CN210804104U

CN210804104U - Unmanned aerial vehicle flight control technology testing device

Info

Publication number: CN210804104U
Application number: CN201922191532.9U
Authority: CN
Inventors: 邵宇; 崔海龙; 梁耀; 谢俊杰; 严扬扬; 唐柯铖; 孙世成; 李嘉涛
Original assignee: NINGBO YINZHOU VOCATIONAL EDUCATION CENTER SCHOOL
Current assignee: NINGBO YINZHOU VOCATIONAL EDUCATION CENTER SCHOOL
Priority date: 2019-12-09
Filing date: 2019-12-09
Publication date: 2020-06-19
Anticipated expiration: 2029-12-09

Abstract

The utility model discloses an unmanned aerial vehicle flight control technology testing device, which comprises a host, a shutdown platform for supporting an unmanned aerial vehicle and a plurality of detection frames which are sequentially placed, wherein the bottom of each detection frame is fixed with a bracket; the host comprises a main controller, a power supply module, a display module and a main wireless communication module, wherein the main controller is electrically connected with the power supply module, and the display module and the main wireless communication module are electrically connected with the main controller; a pressure sensor for supporting the unmanned aerial vehicle is installed on the shutdown platform and is electrically connected with the main controller; each detection frame is internally provided with a detection device for detecting the unmanned aerial vehicle when the unmanned aerial vehicle passes through the detection frame; each detection frame is in communication connection with the host; the utility model discloses unmanned aerial vehicle's flight control technique can be tested, unmanned aerial vehicle user's the ability of controlling helps improving.

Description

Unmanned aerial vehicle flight control technology testing device

Technical Field

The utility model relates to a testing arrangement technical field, concretely relates to unmanned aerial vehicle flies accuse technical test device.

Background

At present, unmanned aerial vehicle's application is more and more extensive, for example, utilizes unmanned aerial vehicle to take photo by plane, and unmanned aerial vehicle's flight control technique is the key that unmanned aerial vehicle flies, but to unmanned aerial vehicle beginner, does not have the device that can test unmanned aerial vehicle flight technique yet at present, the utility model aims at providing a device for testing unmanned aerial vehicle flight control technique.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art, the utility model provides an unmanned aerial vehicle flies to control technique testing arrangement, its flight control technique that can test unmanned aerial vehicle helps improving unmanned aerial vehicle user's the ability of controlling.

The utility model discloses an unmanned aerial vehicle flight control technology testing device, which comprises a host, a shutdown platform for supporting the unmanned aerial vehicle and a plurality of detection frames which are placed in sequence, wherein the bottom of each detection frame is fixed with a bracket; the host comprises a main controller, a power supply module, a display module and a main wireless communication module, wherein the main controller is electrically connected with the power supply module, and the display module and the main wireless communication module are electrically connected with the main controller; a pressure sensor for supporting the unmanned aerial vehicle is installed on the shutdown platform and is electrically connected with the main controller; each detection frame is internally provided with a detection device for detecting the unmanned aerial vehicle when the unmanned aerial vehicle passes through the detection frame; each detection frame is in communication connection with the host.

The utility model discloses an unmanned aerial vehicle flies to control technical test device, wherein, detection device includes first sensor unit and the second sensor unit of installing in detecting the frame, and first sensor unit and second sensor unit distribute along the width direction that detects the frame; the first sensor unit comprises a plurality of first infrared transmitting sensors and a plurality of first infrared receiving sensors, the plurality of first infrared transmitting sensors are fixed at the inner top of the detection frame and distributed along the length direction of the detection frame, the plurality of first infrared receiving sensors are fixed at the inner bottom of the detection frame and distributed along the length direction of the detection frame, and each first infrared receiving sensor is respectively arranged corresponding to one first infrared transmitting sensor in the vertical direction; the second sensor unit comprises a plurality of second infrared transmitting sensors and a plurality of second infrared receiving sensors, the plurality of second infrared transmitting sensors are fixed at the inner top of the detection frame and distributed along the length direction of the detection frame, the plurality of second infrared receiving sensors are fixed at the inner bottom of the detection frame and distributed along the length direction of the detection frame, and each second infrared receiving sensor is respectively arranged corresponding to one of the second infrared transmitting sensors in the vertical direction; the slave controller, the slave wireless communication module and the storage battery are installed in the support at the bottom of each detection frame, the first sensor unit and the second sensor unit in each detection frame are electrically connected with the slave controller in the corresponding support at the bottom of the detection frame, the slave controller is electrically connected with the storage battery, the slave wireless communication module is electrically connected with the slave controller, and the slave wireless communication module is in communication connection with the master wireless communication module.

The utility model discloses an unmanned aerial vehicle flies to control technical test device, wherein, the interval of two adjacent first infrared emission sensors is less than unmanned aerial vehicle's width, and the interval of two adjacent second infrared emission sensors is less than unmanned aerial vehicle's width; after through adopting this kind of structure, when unmanned aerial vehicle passes through the detection frame, can avoid first infrared emission sensor and first infrared receiving sensor can not detect unmanned aerial vehicle, and in the same way, when unmanned aerial vehicle passes through the detection frame, also can avoid second infrared emission sensor and second infrared receiving sensor to detect unmanned aerial vehicle.

The utility model discloses unmanned aerial vehicle's flight control technique can be tested, unmanned aerial vehicle user's the ability of controlling helps improving.

Drawings

The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:

fig. 1 is a schematic top view of the present invention;

FIG. 2 is a schematic structural diagram of a detection frame;

FIG. 3 is a schematic view of a partial cross-sectional structure of a detection frame;

fig. 4 is a schematic block diagram of the circuit of the present invention.

Detailed Description

In the following description, numerous implementation details are set forth in order to provide a more thorough understanding of the present invention. It should be understood, however, that these implementation details should not be used to limit the invention. That is, in some embodiments of the invention, details of these implementations are not necessary. In addition, some conventional structures and components are shown in simplified schematic form in the drawings.

In addition, the descriptions related to "first", "second", etc. in the present invention are only for description purposes, not specifically referring to the order or sequence, and are not intended to limit the present invention, but only to distinguish the components or operations described in the same technical terms, and are not to be construed as indicating or implying any relative importance or implicit indication of the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should not be considered to exist, and is not within the protection scope of the present invention.

The utility model discloses an unmanned aerial vehicle flies to control technical test device, including host computer 1, the shutdown platform 3 that is used for supporting unmanned aerial vehicle 2 and a plurality of detection frame 4 placed according to the preface, the bottom of every detection frame 4 all is fixed with support 46; the host 1 comprises a main controller 11, a power module 12, a display module 13 and a main wireless communication module 14, wherein the main controller 11 is electrically connected with the power module 12, and both the display module 13 and the main wireless communication module 14 are electrically connected with the main controller 11; a pressure sensor 31 for supporting the unmanned aerial vehicle 2 is mounted on the shutdown platform 3, and the pressure sensor 31 is electrically connected with the main controller 11; each detection frame 4 is provided with a detection device for detecting the unmanned aerial vehicle 2 when the unmanned aerial vehicle 2 passes through the detection frame 4; each detection frame 4 is in communication connection with the host 1.

The detection device includes a first sensor unit 41 and a second sensor unit 42 installed in the detection frame 4, the first sensor unit 41 and the second sensor unit 42 being distributed in the width direction of the detection frame 4; the first sensor unit 41 includes a plurality of first infrared emission sensors 411 and a plurality of first infrared receiving sensors 412, the plurality of first infrared emission sensors 411 are fixed on the inner top of the detection frame 4 and distributed along the length direction of the detection frame 4, the plurality of first infrared receiving sensors 412 are fixed on the inner bottom of the detection frame 4 and distributed along the length direction of the detection frame 4, and each first infrared receiving sensor 412 is respectively arranged corresponding to one of the first infrared emission sensors 411 in the vertical direction; the second sensor unit 42 includes a plurality of second infrared emission sensors 421 and a plurality of second infrared receiving sensors 422, the plurality of second infrared emission sensors 421 are fixed on the inner top of the detection frame 4 and distributed along the length direction of the detection frame 4, the plurality of second infrared receiving sensors 422 are fixed on the inner bottom of the detection frame 4 and distributed along the length direction of the detection frame 4, and each second infrared receiving sensor 422 is respectively arranged corresponding to one of the second infrared emission sensors 421 in the vertical direction; the bracket 46 at the bottom of each detection frame 4 is provided with a slave controller 43, a slave wireless communication module 44 and a storage battery 45, the first sensor unit 41 and the second sensor unit 42 in each detection frame 4 are electrically connected with the slave controller 43 in the corresponding bracket 46 at the bottom of the detection frame 4, the slave controller 43 is electrically connected with the storage battery 45, the slave wireless communication module 44 is electrically connected with the slave controller 43, and the slave wireless communication module 44 is in communication connection with the master wireless communication module 14.

The distance between two adjacent first infrared emission sensors 411 is smaller than the width of the unmanned aerial vehicle 2, and the distance between two adjacent second infrared emission sensors 421 is smaller than the width of the unmanned aerial vehicle 2; after through adopting this kind of structure, when unmanned aerial vehicle passes through the detection frame, can avoid first infrared emission sensor and first infrared receiving sensor can not detect unmanned aerial vehicle, and in the same way, when unmanned aerial vehicle passes through the detection frame, also can avoid second infrared emission sensor and second infrared receiving sensor to detect unmanned aerial vehicle.

In use the utility model discloses in the time, at first all establish communication connection with the host computer with every detection frame (namely make every detect the main communication module of following in wireless communication module and the host computer in the frame and establish communication connection), then unmanned aerial vehicle operating personnel controls unmanned aerial vehicle, when unmanned aerial vehicle takes off, pressure sensor can not detect unmanned aerial vehicle's weight, main control unit in the host computer begins timing, then unmanned aerial vehicle controls personnel and makes unmanned aerial vehicle pass each detection frame according to the sequence number that detects the frame in proper order, until after unmanned aerial vehicle passes last detection frame, main control unit in the host computer stops timing, and show unmanned aerial vehicle flight time on display module. In the flight process of the unmanned aerial vehicle, if the sequence of the unmanned aerial vehicle passing through each detection frame is wrong, the flight test of the unmanned aerial vehicle fails, and a display module in the host displays failure information; when the direction of the unmanned aerial vehicle passing through each detection frame is wrong, the flight test of the unmanned aerial vehicle is failed, and a display module in the host machine can display failure information; judging the sequence of the unmanned aerial vehicle passing through each detection frame according to the sequence of triggering the detection device in each detection frame; judging the direction of the unmanned aerial vehicle passing through each detection frame according to the triggering sequence of the first sensor unit and the second sensor unit in each detection frame; in addition, the host computer can consider the unmanned aerial vehicle as successfully flying only if the sequence and the direction of the unmanned aerial vehicle passing through each detection frame are ensured to be correct; it should be noted that, when the first sensor unit and the second sensor unit in each detection frame are triggered by the unmanned aerial vehicle, the detection frame can send the trigger information to the host computer in real time.

The above description is only an embodiment of the present invention, and is not intended to limit the present invention. Various modifications and changes may occur to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle flies accuse technical test device which characterized in that: the unmanned aerial vehicle detection system comprises a host (1), a shutdown platform (3) for supporting an unmanned aerial vehicle (2) and a plurality of detection frames (4) which are sequentially placed, wherein a support (46) is fixed at the bottom of each detection frame (4); the host (1) comprises a main controller (11), a power supply module (12), a display module (13) and a main wireless communication module (14), wherein the main controller (11) is electrically connected with the power supply module (12), and the display module (13) and the main wireless communication module (14) are both electrically connected with the main controller (11); a pressure sensor (31) for supporting the unmanned aerial vehicle (2) is mounted on the shutdown platform (3), and the pressure sensor (31) is electrically connected with the main controller (11); each detection frame (4) is internally provided with a detection device for detecting the unmanned aerial vehicle (2) when the unmanned aerial vehicle (2) passes through the detection frame (4); each detection frame (4) is in communication connection with the host (1).

2. The unmanned aerial vehicle flight control technology test device of claim 1, wherein the detection device comprises a first sensor unit (41) and a second sensor unit (42) installed in the detection frame (4), and the first sensor unit (41) and the second sensor unit (42) are distributed along the width direction of the detection frame (4); the first sensor unit (41) comprises a plurality of first infrared emission sensors (411) and a plurality of first infrared receiving sensors (412), the plurality of first infrared emission sensors (411) are fixed at the inner top of the detection frame (4) and distributed along the length direction of the detection frame (4), the plurality of first infrared receiving sensors (412) are fixed at the inner bottom of the detection frame (4) and distributed along the length direction of the detection frame (4), and each first infrared receiving sensor (412) is arranged corresponding to one first infrared emission sensor (411) in the vertical direction; the second sensor unit (42) comprises a plurality of second infrared emission sensors (421) and a plurality of second infrared receiving sensors (422), the plurality of second infrared emission sensors (421) are fixed at the inner top of the detection frame (4) and distributed along the length direction of the detection frame (4), the plurality of second infrared receiving sensors (422) are fixed at the inner bottom of the detection frame (4) and distributed along the length direction of the detection frame (4), and each second infrared receiving sensor (422) is respectively arranged corresponding to one of the second infrared emission sensors (421) in the vertical direction; the slave controller (43), the slave wireless communication module (44) and the storage battery (45) are installed in the support (46) at the bottom of each detection frame (4), the first sensor unit (41) and the second sensor unit (42) in each detection frame (4) are electrically connected with the slave controller (43) in the support (46) at the bottom of the corresponding detection frame (4), the slave controller (43) is electrically connected with the storage battery (45), the slave wireless communication module (44) is electrically connected with the slave controller (43), and the slave wireless communication module (44) is in communication connection with the master wireless communication module (14).

3. The unmanned aerial vehicle flight control technology test device of claim 2, wherein the distance between two adjacent first infrared emission sensors (411) is smaller than the width of the unmanned aerial vehicle (2), and the distance between two adjacent second infrared emission sensors (421) is smaller than the width of the unmanned aerial vehicle (2).