicle remote sensing detector of synchronous recording when operation.
2. unmanned aerial vehicle remote sensing detector according to claim 1 is characterized in that, described remote sensing module is a camera.
3. unmanned aerial vehicle remote sensing detector according to claim 1 is characterized in that, described remote sensing module is an infrared imaging machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202183228U CN201517925U (en) | 2009-10-13 | 2009-10-13 | Unmanned aerial vehicle remote sensing detector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202183228U CN201517925U (en) | 2009-10-13 | 2009-10-13 | Unmanned aerial vehicle remote sensing detector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201517925U true CN201517925U (en) | 2010-06-30 |
Family
ID=42498647
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009202183228U Expired - Lifetime CN201517925U (en) | 2009-10-13 | 2009-10-13 | Unmanned aerial vehicle remote sensing detector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201517925U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102538747A (en) * | 2010-12-20 | 2012-07-04 | 西安韦德沃德航空科技有限公司 | System and method for measuring height of cloud base |
| CN102591356A (en) * | 2012-03-13 | 2012-07-18 | 中国科学院对地观测与数字地球科学中心 | Navigation control system and method for achieving navigation control |
| WO2013083038A1 (en) * | 2011-12-08 | 2013-06-13 | 腾讯科技（深圳）有限公司 | Picture positioning method and system based on mobile terminal navigation function |
| CN103234525A (en) * | 2013-04-12 | 2013-08-07 | 王德荣 | Geology shooting instrument |
| CN103376455A (en) * | 2012-04-23 | 2013-10-30 | 中国科学院、水利部成都山地灾害与环境研究所 | Sensor posture coordinate recording device applicable to low-altitude unpiloted remote sensing platform |
| CN103546468A (en) * | 2013-10-22 | 2014-01-29 | 中测新图(北京)遥感技术有限责任公司 | Unmanned aerial vehicle flight data transmission method and system based on Beidou satellite |
| CN104501779A (en) * | 2015-01-09 | 2015-04-08 | 中国人民解放军63961部队 | High-accuracy target positioning method of unmanned plane on basis of multi-station measurement |
-
2009
- 2009-10-13 CN CN2009202183228U patent/CN201517925U/en not_active Expired - Lifetime
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102538747A (en) * | 2010-12-20 | 2012-07-04 | 西安韦德沃德航空科技有限公司 | System and method for measuring height of cloud base |
| WO2013083038A1 (en) * | 2011-12-08 | 2013-06-13 | 腾讯科技（深圳）有限公司 | Picture positioning method and system based on mobile terminal navigation function |
| US8976266B2 (en) | 2011-12-08 | 2015-03-10 | Tencent Technology (Shenzhen) Company Limited | Picture locating method and system based on navigation function of mobile terminal |
| CN102591356A (en) * | 2012-03-13 | 2012-07-18 | 中国科学院对地观测与数字地球科学中心 | Navigation control system and method for achieving navigation control |
| CN103376455A (en) * | 2012-04-23 | 2013-10-30 | 中国科学院、水利部成都山地灾害与环境研究所 | Sensor posture coordinate recording device applicable to low-altitude unpiloted remote sensing platform |
| CN103234525A (en) * | 2013-04-12 | 2013-08-07 | 王德荣 | Geology shooting instrument |
| CN103234525B (en) * | 2013-04-12 | 2016-09-14 | 王德文 | Geology recording instrument |
| CN103546468A (en) * | 2013-10-22 | 2014-01-29 | 中测新图(北京)遥感技术有限责任公司 | Unmanned aerial vehicle flight data transmission method and system based on Beidou satellite |
| CN104501779A (en) * | 2015-01-09 | 2015-04-08 | 中国人民解放军63961部队 | High-accuracy target positioning method of unmanned plane on basis of multi-station measurement |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201517925U (en) | Unmanned aerial vehicle remote sensing detector | |
| CN110308457B (en) | Unmanned aerial vehicle-based power transmission line inspection system | |
| CN109596118B (en) | Method and equipment for acquiring spatial position information of target object | |
| CA2773303C (en) | Systems and methods of capturing large area images in detail including cascaded cameras and/or calibration features | |
| JP6016264B2 (en) | Visual stakeout | |
| CN106526551A (en) | Radar antenna dynamic performance testing system and method | |
| CN103822631B (en) | Localization method and the device of a kind of satellite towards rotor and the combination of optical flow field vision | |
| CN105549060A (en) | Object positioning system based on position and attitude of airborne photoelectric gondola | |
| CN105182995A (en) | Automatic unmanned plane landing system | |
| CN105627991A (en) | Real-time panoramic stitching method and system for unmanned aerial vehicle images | |
| CN103453891B (en) | Small-sized unmanned aerial vehicle onboard looks three-dimensional airborne remote sensing device and system more | |
| CN106468547A (en) | Utilize multiple optical pickocffs is independent of global positioning system for self-conductance aircraft（“GPS”）Navigation system | |
| KR102239562B1 (en) | Fusion system between airborne and terrestrial observation data | |
| EP0148704A2 (en) | Monitoring method for target localization by way of an unmanned aircraft | |
| CN105388908A (en) | Machine vision-based unmanned aerial vehicle positioned landing method and system | |
| CN106872369A (en) | The airborne hyperspectral imaging system and method for a kind of spilled oil monitoring | |
| US8620023B1 (en) | Object detection and location system | |
| US20200333140A1 (en) | Image data capturing arrangement | |
| Walko et al. | Flying a helicopter with the HoloLens as head-mounted display | |
| Calantropio et al. | 360 images for UAV multisensor data fusion: First tests and results | |
| CN112013716A (en) | Method for capturing fast moving target by television seeker simulation system | |
| CN109084733A (en) | A kind of intelligence remote sensing mapping system | |
| TWM377016U (en) | Remote sensing system carried on unmanned aerial vehicle | |
| JP7332445B2 (en) | Display control device, display control method and display control program | |
| Melega | Design, assembly and test of an airborne automated imaging system for environmental monitoring |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: GEO AEROSPACE TECHNOLOGY CO., LTD. Free format text: FORMER OWNER: GEO SAT INFORMATICS TECHNOLOGY CORP. Effective date: 20150909 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150909 Address after: Chinese Taiwan East District of Tainan city in the East Gate Road three Huwei No. 253 12 floor Patentee after: Jingwei Polytron Technologies Inc Address before: Taiwan, China Tainan East Road, East Gate Road, No. 3, No. 12, building 253 Patentee before: GeoSat Informatics Technology Co. |
|
| CX01 | Expiry of patent term |
Granted publication date: 20100630 |
|
| CX01 | Expiry of patent term |