CN215155742U - Airborne hyperspectral imaging device for flight platform and connecting structure - Google Patents
Airborne hyperspectral imaging device for flight platform and connecting structure Download PDFInfo
- Publication number
- CN215155742U CN215155742U CN202121399122.4U CN202121399122U CN215155742U CN 215155742 U CN215155742 U CN 215155742U CN 202121399122 U CN202121399122 U CN 202121399122U CN 215155742 U CN215155742 U CN 215155742U
- Authority
- CN
- China
- Prior art keywords
- mounting plate
- mounting
- personal computer
- industrial personal
- pos system
- 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.)
- Active
Links
Images
Landscapes
- Studio Devices (AREA)
Abstract
The utility model discloses an airborne high spectrum imaging device and connection structure for flight platform, airborne high spectrum imaging device includes: a connection structure for detachable mounting on a flight platform; the POS system, the industrial personal computer and the hyperspectral camera are detachably arranged on the three end faces of the connecting structure; the solid state disk is externally arranged on the industrial personal computer; the industrial personal computer is respectively connected with the hyperspectral camera, the solid state disk and the POS system. The utility model discloses an airborne hyperspectral imaging device, compact structure, easy dismounting, overall structure is rationally distributed, and the integration has high accuracy POS system, through connection structure with hyperspectral imaging device fast, conveniently carry on flight platform, avoid the problem of the image deformation because of flight platform is unstable and lead to.
Description
Technical Field
The utility model relates to a high spectrum remote sensing technical field especially relates to an airborne high spectrum imaging device and connection structure for flight platform.
Background
With the progress of electronic science and technology and the development of the industrial level of computers, small-sized multi-rotor unmanned flight equipment gradually enters the living field of people, and particularly the commercialization of a four-axis aircraft is greatly developed; for example, in some occasions such as shooting, article transfer, flight performance and the like, small-sized multi-rotor unmanned aerial devices are often needed to perform corresponding tasks.
However, the unmanned aerial vehicle in the prior art only considers the implementation of structural functions, does not systematically consider the overall layout of the unmanned aerial vehicle, is usually external to most electronic devices (such as an electronic governor and the like are externally arranged outside the vehicle body), is not beneficial to protecting the electronic devices, and makes the connection of the unmanned aerial vehicle messy, and is difficult to quickly find out the problem when the problem occurs. In addition, the battery is usually bound by magic tape, so that the battery after installation is not firm, relative movement of the position is likely to occur in the flying process, the stability of the unmanned aerial vehicle is influenced, and the position is different when the battery is installed every time, and the stability of the unmanned aerial vehicle is also influenced.
Disclosure of Invention
The utility model aims at solving above-mentioned problem, provide an airborne hyperspectral imaging device and connection structure for flight platform, compact structure, easy dismounting, overall structure is rationally distributed, and the integration has high accuracy POS system, through connection structure with hyperspectral imaging device fast, conveniently carry on flight platform, avoid the problem of the image deformation because of flight platform is unstable and lead to.
In order to realize the above object of the present invention, the present invention provides a connection structure for flying platform, which includes: a first mounting plate for mounting a POS system thereon; the second mounting plate is used for mounting the industrial personal computer; a third mounting plate for mounting a hyperspectral camera thereon; wherein, the first mounting panel, the second mounting panel, the third mounting panel are two-by-two perpendicular.
The first mounting plate, the second mounting plate and the third mounting plate are connected in a detachable or non-detachable mode.
The first mounting plate is provided with an extension part which is detachably mounted on the flying platform, and the POS system is mounted on an end face perpendicular to the extension part.
The second mounting plate is vertically connected with the other end face of the first mounting plate, and an industrial personal computer is mounted on the end face, perpendicular to the end face of the first mounting plate, of the second mounting plate, where the POS system is mounted.
The third mounting plate is vertically connected with one side face of the second mounting plate, and a hyperspectral camera is mounted on the end face, perpendicular to the end face, used for mounting the industrial personal computer, of the second mounting plate; or the third mounting plate is vertically connected with the other end face of the first mounting plate, and the hyperspectral cameras are arranged on the end faces, which are perpendicular to the end face of the first mounting plate for mounting the POS system and the end face of the second mounting plate for mounting the industrial personal computer in pairs.
Furthermore, the utility model also provides an airborne hyperspectral imaging device for flight platform, it includes: a connection structure as described above for detachable mounting on a flying platform; the POS system, the industrial personal computer and the hyperspectral camera are detachably arranged on the three end faces of the connecting structure; the solid state disk is externally arranged on the industrial personal computer; the industrial personal computer is connected with the hyperspectral camera, the solid state disk and the POS system respectively, and data collected by the hyperspectral camera is transmitted to the industrial personal computer and stored in the solid state disk.
The connecting structure comprises a first mounting plate, a second mounting plate and a third mounting plate which are connected in a pairwise detachable mode or in a non-detachable mode.
Preferably, the first mounting plate, the second mounting plate and the third mounting plate are perpendicular to each other in pairs.
Preferably, the first mounting plate is provided with an extension for detachable mounting on the flying platform, and the POS system is mounted on an end face perpendicular to the extension.
Preferably, the second mounting plate is vertically connected with the other end face of the first mounting plate, and an industrial personal computer is mounted on the end face of the second mounting plate, which is perpendicular to the end face of the first mounting plate, on which the POS system is mounted.
Preferably, the third mounting panel is connected with a side face of the second mounting panel perpendicularly, and the hyperspectral camera is installed on the end face of the third mounting panel perpendicular to the end face of the second mounting panel, which is used for installing the industrial personal computer.
Preferably, one side of the industrial personal computer, which is far away from the surface, is provided with two protruding extension parts for forming a bayonet, and the bayonet is used for arranging a solid state disk.
Preferably, a hard disk protection shell used for protecting and arranging the solid state disk is sleeved at the rear end of the solid state disk.
Preferably, the POS system is provided with one or more of ETH, IO, PWR, GNSS _1, GNSS _2, 4G interfaces, and is provided with a SIMCARD slot.
Wherein, flight platform is for having man-machine or unmanned aerial vehicle.
Compared with the prior art, the utility model discloses an airborne hyperspectral imaging device and connection structure for flying platform has following advantage:
the utility model discloses an airborne hyperspectral imaging device for a flight platform, including hyperspectral camera, industrial computer, POS system, solid state hard drives, connection structure, hyperspectral camera, industrial computer, POS system settle on connection structure, solid state hard drives externally locate above the industrial computer, the industrial computer respectively with hyperspectral camera, solid state hard drives and POS system connection, overall structure is compact, easy dismouting; the extension part for mounting the flight platform through the connecting structure can be quickly connected with the flight platform, can meet the mounting requirements of different flight platforms, and is low in maintenance and test cost; the POS system has high precision, the positioning data is more accurate, the POS system can be in time synchronization with the hyperspectral camera, and high-quality and high-precision data achievements are acquired under the condition that the flight platform is unstable.
The embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
Drawings
FIG. 1 is a structural diagram of an airborne hyperspectral imaging device for a flight platform according to an embodiment of the invention;
fig. 2 is a schematic view of a connection structure according to an embodiment of the present invention;
fig. 3 is a schematic diagram of a POS system according to an embodiment of the present invention.
Detailed Description
As shown in fig. 2, for the structural schematic diagram of the connection structure for a flight platform provided in the embodiment of the present invention, as can be seen from the figure, the connection structure includes: a first mounting plate 8 for mounting a POS system thereon; a second mounting plate 10 for mounting an industrial personal computer thereon; a third mounting plate 9 for mounting a hyperspectral camera thereon; the first mounting plate 8, the second mounting plate 10 and the third mounting plate 9 are vertical to each other, and can be detachably connected or not detachably connected. Preferably, every two of the connecting rods are detachably connected together.
Wherein, as shown in fig. 2, the first mounting panel 8, the second mounting panel 10, the third mounting panel 9 are two by two perpendicular to install hyperspectral camera 1, POS system 2, industrial computer 3 on each mounting panel, make whole compact structure, easy dismouting, maintain, test cost are low.
When in connection, different connection schemes can be adopted, for example, the hyperspectral camera mounting plate (i.e. the third mounting plate 9), the industrial personal computer mounting plate (i.e. the second mounting plate 10) can be respectively connected with the POS system mounting plate (i.e. the first mounting plate 8) through screws, or the hyperspectral camera mounting plate (i.e. the third mounting plate 9) is connected with the POS system mounting plate (i.e. the first mounting plate 8) through screws, and the industrial personal computer mounting plate (i.e. the second mounting plate 10) is connected with the hyperspectral camera mounting plate (i.e. the third mounting plate 9) through screws, of course, the mounting plates can be detachably connected together in other modes, but the requirement that the three mounting plates are perpendicular to each other is met, so that the hyperspectral camera 1, the POS system 2 and the industrial personal computer 3 are integrated on the same connecting structure, and therefore, the hyperspectral camera 1, the industrial personal computer 3 can be conveniently connected through the connecting structure, And the POS system 2 and the industrial personal computer 3 are quickly carried on the flight platform.
The first mounting plate 8 is provided with an extension portion for being detachably mounted on a flight platform (not shown in the figure), the POS system is mounted on a terminal surface perpendicular to the terminal surface of the extension portion for connecting the flight platform, the terminal surface of the extension portion is provided with a plurality of screw holes 11, the extension portion can be connected with the flight platform through screws, and therefore the connection structure is connected with the flight platform, all components mounted on the connection structure can be hung on the flight platform, and the flight platform is a manned machine or an unmanned aerial vehicle.
The second mounting plate 10 is connected perpendicularly to the other end surface of the first mounting plate 8 (i.e., the other end surface is opposite to the end surface of the first mounting plate on which the POS machine is mounted), and the industrial personal computer is mounted on the end surface perpendicular to the end surface of the first mounting plate 8 on which the POS system is mounted. The third mounting plate 9 is vertically connected with one side face of the second mounting plate 10, the hyperspectral camera is mounted on the end face, perpendicular to the end face, used for mounting the industrial personal computer, of the second mounting plate 10, or the third mounting plate 9 is vertically connected with the other end face of the first mounting plate 8, and the hyperspectral camera is mounted on the end face, used for mounting the POS system, of the first mounting plate 8 and the end face, used for mounting the industrial personal computer, of the second mounting plate 10, perpendicular to each other.
The utility model discloses except providing foretell connection structure, still provide the airborne high spectrum imaging device who is used for flight platform, it includes: a connection structure as described above for detachable mounting on a flying platform; the POS system, the industrial personal computer and the hyperspectral camera are detachably arranged on the three end faces of the connecting structure; the solid state disk is externally arranged on the industrial personal computer; the industrial personal computer is connected with the hyperspectral camera, the solid state disk and the POS system respectively, and data collected by the hyperspectral camera is transmitted to the industrial personal computer and stored in the solid state disk. The flying platform can be an unmanned plane or an unmanned plane.
Specifically, the utility model discloses an airborne high spectrum imaging device for flight platform includes: the system comprises a hyperspectral camera 1, a POS system 2, an industrial personal computer 3, a solid state disk 4 and a connecting structure. The hyperspectral camera 1, the POS system 2 and the industrial personal computer 3 are arranged on the connecting structure through screws, the relative positions are fixed, the overall structure is compact, the assembly and disassembly are easy, and the maintenance and test cost is low; the solid state disk 4 is arranged outside the industrial personal computer 3 through a bayonet formed by the two protruding extending parts 5.
The solid state disk 4 is connected with the industrial personal computer 3 through an SATA3.0 interface and is used for storing data collected by the hyperspectral camera 1; the hyperspectral camera 1 and the POS system 2 are respectively connected to a USB interface on the industrial personal computer 3, and the industrial personal computer 3 is loaded with special data acquisition control software and used for hyperspectral acquisition control; the data acquisition control software has a time synchronization function and realizes the synchronous acquisition of the data of the hyperspectral camera 1 and the POS system 2.
Wherein, the utility model discloses hyperspectral camera 1 can be for pushing away the Pika L hyperspectral camera of sweeping the formation of image for gather ground object image and spectral information, it includes camera lens 6, the model of the different specifications of the 6 optional uses of camera lens, thereby can have different angles of vision, and camera lens 6 is connected with hyperspectral camera 1 through the hickey mount pad of hyperspectral camera 1. The data collected by the hyperspectral camera 1 are transmitted to the industrial personal computer 3 and stored in the solid state disk 4.
The utility model discloses POS system 2 of embodiment is provided with one or more in ETH, IO, PWR, GNSS _1, GNSS _2, the 4G interface, and is provided with the SIMCARD slot. Preferably, the POS system 2 of the present embodiment may simultaneously set the following interfaces: setting an ETH interface 12 for network communication; an IO interface 13 is arranged and used for connecting and communicating with the industrial personal computer 3; a PWR interface 14 is provided for supplying power to the POS system 2; setting a GNSS _1 interface 15 and a GNSS _2 interface 16 for connecting a GNSS antenna to acquire satellite signals; a 4G interface 17 is arranged for connecting a 4G antenna; a SIMCARD slot 18 is provided for placement of a SIMCARD; according to the POS system, the updating frequency of the combined positioning data reaches 100Hz, the plane position precision is 1cm, the elevation precision is 2cm, the pitch angle precision and the roll angle precision reach 0.005 degrees, the course angle precision reaches 0.01 degrees, the precision is high, and time synchronization can be carried out with the hyperspectral camera.
The POS system 2 and the hyperspectral camera 1 in the embodiment can be fixed in relative positions through the connecting structure, and through time synchronization, the position and posture information corresponding to each line of data of the hyperspectral camera 1 can be acquired, so that high-precision geometric correction of spectral images is realized.
The solid state disk 4 of the embodiment includes a hard disk protection shell 7, and the hard disk protection shell 7 is sleeved at the rear end 4 of the solid state disk and used for protecting and arranging the solid state disk.
The industrial computer of this embodiment can adopt Intel BLKNUC7i7DNK1E NUC computer platform, loads the special data acquisition control software in the industrial computer, sets up the extension of two salients as the bayonet socket in industrial computer one side, can settle and fix solid state hard drives through the bayonet socket.
To sum up, the utility model provides a machine carries high spectral imaging system, including high spectrum camera, industrial computer, POS system, solid state hard drives, connection structure, high spectrum camera, industrial computer, POS system can be dismantled and settle on connection structure, and solid state hard drives externally arrange the industrial computer top in, and the industrial computer respectively with high spectrum camera, solid state hard drives and POS headtotail, makes the utility model discloses overall structure is compact, easy dismouting, the extension that is used for flight platform carry that sets up on the connection structure can satisfy different flight platform's carry demand, maintains, test cost is low. The high-precision POS system is adopted, the updating frequency of combined positioning data reaches 100Hz, the plane position precision reaches 1cm, the elevation precision reaches 2cm, the pitch angle and roll angle precision reaches 0.005 degrees, the course angle precision reaches 0.01 degrees, time synchronization is carried out through the high-precision POS system and the high-quality high-precision data achievement is collected under the condition that a flight platform is unstable.
Although the embodiments of the present invention have been described in detail, the embodiments of the present invention are not limited thereto, and those skilled in the art can modify the principles of the embodiments of the present invention, and therefore, various modifications performed according to the principles of the embodiments of the present invention should be understood as falling into the scope of the embodiments of the present invention.
Claims (10)
1. A connection structure for a flying platform, comprising:
a first mounting plate for mounting a POS system thereon;
the second mounting plate is used for mounting the industrial personal computer;
a third mounting plate for mounting a hyperspectral camera thereon;
wherein, the first mounting panel, the second mounting panel, the third mounting panel are two-by-two perpendicular.
2. The connecting structure according to claim 1, wherein the first mounting plate, the second mounting plate and the third mounting plate are detachably connected or non-detachably connected two by two.
3. A connection arrangement according to claim 1 or 2, wherein the first mounting plate is provided with an extension for detachable mounting on a flying platform, the POS system being mounted on an end face perpendicular to the extension.
4. The connecting structure according to claim 3, wherein the second mounting plate is perpendicularly connected to the other end surface of the first mounting plate, and an industrial personal computer is mounted on the end surface thereof perpendicular to the end surface of the first mounting plate on which the POS system is mounted.
5. The connecting structure of claim 4, wherein the third mounting plate is vertically connected with one side surface of the second mounting plate, and a hyperspectral camera is mounted on the end surface of the third mounting plate, which is perpendicular to the end surface of the second mounting plate for mounting an industrial personal computer; or the third mounting plate is vertically connected with the other end face of the first mounting plate, and the hyperspectral cameras are arranged on the end faces, which are perpendicular to the end face of the first mounting plate for mounting the POS system and the end face of the second mounting plate for mounting the industrial personal computer in pairs.
6. An airborne hyperspectral imaging apparatus for a flying platform, comprising:
a connection according to any one of claims 1 to 5 for detachable mounting on a flying platform;
the POS system, the industrial personal computer and the hyperspectral camera are detachably arranged on the three end faces of the connecting structure;
the solid state disk is externally arranged on the industrial personal computer;
the industrial personal computer is connected with the hyperspectral camera, the solid state disk and the POS system respectively, and data collected by the hyperspectral camera is transmitted to the industrial personal computer and stored in the solid state disk.
7. The airborne hyperspectral imaging device according to claim 6, wherein one side of the industrial personal computer, which faces away from the surface, is provided with two protruding extensions for forming a bayonet for accommodating a solid state disk.
8. The airborne hyperspectral imaging device according to claim 6, wherein a hard disk protection shell used for protecting and placing the solid state disk is sleeved at the rear end of the solid state disk.
9. The onboard hyperspectral imaging apparatus according to claim 6, wherein the POS system is provided with one or more of ETH, IO, PWR, GNSS _1, GNSS _2, 4G interfaces and a SIMCARD slot.
10. The airborne hyperspectral imaging apparatus according to claim 6, wherein the flying platform is a manned machine or an unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121399122.4U CN215155742U (en) | 2021-06-23 | 2021-06-23 | Airborne hyperspectral imaging device for flight platform and connecting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121399122.4U CN215155742U (en) | 2021-06-23 | 2021-06-23 | Airborne hyperspectral imaging device for flight platform and connecting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215155742U true CN215155742U (en) | 2021-12-14 |
Family
ID=79385441
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121399122.4U Active CN215155742U (en) | 2021-06-23 | 2021-06-23 | Airborne hyperspectral imaging device for flight platform and connecting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215155742U (en) |
-
2021
- 2021-06-23 CN CN202121399122.4U patent/CN215155742U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN113911326A (en) | Unmanned aerial vehicle | |
| US7099152B2 (en) | Computer system with configurable docking station | |
| CN107804474B (en) | Design method of complete machine system of multi-rotor flying robot with redundant mechanical arm | |
| CN204383757U (en) | Unmanned vehicle and circuit board assemblies thereof | |
| CN202929406U (en) | Portable earth station | |
| WO2009138948A1 (en) | Data acquisition module and system | |
| CN108357673A (en) | A kind of unmanned plane including modular extendable load cabin and function module | |
| CN215155742U (en) | Airborne hyperspectral imaging device for flight platform and connecting structure | |
| CN207319073U (en) | Unmanned plane and unmanned flight's system | |
| Singh et al. | Industrial System Engineering for Drones | |
| CN212354387U (en) | Many rotor unmanned aerial vehicle dynamic identification system | |
| CN117782227A (en) | Multisource aerial remote sensing data acquisition device, system and control method | |
| CN208699053U (en) | A kind of unmanned plane including modular extendable load cabin and functional module | |
| CN204587320U (en) | A kind of remotely sensed image is taken photo by plane system | |
| CN205203414U (en) | Low latitude image acquisition device | |
| CN207907901U (en) | A kind of unmanned plane polyphaser position and orientation measurement recorder | |
| CN102853221A (en) | Quickly-assembled/disassembled inner-frame mechanism of airborne photoelectric platform | |
| US6907332B1 (en) | Method and apparatus to align auxiliary aircraft equipment attitude and heading | |
| RU2702845C1 (en) | Navigation system and housing of navigation system | |
| KR101623410B1 (en) | Board stack module for multicopter and multicopter using the module | |
| CN214427616U (en) | GNSS receiver | |
| WO2018214014A1 (en) | Method and device for measuring mounting error of accelerometer, and unmanned aerial vehicle | |
| CN109900299B (en) | Radio altimeter large-angle test system, unmanned aerial vehicle and implementation method | |
| CN211956225U (en) | Flight control equipment, system and unmanned aerial vehicle | |
| CN210221080U (en) | Unmanned aerial vehicle measuring equipment and system integrated with depth camera |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |