CN212060557U - Remote calibration device of remote sensing satellite receiving system based on unmanned aerial vehicle - Google Patents
Remote calibration device of remote sensing satellite receiving system based on unmanned aerial vehicle Download PDFInfo
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- CN212060557U CN212060557U CN202020472449.9U CN202020472449U CN212060557U CN 212060557 U CN212060557 U CN 212060557U CN 202020472449 U CN202020472449 U CN 202020472449U CN 212060557 U CN212060557 U CN 212060557U
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Abstract
The utility model relates to an unmanned aerial vehicle signal reception field specifically discloses a remote calibration device based on unmanned aerial vehicle's remote sensing satellite receiving system, including the unmanned aerial vehicle controller, one side of back bracket is installed and is presented the source, present and install the pull rod between source and the back bracket, install the rotation support between back bracket and the installation stand, the regulation lifter is installed to one side of rotation support, one side of host system has the IMU module to be located the internally mounted of unmanned aerial vehicle controller. Master module can coordinate each module function, and the IMU module can respond to, control the various gesture of unmanned aerial vehicle, can audio-visually judge unmanned aerial vehicle's flight mode through the LED lamp, conveniently supplies the purpose that ground operating personnel confirmed the aircraft night, and the flexible of lifter on the installation stand is adjusted in the control to can control the inclination of back bracket, can conveniently receive the signal of telecommunication of different angle transmissions.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle signal reception field specifically is a remote calibration device based on unmanned aerial vehicle's remote sensing satellite receiving system.
Background
With the deepening of understanding of earth resources and environment and the improvement of earth observation technology, the information transmission rate required by a satellite-earth link of a remote sensing satellite is higher and higher, the calibration test of a data receiving system of the remote sensing satellite is an essential technical link in the process of system development and test, and the remote calibration of the data receiving system of the remote sensing satellite is to remotely monitor the running state of radar calibration equipment and realize the functions of real-time data acquisition, data transmission, analysis processing, configuration setting, data storage management and the like while monitoring.
However, the unmanned aerial vehicle on the market is far away from the ground control device in use, so that the situation that signal transmission is unstable is easily caused when the unmanned aerial vehicle is used for easily causing signal transmission. Therefore, the technical personnel in the field provide a remote calibration device of a remote sensing satellite receiving system based on an unmanned aerial vehicle, so as to solve the problems in the background technology.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a remote sensing satellite receiving system's long-range school device of marking based on unmanned aerial vehicle to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides a remote calibration device that marks based on remote sensing satellite receiving system of unmanned aerial vehicle, includes the unmanned aerial vehicle controller, the last surface mounting of unmanned aerial vehicle controller has the installation stand, the top of installation stand is provided with back bracket, one side of back bracket is installed and is presented the source, present and install the pull rod between source and the back bracket, install the rotation support between back bracket and the installation stand, rotate one side of support and install the regulation lifter, the internally mounted of unmanned aerial vehicle controller has host system, the internally mounted that one side of host system is located the unmanned aerial vehicle controller has the IMU module, the inside that one side of IMU module is located the unmanned aerial vehicle controller is provided with the GPS module, signal transceiver module is installed to host system's opposite side, drive connecting rod is installed in the outside of unmanned aerial vehicle controller.
As a further aspect of the present invention: an annular LED lamp is installed between the main control module and the driving connecting rod, and a helical blade is installed at one end of the driving connecting rod.
As a further aspect of the present invention: the lower surface mounting of unmanned aerial vehicle controller has the camera, the outside of camera is located the lower surface mounting that unmanned aerial vehicle controller is right and has buffering callus on the sole.
As a further aspect of the present invention: buffering callus on the sole is beautiful aluminium material component, camera and unmanned aerial vehicle controller electric connection.
As a further aspect of the present invention: the annular LED lamp is electrically connected with the main control module, and the spiral blade is rotationally connected with the driving connecting rod.
As a further aspect of the present invention: the pull rod is connected with the feed source head and the back bracket in a rotating mode, the back bracket is connected with the mounting upright post in a rotating mode through the rotating support, and the adjusting lifting rod is connected with the mounting upright post in a rotating mode.
As a further aspect of the present invention: the main control module is electrically connected with the annular LED lamp, and the IMU module, the signal transceiving module and the GPS module are electrically connected with the main control module.
Compared with the prior art, the beneficial effects of the utility model are that: the designed main control module can simultaneously play a role in controlling a CPU of the unmanned aerial vehicle, and can coordinate functions of various modules, the IMU module can sense and control various postures of the unmanned aerial vehicle, the GPS module realizes positioning and return voyage of the unmanned aerial vehicle, and the annular LED lamp can visually judge the flight mode of the unmanned aerial vehicle through the color and the flicker frequency of the lamp, so that ground operators can conveniently determine the aircraft at night; and the structure of signal reception feed reply the shielding of principal plane radiation as little as possible, through adjusting the flexible of lifter on the installation stand through control in the aircraft working process, thereby can control the inclination of back bracket, can conveniently receive the signal of telecommunication of different angle transmissions, and adjust and rotate through the pull rod between lifter and the back bracket, thereby the detection range of feed head has been increased, the convenient acceptance range to the signal, unmanned aerial vehicle's signal transmission's stability and accuracy nature have been guaranteed.
Drawings
FIG. 1 is a schematic structural diagram of a remote calibration device of a remote sensing satellite receiving system based on an unmanned aerial vehicle;
FIG. 2 is a schematic diagram of an internal structure of a remote calibration device of a remote sensing satellite receiving system based on an unmanned aerial vehicle, wherein the remote sensing satellite receiving system is provided with an unmanned aerial vehicle controller;
fig. 3 is a schematic structural diagram of a signal transceiver in a remote calibration device of a remote sensing satellite receiving system based on an unmanned aerial vehicle.
In the figure: 1. an unmanned aerial vehicle controller; 2. a helical blade; 3. a buffer foot pad; 4. a drive link; 5. an annular LED lamp; 6. mounting the upright post; 7. a camera; 101. an IMU module; 102. a GPS module; 103. a main control module; 104. a signal transceiving module; 601. a pull rod; 602. a feed source; 603. a back bracket; 604. adjusting the lifting rod; 605. the bracket is rotated.
Detailed Description
Referring to fig. 1-3, in the embodiment of the present invention, a remote calibration device for a remote sensing satellite receiving system based on an unmanned aerial vehicle comprises an unmanned aerial vehicle controller 1, an installation upright 6 is installed on the upper surface of the unmanned aerial vehicle controller 1, a back bracket 603 is arranged above the installation upright 6, a feed source head 602 is installed on one side of the back bracket 603, a pull rod 601 is installed between the feed source head 602 and the back bracket 603, a rotating bracket 605 is installed between the back bracket 603 and the installation upright 6, an adjusting lifting rod 604 is installed on one side of the rotating bracket 605, a main control module 103 is installed inside the unmanned aerial vehicle controller 1, an IMU module 101 is installed inside the unmanned aerial vehicle controller 1 on one side of the main control module 103 (model: E62-DTU), a GPS module 102 (model: a20-0110) is installed inside the unmanned aerial vehicle controller 1 on one side of the IMU module 101 (model: SC-INS-100S), the other side of the main control module 103 is provided with a signal transceiving module 104, and the outer side of the unmanned aerial vehicle controller 1 is provided with a driving connecting rod 4.
In fig. 1, 2, 3: install annular LED lamp 5 between host system 103 and the drive connecting rod 4, helical blade 2 is installed to the one end of drive connecting rod 4, the lower surface mounting of unmanned aerial vehicle controller 1 has camera 7, the outside of camera 7 is located the lower surface mounting of unmanned aerial vehicle controller 1 right and has buffering callus on the sole 3, buffering callus on the sole 3 is beautiful aluminium material component, camera 7 and unmanned aerial vehicle controller 1 electric connection, annular LED lamp 5 and host system 103 electric connection, helical blade 2 rotates with drive connecting rod 4 to be connected, pull rod 601 and feed head 602, back bracket 603 rotates to be connected, back bracket 603 rotates through rotating bracket 605 with installation stand 6 to be connected, adjust lifter 604 and installation stand 6 and rotate to be connected, host system 103 and annular LED lamp 5 electric connection, IMU module 101, signal transceiver module 104 and GPS module 102 all with host system 103 electric connection.
In fig. 1: at the buffering callus on the sole 3 that 1 lower surface of unmanned aerial vehicle controller set up, helical blade 2 can be used for providing the take-off power of aircraft, can play the bradyseism effect at aircraft lift in-process, and camera 7 can be used for the shooting effect of aircraft in flight.
The utility model discloses a theory of operation is: the rotation of the helical blade 2 is controlled by the unmanned aerial vehicle controller 1 to provide a power source for the unmanned aerial vehicle, in the flying process of the aircraft, the camera 7 controls the signal transceiver module 104 to transmit a video signal to a control device of a ground operator by shooting an image and then controls the signal transceiver module 103 to transmit the video signal, the ground operator needs to control the aircraft to transmit the signal, the signal is received by the feed source head 602 and then fed back to the signal transceiver module 104, the signal transceiver module 104 transmits the signal to the main control module 103, the main control module 103 issues different instructions according to the type of the signal, when the traveling or suspension of the aircraft needs to be controlled, the instruction is issued to the IMU module 101, so that the motion state of the aircraft is controlled, and when the position of the aircraft needs to be tracked and positioned, the GPS module 102 is used for transmitting the real-time status of the aircraft through telecommunication, the processing transmission of source 602 is presented to the control system on ground through presenting, when the aircraft is in the environment of flying at night under, utilize the annular LED lamp 5 that is located the drive connecting rod 4 outside can conveniently fix a position the aircraft, adjust the flexible of lifter 604 on installation post 6 through control in the aircraft working process, thereby can control the inclination of back bracket 603, can conveniently present the signal of telecommunication of source 602 receipt different angle transmissions, and adjust and rotate through pull rod 601 between lifter 604 and the back bracket 603, thereby the detection scope of source head 602 has been increased, the convenience is to the acceptance range of signal.
The above-mentioned, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (7)
1. The remote calibration device of the remote sensing satellite receiving system based on the unmanned aerial vehicle comprises an unmanned aerial vehicle controller (1) and is characterized in that an installation upright post (6) is installed on the upper surface of the unmanned aerial vehicle controller (1), a back bracket (603) is arranged above the installation upright post (6), a feed source head (602) is installed on one side of the back bracket (603), a pull rod (601) is installed between the feed source head (602) and the back bracket (603), a rotating support (605) is installed between the back bracket (603) and the installation upright post (6), an adjusting lifting rod (604) is installed on one side of the rotating support (605), a main control module (103) is installed inside the unmanned aerial vehicle controller (1), an IMU module (101) is installed inside the main control module (103) and is located inside the unmanned aerial vehicle controller (1), the inside that one side of IMU module (101) is located unmanned aerial vehicle controller (1) is provided with GPS module (102), signal transceiver module (104) are installed to the opposite side of host system (103), drive connecting rod (4) are installed in the outside of unmanned aerial vehicle controller (1).
2. The remote calibration device of the unmanned aerial vehicle-based remote sensing satellite receiving system according to claim 1, wherein an annular LED lamp (5) is installed between the main control module (103) and the driving connecting rod (4), and one end of the driving connecting rod (4) is provided with a helical blade (2).
3. The remote calibration device of the unmanned aerial vehicle-based remote sensing satellite receiving system according to claim 1, wherein a camera (7) is mounted on the lower surface of the unmanned aerial vehicle controller (1), and a buffering foot pad (3) is mounted on the lower surface of the unmanned aerial vehicle controller (1) pair on the outer side of the camera (7).
4. The remote calibration device of the unmanned aerial vehicle-based remote sensing satellite receiving system according to claim 3, wherein the buffering foot pad (3) is a component made of aluminum, and the camera (7) is electrically connected with the unmanned aerial vehicle controller (1).
5. The remote calibration device of the unmanned aerial vehicle-based remote sensing satellite receiving system according to claim 2, wherein the annular LED lamp (5) is electrically connected with the main control module (103), and the helical blade (2) is rotatably connected with the driving connecting rod (4).
6. The remote calibration device of the unmanned aerial vehicle-based remote sensing satellite receiving system is characterized in that the pull rod (601) is rotatably connected with the feed head (602) and the back bracket (603), the back bracket (603) is rotatably connected with the mounting upright post (6) through a rotating support (605), and the adjusting lifting rod (604) is rotatably connected with the mounting upright post (6).
7. The remote calibration device of the unmanned aerial vehicle-based remote sensing satellite receiving system according to claim 2, wherein the main control module (103) is electrically connected with the annular LED lamp (5), and the IMU module (101), the signal transceiver module (104) and the GPS module (102) are electrically connected with the main control module (103).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020472449.9U CN212060557U (en) | 2020-04-03 | 2020-04-03 | Remote calibration device of remote sensing satellite receiving system based on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020472449.9U CN212060557U (en) | 2020-04-03 | 2020-04-03 | Remote calibration device of remote sensing satellite receiving system based on unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN212060557U true CN212060557U (en) | 2020-12-01 |
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| CN202020472449.9U Active CN212060557U (en) | 2020-04-03 | 2020-04-03 | Remote calibration device of remote sensing satellite receiving system based on unmanned aerial vehicle |
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| CN (1) | CN212060557U (en) |
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