CN207556584U - A kind of six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight - Google Patents
A kind of six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight Download PDFInfo
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- CN207556584U CN207556584U CN201721493617.7U CN201721493617U CN207556584U CN 207556584 U CN207556584 U CN 207556584U CN 201721493617 U CN201721493617 U CN 201721493617U CN 207556584 U CN207556584 U CN 207556584U
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- 238000007689 inspection Methods 0.000 title claims abstract description 19
- 230000005540 biological transmission Effects 0.000 claims abstract description 11
- 230000006641 stabilisation Effects 0.000 claims abstract description 6
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- 229910000838 Al alloy Inorganic materials 0.000 claims description 4
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Abstract
The utility model provides a kind of six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight, and including six rotor wing unmanned aerial vehicle subsystems and ground subsystem, six rotor wing unmanned aerial vehicle subsystems include flight controller and image transmission module；Flight controller includes microprocessor, GPS module, main WIFI module, barometertic altimeter, IMU modules, avoidance sensor, camera cradle head, Gyroscopic stabilization device, six motor-drive circuits and six brushless motors；Image transmission module includes dsp processor, the video camera on camera cradle head and image and sends WIFI module；Ground subsystem includes flying control remote controler, terminal handler, terminal display, image receiving WIFI module and from WIFI module.The communications optical cable inspection system has the advantages that high efficiency, low cost, low danger, high reliability is not easily susceptible to geographical, meteorological condition limitation, easy to operate, and speed is fast, and intelligence degree is high.
Description
Technical field
The utility model is related to a kind of communications optical cable inspection system, especially a kind of six rotor wing unmanned aerial vehicle electric power of autonomous flight
Communications optical cable inspection system.
Background technology
With economic and society development, aerial fiber cable network becomes increasingly complex, this just makes to optical cable power-line patrolling work
Make increasingly heavy.Traditional mainly has high altitude optical cable power-line patrolling mode：Artificial ground line walking, artificial high-altitude line walking, satellite
The modes such as remote sensing, manned helicopter high-altitude line walking.It can be seen that traditional power-line patrolling method inefficiency, and often companion
With high cost, high risk, low reliability is easily limited by geographical, meteorological condition.
Invention content
The technical problems to be solved in the utility model is traditional to high altitude optical cable power-line patrolling inefficiency, and often
Along with high cost, high risk, low reliability is easily limited by geographical, meteorological condition.
In order to solve the above-mentioned technical problem, the utility model provides a kind of six rotor wing unmanned aerial vehicle power communication of autonomous flight
Optical cable inspection system, including six rotor wing unmanned aerial vehicle subsystems and ground subsystem, six rotor wing unmanned aerial vehicle subsystems include flight and control
Device processed and image transmission module；Flight controller includes microprocessor, GPS module, main WIFI module, barometertic altimeter, IMU moulds
Block, avoidance sensor, camera cradle head, Gyroscopic stabilization device, six motor-drive circuits and six brushless motors；Image transmitting
Module includes dsp processor, the video camera on camera cradle head and image and sends WIFI module；Ground subsystem includes
Fly control remote controler, terminal handler, terminal display, image and receive WIFI module and from WIFI module；Microprocessor is distinguished
With GPS module, main WIFI module, barometertic altimeter, IMU modules, avoidance sensor, camera cradle head, Gyroscopic stabilization device and
Six motor-drive circuit electrical connections；Six motor-drive circuits are electrically connected respectively with six brushless motors, for respectively driving
Six brushless motor rotations；Dsp processor sends WIFI module with video camera and image respectively and is electrically connected；Terminal handler point
WIFI module is not received with winged control remote controler, terminal display, image and be electrically connected from WIFI module；Image sends WIFI moulds
Block receives WIFI module wireless communication with image；Main WIFI module from WIFI module with wirelessly communicating.
As the further limits scheme of the utility model, IMU modules be built-in with three-axis gyroscope, three axis accelerometer with
And three axis magnetic compass.
As the further limits scheme of the utility model, video camera is high-resolution DV, and is provided with AV
Interface.
As the further limits scheme of the utility model, microprocessor is STM32 embeded processors.
As the further limits scheme of the utility model, flight controller and image transmission module are fixedly mounted on aluminium conjunction
On golden thin-walled casing.
As the further limits scheme of the utility model, avoidance sensor is ultrasonic sensor.
As the further limits scheme of the utility model, image transmission module further includes the finger being connected with dsp processor
Show lamp.
The beneficial effects of the utility model are：Six rotorcraft is employed as inspection carrier, by its mobility
By force, the characteristics of easy manipulation, pollution-free, easy to maintain and convenience in transport, the limitation of geographical conditions can be overcome, and greatly drop
Low cost；Six rotor wing unmanned aerial vehicle stability are extremely strong, by adjusting posture, can resist the interference of wind with stable suspersion in the air
Ability is strong, and reliability is high, can carry out careful observation to circuit；Pass through GPS navigation satellite system, six rotor wing unmanned aerial vehicle of autonomous flight
Subsystem, ground subsystem form a kind of six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight, aircraft lift-off
Afterwards, it without excessive operation, can realize along high altitude optical cable scheduled circuit automatic detecting；It, can be with there is provided 6 brushless motors
The effectively flight attitude of control six wing unmanned plane of autonomous flight, is conducive to it and accurately flies along scheduled circuit；Employ STM32
Embeded processor has the advantages that low in energy consumption, processing speed is fast；The video camera of setting is digital for the high-resolution with AV interfaces
Video camera has many advantages, such as that shooting speed is fast, data storage is convenient, shooting capacity is big, and high resolution can clearly be schemed
Picture；The communications optical cable inspection system has high efficiency, inexpensive, low danger, high reliability, is not easily susceptible to geographical, meteorological item
The limitation of part, easy to operate, the advantages that speed is fast, and intelligence degree is high.
Description of the drawings
Fig. 1 is the integrated circuit structure diagram of the utility model.
Specific embodiment
For the purpose of this utility model, technical solution and advantage is more clearly understood, with reference to specific embodiment and
The utility model is further described in attached drawing.
As shown in Figure 1, six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight disclosed in the utility model, packet
Six rotor wing unmanned aerial vehicle subsystems and ground subsystem are included, six rotor wing unmanned aerial vehicle subsystems include flight controller and image transmitting mould
Block；Flight controller includes microprocessor, GPS module, main WIFI module, barometertic altimeter, IMU modules, avoidance sensor, takes the photograph
As holder, Gyroscopic stabilization device, six motor-drive circuits and six brushless motors；Image transmission module includes DSP processing
Device, the video camera on camera cradle head and image send WIFI module；Ground subsystem includes flying control remote controler, terminal
Processor, terminal display, image receive WIFI module and from WIFI modules；Microprocessor respectively with GPS module, main WIFI
Module, barometertic altimeter, IMU modules, avoidance sensor, camera cradle head, Gyroscopic stabilization device and six motor-drive circuits
Electrical connection；Six motor-drive circuits are electrically connected respectively with six brushless motors, for respectively driving six brushless motor rotations；
Dsp processor sends WIFI module with video camera and image respectively and is electrically connected；Terminal handler controls remote controler, end with winged respectively
Display, image is held to receive WIFI module and be electrically connected from WIFI module；Image sends WIFI module and receives WIFI with image
Module wirelessly communicates；Main WIFI module from WIFI module with wirelessly communicating.
Wherein, IMU modules are built-in with three-axis gyroscope, three axis accelerometer and three axis magnetic compasses；Video camera is high score
Resolution DV, and it is provided with AV interfaces；Microprocessor is STM32 embeded processors；Flight controller and image pass
Defeated module is fixedly mounted on aluminium alloy thin-walled casing；Avoidance sensor is ultrasonic sensor, and ultrasonic sensor is set altogether
There are four putting, respectively on the four direction all around of aluminium alloy thin-walled casing；Image transmission module further include at DSP
The indicator light that reason device is connected is used to indicate the working condition of image transmitting.Image sends WIFI module, image receives WIFI moulds
Block, main WIFI module and the WIFI module that technical grade is used from WIFI module, have wireless communication distance farther out.Six rotations
Each electronic component of wing unmanned plane subsystem is powered by the rechargeable battery in aluminium alloy thin-walled casing.
Six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight disclosed in the utility model when in use, first
The code of region of patrolling and examining, the unmanned plane that terminal handler will have been demarcated are needed by the winged control remote controler input in ground subsystem
GPS ship trajectories data pass through main WIFI module and the microprocessor that flight controller is wirelessly transmitted to from WIFI module, micro- place
Reason device controls six brushless motors to work respectively by six motor-drive circuits so that mark is arrived in flight to six rotor wing unmanned aerial vehicles automatically
It hovers at fixed initial position GPS coordinate, unmanned plane is in above optical cable to be measured at this time, and head direction and line direction one
It causes；Then the angle of high-resolution DV is adjusted by microprocessor control camera cradle head again, it is ensured that ground subsystem
Image in system is shown normally；Again by GPS module receive GPS data, and by microprocessor under the conditions of GPS data according to boat
Row track data autonomous flight, passes through ultrasonic sensor avoiding obstacles；Light is finally acquired by high-resolution DV
Cable image after dsp processor is handled, reinforms image and sends WIFI module and image reception WIFI module wireless communication,
It passes picture signal back ground subsystem, is shown after terminal handler is handled by terminal display, staff is made independently to supervise
Depending on optical cable health status.
Claims (7)
1. a kind of six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight, it is characterised in that：Including six rotors nobody
Loom system and ground subsystem, six rotor wing unmanned aerial vehicle subsystems include flight controller and image transmission module；Flight control
Device includes microprocessor, GPS module, main WIFI module, barometertic altimeter, IMU modules, avoidance sensor, camera cradle head, gyro
Instrument stabilizer, six motor-drive circuits and six brushless motors；Image transmission module includes dsp processor, mounted on taking the photograph
As the video camera on holder and image send WIFI module；Ground subsystem includes flying control remote controler, terminal handler, terminal
Display, image receive WIFI module and from WIFI modules；Microprocessor is high with GPS module, main WIFI module, air pressure respectively
Spend meter, IMU modules, avoidance sensor, camera cradle head, Gyroscopic stabilization device and six motor-drive circuit electrical connections；Six
Motor-drive circuit is electrically connected respectively with six brushless motors, for respectively driving six brushless motor rotations；Dsp processor point
WIFI module is not sent with video camera and image to be electrically connected；Terminal handler controls remote controler, terminal display, figure with winged respectively
As receiving WIFI module and being electrically connected from WIFI module；Image sends WIFI module and receives WIFI module channel radio with image
Letter；Main WIFI module from WIFI module with wirelessly communicating.
2. six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight according to claim 1, it is characterised in that：
IMU modules are built-in with three-axis gyroscope, three axis accelerometer and three axis magnetic compasses.
3. six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight according to claim 1, it is characterised in that：
Video camera is high-resolution DV, and is provided with AV interfaces.
4. six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight according to claim 1, it is characterised in that：
Microprocessor is STM32 embeded processors.
5. six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight according to claim 1, it is characterised in that：
Flight controller and image transmission module are fixedly mounted on aluminium alloy thin-walled casing.
6. six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight according to claim 1, it is characterised in that：
Avoidance sensor is ultrasonic sensor.
7. six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight according to claim 1, it is characterised in that：
Image transmission module further includes the indicator light being connected with dsp processor.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721493617.7U CN207556584U (en) | 2017-11-10 | 2017-11-10 | A kind of six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721493617.7U CN207556584U (en) | 2017-11-10 | 2017-11-10 | A kind of six rotor wing unmanned aerial vehicle electric power communication optical cable inspection system of autonomous flight |
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| Publication Number | Publication Date |
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| CN207556584U true CN207556584U (en) | 2018-06-29 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109213189A (en) * | 2018-07-19 | 2019-01-15 | 安徽共生物流科技有限公司 | A kind of unmanned plane inspection system and movement determination method |
| CN115494878A (en) * | 2022-10-24 | 2022-12-20 | 中国南方电网有限责任公司超高压输电公司广州局 | Unmanned aerial vehicle line patrol path adjusting method and device based on obstacle avoidance |
-
2017
- 2017-11-10 CN CN201721493617.7U patent/CN207556584U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109213189A (en) * | 2018-07-19 | 2019-01-15 | 安徽共生物流科技有限公司 | A kind of unmanned plane inspection system and movement determination method |
| CN115494878A (en) * | 2022-10-24 | 2022-12-20 | 中国南方电网有限责任公司超高压输电公司广州局 | Unmanned aerial vehicle line patrol path adjusting method and device based on obstacle avoidance |
| CN115494878B (en) * | 2022-10-24 | 2024-06-07 | 中国南方电网有限责任公司超高压输电公司广州局 | Unmanned aerial vehicle line patrol path adjustment method and device based on obstacle avoidance |
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| CB03 | Change of inventor or designer information |
Inventor after: Jiang Ling Inventor after: Wang Hongyan Inventor after: Yu Xingqi Inventor after: Zhao Xuedong Inventor after: Tan Haitao Inventor after: Kong Qingwei Inventor after: Huang Longlong Inventor before: Jiang Ling Inventor before: Wang Hongyan Inventor before: Yu Xingqi Inventor before: Zhao Xuedong Inventor before: Tan Haitao Inventor before: Kong Qingwei Inventor before: Huang Longlong |
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| CB03 | Change of inventor or designer information |