CN207937857U - A kind of monitoring unmanned equipment fault detecting system - Google Patents
A kind of monitoring unmanned equipment fault detecting system Download PDFInfo
- Publication number
- CN207937857U CN207937857U CN201820278294.8U CN201820278294U CN207937857U CN 207937857 U CN207937857 U CN 207937857U CN 201820278294 U CN201820278294 U CN 201820278294U CN 207937857 U CN207937857 U CN 207937857U
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- module
- monitoring probe
- plc controller
- output end
- input terminal
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Abstract
The utility model discloses a kind of monitoring unmanned equipment fault detecting systems, including power module, PLC controller, communication module, failure monitoring platform, detection module, feedback module, execution module and drive module, the PLC controller is connect by communication module with failure monitoring Platform communication;The detection module output end is connected with feedback module input terminal, the feedback module output end is connected with PLC controller input terminal, the execution module includes main monitoring probe and spare monitoring probe, the drive module includes the first driver and the second driver, and the detection module input terminal is connected with main monitoring probe and spare monitoring probe respectively.The utility model is detected main monitoring probe by detection module, it is transferred data in PLC controller by feedback module, if main monitoring probe operation irregularity, then drive module stops the work of main monitoring probe, and start spare monitoring probe, continue to work to the operating status inside unmanned plane.
Description
Technical field
The utility model is related to UAV system technical fields, more specifically to a kind of monitoring unmanned equipment fault
Detecting system.
Background technology
UAV, abbreviation unmanned plane are manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle.
Unmanned plane is not due to having driver to operate, so being needed when unmanned plane is run using monitoring device to nobody
The operating status of machine is monitored, so as to be timely adjusted to the state of flight of unmanned plane, but monitoring device
It can be broken down due to long-term work, and unmanned plane can not timely be detected it in long-range flight, to bring
Great security risk.
Utility model content
The technical problems to be solved in the utility model is:A kind of monitoring unmanned device detection system is provided.
The solution that the utility model solves its technical problem is:
A kind of monitoring unmanned equipment fault detecting system, including power module, PLC controller, communication module, failure prison
Platform, detection module, feedback module, execution module and drive module are controlled, the power module is powered for each circuit module,
The PLC controller is connect by communication module with failure monitoring Platform communication;The PLC controller output end and detection module
Input terminal is connected, and the detection module output end is connected with feedback module input terminal, and the feedback module output end is controlled with PLC
Device input terminal is connected, and the execution module includes main monitoring probe and spare monitoring probe, and the drive module includes first
Driver and the second driver, the PLC controller output end are electrically connected with the first driver and the second driver respectively,
First driver and the second driver are electrically connected with main monitoring probe and spare monitoring probe respectively, the detection mould
Block input terminal is connected with main monitoring probe and spare monitoring probe respectively.
As a further improvement of the above technical scheme, the communication module includes analog-digital converter, GPRS communication units
And antenna, the PLC controller two-way communication link, the analog-digital converter with GPRS communication units are two-way is electrically connected, institute
GPRS communication units are stated to be electrically connected with antenna.
As a further improvement of the above technical scheme, the power module include solar panel, inverter and
Accumulator, the solar panel are electrically connected with inverter input terminal, and the inverter output end is electrically connected with accumulator, institute
Accumulator is stated to be electrically connected with each circuit module.
As a further improvement of the above technical scheme, the PLC controller model is 226 CN of S7-200 CN CPU.
As a further improvement of the above technical scheme, this system further includes red signal light lamp and green optical signal lamp, institute
PLC controller output end is stated respectively to be connected with red signal light lamp and green optical signal lamp.
The utility model has the beneficial effects that:The utility model by detection module to the working condition of main monitoring probe into
Related data, is transferred in PLC controller, if main monitoring probe operation irregularity, drives by row detection by feedback module
Module stops the work of main monitoring probe, and starts spare monitoring probe, continues to carry out work to the operating status inside unmanned plane
Make.
Description of the drawings
It is required in being described below to embodiment in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing to be used is briefly described.Obviously, described attached drawing is a part of the embodiment of the utility model, rather than complete
Portion's embodiment, those skilled in the art without creative efforts, can also be obtained according to these attached drawings it
His design scheme and attached drawing.
Fig. 1 is the circuit module frame figure of the utility model.
Specific implementation mode
The technique effect of the design of the utility model, concrete structure and generation is carried out below with reference to embodiment and attached drawing
It clearly and completely describes, to be completely understood by the purpose of this utility model, feature and effect.Obviously, described embodiment
It is a part of the embodiment of the utility model, rather than whole embodiments, it is based on the embodiments of the present invention, the skill of this field
The other embodiment that art personnel are obtained without creative efforts belongs to the model of the utility model protection
It encloses.In addition, all connection/connection relations being previously mentioned in text, not singly refer to component and directly connect, and referring to can be according to specific reality
Situation is applied, by adding or reducing couple auxiliary, to form more preferably coupling structure.Each technology in the invention is special
Sign, can be with combination of interactions under the premise of not conflicting conflict.
Referring to Fig.1, the utility model discloses a kind of monitoring unmanned equipment fault detecting system, including power module,
PLC controller, communication module, failure monitoring platform, detection module, feedback module, execution module and drive module, the electricity
Source module is powered for each circuit module, and the PLC controller is connect by communication module with failure monitoring Platform communication;It is described
PLC controller output end is connected with detection module input terminal, and the detection module output end is connected with feedback module input terminal, institute
It states feedback module output end with PLC controller input terminal to be connected, the execution module includes main monitoring probe and spare monitoring
Probe, the drive module include the first driver and the second driver, and the PLC controller output end drives with first respectively
Dynamic device and the electrical connection of the second driver, first driver and the second driver respectively with main monitoring probe and spare
Monitoring probe is electrically connected, and the detection module input terminal is connected with main monitoring probe and spare monitoring probe respectively.Specifically,
The main monitoring probe and spare monitoring probe are the dresses for monitoring unmanned plane operating status in monitoring unmanned equipment
It sets.The utility model is detected the working condition of main monitoring probe by detection module, by feedback module by dependency number
According to being transferred in PLC controller, if main monitoring probe operation irregularity, drive module stops the work of main monitoring probe, and
Start spare monitoring probe, continues to work to the operating status inside unmanned plane.
Specifically, for the detection module for being detected to main monitoring probe and spare monitoring probe, this practicality is new
In type specific implementation mode, the detection module includes for detecting main monitoring probe and spare monitoring probe operating current
Current detecting unit and image identification unit for detecting main monitoring probe and spare monitoring probe Image Acquisition quality,
By the current detecting unit and image identification unit to judge whether main monitoring probe and spare monitoring probe are normal
Work.
It should be noted that although the utility model relates to the use of the technological means of computer program, but the technology hand
Section belongs to the prior art, and the utility model mainly protects the hardware configuration of system.
It is further used as preferred embodiment, in specific embodiment of the present invention, the communication module includes mould
Number converter, GPRS communication units and antenna, the PLC controller two-way communication link, the analog-digital converter and GPRS
The two-way electrical connection of communication unit, the GPRS communication units are electrically connected with antenna.Specifically, specific embodiment of the present invention
In, using the communication connection of GPRS communication modes realization detecting system and monitor supervision platform, transmission rate block, communication range is extensive.
It is further used as preferred embodiment, to make detecting system described in the utility model be suitble to use outdoors, this
In utility model specific embodiment, the power module includes solar panel, inverter and accumulator, the sun
Can solar panel be electrically connected with inverter input terminal, the inverter output end is electrically connected with accumulator, the accumulator with it is each
Circuit module is electrically connected.
It is further used as preferred embodiment, in specific embodiment of the present invention, the PLC controller model
PLC controller for 226 CN of S7-200CN CPU, the model has/16 output of 24 input totally 40 digital quantity I/O points,
With 6 independent 30KHZ high-speed counters, there is the independent 20KHZ high-speed pulse outputs in 2 tunnels, have 2 RS485 logical
News/programming port, powerful, operation and processing speed are preferable.
It is further used as preferred embodiment, in order to which the personnel for making scene operate detecting system have found nothing in time
The fault condition of man-machine monitoring device further includes red signal light lamp and green optical signal in specific embodiment of the present invention
Lamp, the PLC controller output end are connected with red signal light lamp and green optical signal lamp respectively, and green optical signal lamp indicates one when bright
It cuts normally, red signal light lamp indicates that main monitoring probe breaks down when bright.
The better embodiment of the utility model is illustrated above, but the invention be not limited to it is described
Embodiment, those skilled in the art can also make various equivalent changes without departing from the spirit of the present invention
Type or replacement, these equivalent modifications or replacement are all contained in the application claim limited range.
Claims (5)
1. a kind of monitoring unmanned equipment fault detecting system, it is characterised in that:Including power module, PLC controller, communication mould
Block, failure monitoring platform, detection module, feedback module, execution module and drive module, the power module are each circuit
Module for power supply, the PLC controller are connect by communication module with failure monitoring Platform communication;The PLC controller output end
It is connected with detection module input terminal, the detection module output end is connected with feedback module input terminal, the feedback module output
End is connected with PLC controller input terminal, and the execution module includes main monitoring probe and spare monitoring probe, the driving mould
Block includes the first driver and the second driver, and the PLC controller output end drives with the first driver and second respectively
Dynamic device electrical connection, first driver and the second driver are electrically connected with main monitoring probe and spare monitoring probe respectively
It connects, the detection module input terminal is connected with main monitoring probe and spare monitoring probe respectively.
2. a kind of monitoring unmanned equipment fault detecting system according to claim 1, it is characterised in that:The communication mould
Block includes analog-digital converter, GPRS communication units and antenna, the PLC controller two-way communication link, the analog-to-digital conversion
Device with GPRS communication units are two-way is electrically connected, the GPRS communication units are electrically connected with antenna.
3. a kind of monitoring unmanned equipment fault detecting system according to claim 2, it is characterised in that:The power supply mould
Block includes solar panel, inverter and accumulator, and the solar panel is electrically connected with inverter input terminal, described
Inverter output end is electrically connected with accumulator, and the accumulator is electrically connected with each circuit module.
4. a kind of monitoring unmanned equipment fault detecting system according to claim 3, it is characterised in that:The PLC controls
Device model S7-200CN CPU 226CN processed.
5. a kind of monitoring unmanned equipment fault detecting system according to claim 4, it is characterised in that:Further include feux rouges
Signal lamp and green optical signal lamp, the PLC controller output end are connected with red signal light lamp and green optical signal lamp respectively.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201820278294.8U CN207937857U (en) | 2018-02-27 | 2018-02-27 | A kind of monitoring unmanned equipment fault detecting system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820278294.8U CN207937857U (en) | 2018-02-27 | 2018-02-27 | A kind of monitoring unmanned equipment fault detecting system |
Publications (1)
Publication Number | Publication Date |
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CN207937857U true CN207937857U (en) | 2018-10-02 |
Family
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Application Number | Title | Priority Date | Filing Date |
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CN201820278294.8U Expired - Fee Related CN207937857U (en) | 2018-02-27 | 2018-02-27 | A kind of monitoring unmanned equipment fault detecting system |
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CN (1) | CN207937857U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114627634A (en) * | 2022-03-21 | 2022-06-14 | 深圳市大疆创新科技有限公司 | Method for controlling movable platform, registration method and device |
CN116009520A (en) * | 2023-03-27 | 2023-04-25 | 四川腾盾科技有限公司 | Triaxial stability excitation test method for unmanned aerial vehicle |
-
2018
- 2018-02-27 CN CN201820278294.8U patent/CN207937857U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114627634A (en) * | 2022-03-21 | 2022-06-14 | 深圳市大疆创新科技有限公司 | Method for controlling movable platform, registration method and device |
CN116009520A (en) * | 2023-03-27 | 2023-04-25 | 四川腾盾科技有限公司 | Triaxial stability excitation test method for unmanned aerial vehicle |
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
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: 20181002 Termination date: 20200227 |