CN207937857U - A kind of monitoring unmanned equipment fault detecting system - Google Patents

A kind of monitoring unmanned equipment fault detecting system Download PDF

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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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CN
China
Prior art keywords
module
monitoring probe
plc controller
output end
input terminal
Prior art date
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Expired - Fee Related
Application number
CN201820278294.8U
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Chinese (zh)
Inventor
王锐
伍国华
何敏藩
苗晴
熊彦
石建迈
王炯琦
戎海武
邢立宁
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Foshan University
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Foshan University
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Priority to CN201820278294.8U priority Critical patent/CN207937857U/en
Application granted granted Critical
Publication of CN207937857U publication Critical patent/CN207937857U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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

A kind of monitoring unmanned equipment fault detecting system
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.
CN201820278294.8U 2018-02-27 2018-02-27 A kind of monitoring unmanned equipment fault detecting system Expired - Fee Related CN207937857U (en)

Priority Applications (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

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
CN207937857U true CN207937857U (en) 2018-10-02

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Cited By (2)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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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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