CN204587320U - A kind of remotely sensed image is taken photo by plane system - Google Patents
A kind of remotely sensed image is taken photo by plane system Download PDFInfo
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- CN204587320U CN204587320U CN201520233439.9U CN201520233439U CN204587320U CN 204587320 U CN204587320 U CN 204587320U CN 201520233439 U CN201520233439 U CN 201520233439U CN 204587320 U CN204587320 U CN 204587320U
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- control module
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- sensed image
- image
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The utility model relates to a kind of remotely sensed image and to take photo by plane system, comprising: control module, the remote sensing equipment be connected with described control module, flight attitude control module and two groups of GPS positioning units; Described flight attitude control module comprises: gyroscope, acceleration pick-up, and the processor module for calculating flight attitude be connected with gyroscope, acceleration pick-up, and this processor module is connected with control module; GPS receiver module in described GPS positioning unit is connected with control module respectively by corresponding serial ports; The take photo by plane fuselage of system of described remotely sensed image is also provided with the touch-screen be connected with control module, and described control module is also connected with on-air radio Transmit-Receive Unit, and is connected with surface control station by on-air radio Transmit-Receive Unit; Described fuselage is also coated with solar panel, and described solar panel to be taken photo by plane system power supply to remotely sensed image by storage battery.
Description
Technical field
The utility model relates to remotely sensed image and to take photo by plane system.
Background technology
Remote sensing, as a kind of technological means that effectively can obtain geodata, is more and more widely used in each technical field; And airborne platform supplementing as space platform, can make up the problem that space platform cost is high, the lead time is long, airborne platform is particularly suitable for carrying out data acquisition among a small circle, is therefore widely used.
Utility model content
The purpose of this utility model is to provide a kind of remotely sensed image and takes photo by plane system, to solve the technical matters that remotely sensed image is taken photo by plane.
In order to solve the problems of the technologies described above, the utility model provides a kind of remotely sensed image and to take photo by plane system, comprising: control module, the remote sensing equipment be connected with described control module, flight attitude control module and two groups of GPS positioning units; Described flight attitude control module comprises: gyroscope, acceleration pick-up, and the processor module for calculating flight attitude be connected with gyroscope, acceleration pick-up, and this processor module is connected with control module; GPS receiver module in described GPS positioning unit is connected with control module respectively by corresponding serial ports; The take photo by plane fuselage of system of described remotely sensed image is also provided with the touch-screen be connected with control module, and described control module is also connected with on-air radio Transmit-Receive Unit, and is connected with surface control station by on-air radio Transmit-Receive Unit; Described fuselage is also coated with solar panel, and described solar panel to be taken photo by plane system power supply to remotely sensed image by storage battery.
Further, described on-air radio Transmit-Receive Unit comprises: WiFi module and CDMA module, and described WiFi module is connected with control module respectively with CDMA module.
Further, described remote sensing equipment comprises: image unit, light spectrum image-forming unit and survey sense unit, and wherein said image unit comprises: photographic camera, pick up camera; Described light spectrum image-forming unit comprises: multispectral scanner, imaging spectrometer; Survey sense unit to comprise: microwave radiometer, synthetic aperture radar.
The beneficial effects of the utility model are, remotely sensed image of the present utility model is taken photo by plane system, its by and two groups of GPS positioning units can effectively avoid because navigation fault causes aircraft to lose, and the photovoltaic panel covered by fuselage is to improve voyage, is particularly suitable for remote measurement and control.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is that remotely sensed image of the present utility model is taken photo by plane the functional block diagram of system.
Detailed description of the invention
By reference to the accompanying drawings the utility model is described in further detail now.These accompanying drawings are the schematic diagram of simplification, only basic structure of the present utility model are described in a schematic way, and therefore it only shows the formation relevant with the utility model.
As shown in Figure 1, a kind of remotely sensed image of the present utility model is taken photo by plane system, comprising: control module, the remote sensing equipment be connected with described control module, flight attitude control module and two groups of GPS positioning units; Described flight attitude control module comprises: gyroscope, acceleration pick-up, and the processor module for calculating flight attitude be connected with gyroscope, acceleration pick-up, and this processor module is connected with control module; GPS receiver module in described GPS positioning unit is connected with control module respectively by corresponding serial ports; The take photo by plane fuselage of system of described remotely sensed image is also provided with the touch-screen be connected with control module, and described control module is also connected with on-air radio Transmit-Receive Unit, and is connected with surface control station by on-air radio Transmit-Receive Unit; Described fuselage is also coated with solar panel, and described solar panel to be taken photo by plane system power supply to remotely sensed image by storage battery.
Wherein, realize redundancy navigation design by two groups of GPS positioning units, prevent from, due to a GPS positioning unit et out of order, aircraft being lost; Directly can carry out optimum configurations to remotely sensed image system of taking photo by plane by touch-screen, and check image, the video of shooting, directly check corresponding data; Solar panel improves the flying power of aircraft, can meet long-haul telemetry and to take photo by plane work; Also by flight attitude control module, the fuselage control area of aircraft is stablized, ensure the quality of data that observing and controlling gathers.
In order to meet multiple transmission of wireless signals, described on-air radio Transmit-Receive Unit comprises: WiFi module and CDMA module, and described WiFi module is connected with control module respectively with CDMA module.
Concrete, in order to be that measuring and control data is more comprehensive, described remote sensing equipment comprises: image unit, light spectrum image-forming unit and survey sense unit, and wherein said image unit comprises: photographic camera, pick up camera; Described light spectrum image-forming unit comprises: multispectral scanner, imaging spectrometer; Survey sense unit to comprise: microwave radiometer, synthetic aperture radar.
Optionally, described control module is such as but not limited to employing S3C2440 embedded chip.
With above-mentioned according to desirable embodiment of the present utility model for enlightenment, by above-mentioned description, relevant staff in the scope not departing from this utility model technological thought, can carry out various change and amendment completely.The technical scope of this utility model is not limited to the content on specification sheets, must determine its technical scope according to right.
Claims (3)
1. remotely sensed image is taken photo by plane a system, it is characterized in that, comprising: control module, the remote sensing equipment be connected with described control module, flight attitude control module and two groups of GPS positioning units;
Described flight attitude control module comprises: gyroscope, acceleration pick-up, and the processor module for calculating flight attitude be connected with gyroscope, acceleration pick-up, and this processor module is connected with control module;
GPS receiver module in described GPS positioning unit is connected with control module respectively by corresponding serial ports;
The take photo by plane fuselage of system of described remotely sensed image is also provided with the touch-screen be connected with control module, and
Described control module is also connected with on-air radio Transmit-Receive Unit, and is connected with surface control station by on-air radio Transmit-Receive Unit;
Described fuselage is also coated with solar panel, and described solar panel to be taken photo by plane system power supply to remotely sensed image by storage battery.
2. remotely sensed image as claimed in claim 1 is taken photo by plane system, and it is characterized in that, described on-air radio Transmit-Receive Unit comprises: WiFi module and CDMA module, and described WiFi module is connected with control module respectively with CDMA module.
3. remotely sensed image as claimed in claim 2 is taken photo by plane system, and it is characterized in that, described remote sensing equipment comprises: image unit, light spectrum image-forming unit and survey sense unit, wherein
Described image unit comprises: photographic camera, pick up camera;
Described light spectrum image-forming unit comprises: multispectral scanner, imaging spectrometer;
Survey sense unit to comprise: microwave radiometer, synthetic aperture radar.
Priority Applications (1)
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CN201520233439.9U CN204587320U (en) | 2015-04-17 | 2015-04-17 | A kind of remotely sensed image is taken photo by plane system |
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CN201520233439.9U CN204587320U (en) | 2015-04-17 | 2015-04-17 | A kind of remotely sensed image is taken photo by plane system |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106197474A (en) * | 2016-08-26 | 2016-12-07 | 云南电网有限责任公司 | A kind of high altitude localities helicopter flight condition checkout gear |
CN106767712A (en) * | 2017-02-27 | 2017-05-31 | 广西翼界科技有限公司 | Aerial survey aids in acquisition module with exterior orientation data |
CN106871875A (en) * | 2017-02-27 | 2017-06-20 | 广西翼界科技有限公司 | A kind of aviation measuring camera exterior orientation data syn-chronization acquisition device |
CN106871874A (en) * | 2017-02-27 | 2017-06-20 | 广西翼界科技有限公司 | A kind of POS management systems for being applied to aerial survey of unmanned aerial vehicle |
-
2015
- 2015-04-17 CN CN201520233439.9U patent/CN204587320U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106197474A (en) * | 2016-08-26 | 2016-12-07 | 云南电网有限责任公司 | A kind of high altitude localities helicopter flight condition checkout gear |
CN106767712A (en) * | 2017-02-27 | 2017-05-31 | 广西翼界科技有限公司 | Aerial survey aids in acquisition module with exterior orientation data |
CN106871875A (en) * | 2017-02-27 | 2017-06-20 | 广西翼界科技有限公司 | A kind of aviation measuring camera exterior orientation data syn-chronization acquisition device |
CN106871874A (en) * | 2017-02-27 | 2017-06-20 | 广西翼界科技有限公司 | A kind of POS management systems for being applied to aerial survey of unmanned aerial vehicle |
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CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150826 Termination date: 20160417 |
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CF01 | Termination of patent right due to non-payment of annual fee |