CN204473130U - A kind of aircraft detecting peripheral wireless network environment - Google Patents
A kind of aircraft detecting peripheral wireless network environment Download PDFInfo
- Publication number
- CN204473130U CN204473130U CN201520166484.7U CN201520166484U CN204473130U CN 204473130 U CN204473130 U CN 204473130U CN 201520166484 U CN201520166484 U CN 201520166484U CN 204473130 U CN204473130 U CN 204473130U
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- wireless network
- network environment
- module
- communication module
- wireless communication
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Abstract
The utility model discloses a kind of aircraft detecting peripheral wireless network environment.Comprise quadrotor main body, micro controller system main control module, wireless network environment detection module, wireless communication module and far-end computer and printing device; Described quadrotor is as carrier, carry micro controller system main control module and wireless network environment detection module and wireless communication module and carry out work, and the data that will detect, as network speed, network stabilization degree etc., be transferred to described far-end computer by wireless communication module and process data into chart, and by described printing device, chart is printed.Substantial effect of the present utility model is: be applicable to most scene, applied widely and cost is not high.By wireless network measurement and quadrotor technology, carry out work in full automatic mode, time saving and energy saving and effect is more accurate reliable, and the result drawn has more reference value.
Description
Technical field
The utility model relate to a kind of can the quadrotor of controlled in wireless, particularly relate to a kind of quadrotor detecting peripheral wireless network environment.
Background technology
Current people are to the raising of network demand, and the coverage of wireless network is also very big.But the network environment of different location, as network speed, degree of stability etc. are all had any different, and the frequency range that different telecom operators use is also different.
Current main-stream network tolling is used as foundation mainly through flow and maximum broadband, and this is not a very fair scheme.
Present urgent need product, be used for allowing client understand environment residing for oneself and use the network of that operator better, telecom operators also can be allowed to understand should improve once again in which region.This can improve our network environment greatly.
Utility model content
For the problems referred to above, the purpose of this utility model is to provide a kind of aircraft detecting peripheral wireless network environment.
For achieving the above object, the technical scheme taked of the utility model is as follows:
Detect an aircraft for peripheral wireless network environment, comprise quadrotor fuselage, micro controller system master control
Module 17, wireless network environment detection module 16, wireless communication module 15; Described quadrotor fuselage comprises fuselage carrier 12, frame 14, motor 11; Micro controller system main control module 17, wireless network environment detection module 16, wireless communication module 15, frame 14 are all arranged on fuselage carrier 12, and motor 11 is arranged in frame; Micro controller system main control module 17 is connected with wireless network environment detection module 16, wireless communication module 15, motor 11 respectively.
Described wireless communication module 15 comprises NRF communication module, GPS module, remote control receiver module; Data are imported in micro controller system main control module 17 each via different I/O ports by these three equal independent work of module.
Described wireless communication module 15 is connected with the far-end computer being connected with printing device.User can be direct
Use far-end computer to arrange the flight range of aircraft or route, the network data measured by aircraft also can be transferred in far-end computer by wireless communication module and process.
Also include LED light 13, lithium cell 18, LED light 13 connects with micro controller system main control module 17
Connect, lithium cell 18 is connected with motor 11.
Described fuselage carrier 12 is provided with charge port 19, and described charge port 19 is connected with lithium cell 18.
Described LED light 13 is positioned at the below of fuselage carrier 12.
When using the utility model, only need by aircraft electric power starting when needs use, after far-end computer and aircraft wireless connections.
The utility model structure is simple, elegant in appearance, easy to use, applied widely, can freely control, by force handling.And there is very high social value.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is lateral plan of the present utility model.
Fig. 3 is birds-eye view of the present utility model.
In figure: 11-motor, 12-fuselage carrier, 13-LED indicator lamp, 14-frame, 15-wireless communication module, 16-wireless network environment detection module, 17-micro controller system main control module, 18-lithium cell, 19-charge port.
Detailed description of the invention
Below in conjunction with embodiment shown in the drawings, the utility model is described in further detail.
As shown in drawings, the utility model comprises quadrotor fuselage, micro controller system main control module 17, wireless network environment detection module 16, wireless communication module 15 and far-end computer and printing device.
Described quadrotor fuselage comprises frame 14, motor 11, lithium cell 18, fuselage carrier 12 and LED light 13 and source switch further.
Described wireless communication module comprises NRF communication module and GPS module and remote control receiver module further.
As shown in the figure, described micro controller system main control module and wireless network environment detection module and wireless communication module are installed on quadrotor fuselage, and micro controller system main control module is also connected with wireless network environment detection module and wireless communication module and controls except controlling the flight of aircraft.
Micro controller system main control module 17, wireless network environment detection module 16, wireless communication module 15, frame 14 are all arranged on fuselage carrier 12, and motor 11 is arranged in frame; Micro controller system main control module 17 is connected with wireless network environment detection module 16, wireless communication module 15, motor 11 respectively.
Wireless communication module 15 is connected with the far-end computer being connected with printing device.
The utility model also includes LED light 13, lithium cell 18, LED light 13 and monolithic owner
Control module 17 connects, and lithium cell 18 is connected with motor 11.
Described fuselage carrier 12 is provided with charge port 19, and described charge port 19 is connected with lithium cell 18.
Described LED light 13 is positioned at the below of fuselage carrier 12.
When using the utility model, just can be connected with far-end computer after opening switch.User only need at far-end computer enterprising walking along the street line setting rear aircraft meeting automatic operation.Can automatically make a return voyage after band aircraft detects, network environment data figure also can be printed by printing device by far-end computer automatically.Meanwhile, if there are abnormal condition in aircraft working process, carry-on LED light can send red alarm signal, also warning information can be sent in far-end computer simultaneously and notify user.
Ought to it is noted that need the part of software programming all to solidify in hardware programmable device in the utility model, user can directly use.
Claims (6)
1. detect an aircraft for peripheral wireless network environment, it is characterized in that: comprise quadrotor fuselage, micro controller system main control module (17), wireless network environment detection module (16), wireless communication module (15); Described quadrotor fuselage comprises fuselage carrier (12), frame (14), motor (11); Micro controller system main control module (17), wireless network environment detection module (16), wireless communication module (15), frame (14) are all arranged on fuselage carrier (12), and motor (11) is arranged in frame; Micro controller system main control module (17) is connected with wireless network environment detection module (16), wireless communication module (15), motor (11) respectively.
2. a kind of aircraft detecting peripheral wireless network environment according to claim 1, is characterized in that: described wireless communication module (15) comprises NRF communication module, GPS module, remote control receiver module; Data are imported in micro controller system main control module (17) each via different I/O ports by these three equal independent work of module.
3. a kind of aircraft detecting peripheral wireless network environment according to claim 1 and 2, is characterized in that: described wireless communication module (15) is connected with the far-end computer being connected with printing device.
4. a kind of aircraft detecting peripheral wireless network environment according to claim 1 and 2, it is characterized in that: also include LED light (13), lithium cell (18), LED light (13) is connected with micro controller system main control module (17), and lithium cell (18) is connected with motor (11).
5. a kind of aircraft detecting peripheral wireless network environment according to claim 4, is characterized in that: described fuselage carrier (12) is provided with charge port (19), and described charge port (19) is connected with lithium cell (18).
6. a kind of aircraft detecting peripheral wireless network environment according to claim 4, is characterized in that: described LED light (13) is positioned at the below of fuselage carrier (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520166484.7U CN204473130U (en) | 2015-03-24 | 2015-03-24 | A kind of aircraft detecting peripheral wireless network environment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520166484.7U CN204473130U (en) | 2015-03-24 | 2015-03-24 | A kind of aircraft detecting peripheral wireless network environment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204473130U true CN204473130U (en) | 2015-07-15 |
Family
ID=53628920
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520166484.7U Expired - Fee Related CN204473130U (en) | 2015-03-24 | 2015-03-24 | A kind of aircraft detecting peripheral wireless network environment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204473130U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105711849A (en) * | 2016-01-25 | 2016-06-29 | 深圳市智璟科技有限公司 | Unmanned aerial vehicle and flying state indicating method and device thereof |
-
2015
- 2015-03-24 CN CN201520166484.7U patent/CN204473130U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105711849A (en) * | 2016-01-25 | 2016-06-29 | 深圳市智璟科技有限公司 | Unmanned aerial vehicle and flying state indicating method and device thereof |
| CN105711849B (en) * | 2016-01-25 | 2018-05-15 | 深圳市智璟科技有限公司 | Unmanned plane and its state of flight indicating means and device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150715 Termination date: 20160324 |