CN206984331U - A kind of unmanned plane with auxiliary positioning mechanism easy to identify - Google Patents
A kind of unmanned plane with auxiliary positioning mechanism easy to identify Download PDFInfo
- Publication number
- CN206984331U CN206984331U CN201720516372.9U CN201720516372U CN206984331U CN 206984331 U CN206984331 U CN 206984331U CN 201720516372 U CN201720516372 U CN 201720516372U CN 206984331 U CN206984331 U CN 206984331U
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- China
- Prior art keywords
- unmanned plane
- identify
- control unit
- positioning mechanism
- auxiliary positioning
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Abstract
The utility model provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, including disc main body, several rotor arms, flight remote control and high-definition shooting machine, also include the first control unit and actuating cylinder, the output end of actuating cylinder is connected with Pneumatic clamping jaw, and the first control unit electrically connects with flight remote control, actuating cylinder respectively；The detachable self-induction brightness regulating apparatus being located in Pneumatic clamping jaw, the inside of detachable self-induction brightness regulating apparatus is provided with the second control unit and power subsystem, outside is provided with elastic shock attenuation protecting crust, the outside of elastic shock attenuation protecting crust is provided with strong adherence layer, strong adherence layer is provided with light sensor and LED combination pattern lamp, second control unit electrically connects with power subsystem and light sensor respectively, power subsystem and LED combination pattern lamp electrical connection, can solve the problem that existing unmanned plane ground environment it is dim it is unsharp in the case of can not steadily hovering the problem of.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, more particularly to a kind of nobody with auxiliary positioning mechanism easy to identify
Machine.
Background technology
With progressively going deep into for China's reform, huge transition occur for economic construction fast development, the landforms of each department.
Existing aerial remote sens ing technique means can not adapt to the needs of economic development.New remote sensing technology is that growing economy is built
If with cultural undertakings service.With the technology that unmanned plane (i.e. unmanned plane device) is aerial remote sensing platform, exactly adapting to this needs
The new application technology wanted and grown up, can preferably meet that China is to the need of air remote sensing business at this stage
Ask, outmoded geographic data is updated.Unmanned plane is carried out by radio robot or airborne computer stored program controlled
The not manned vehicle of manipulation；Its is simple in construction, use cost is low, can not only complete the task of manned aircraft execution, more
Should not being performed suitable for someone's aircraft for task.Burst thing is emergent, early warning plays the role of very big, and played in field of photography
Critically important effect.
Unmanned plane photography is using unmanned plane as aerial platform, with airborne sensory equipment, as high resolution CCD is digital
Camera, light optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain information, and image information is entered with computer
Row processing, and it is fabricated to image according to certain required precision；It is well-known, it is desirable to which that shooting effect reaches expected and requires or carry
High shooting effect, it is necessary to assure it is in stable condition when unmanned plane is taken pictures in the air, in other words, it is necessary to assure the hovering of unmanned plane
Effect.The hovering principle of existing unmanned plane is that the fortune of unmanned plane itself is adjusted using the combination of gesture module and Attitude Algorithm
It is dynamic, but if the drift being horizontally oriented, gesture module can not just detect.In order to solve the above-mentioned technical problem, in nothing
One camera directed downwardly of man-machine upper installation, its face landing ground is to shoot the image information on ground；According to the image photographed
Find an object of reference, judge whether unmanned plane has movement with this object of reference.If movement, then opposite direction moves back to
Come, the function of hovering can be realized by so moving in circles.
But this technology has the defects of very big, 1) in the case where the environment of shooting is dark fuzzy, the court installed on unmanned plane
Camera earthward can not shoot ground clearly image, and then can not determine the position of object of reference, i.e., can not judge nobody
The mobile status of machine, the hovering that unmanned plane can not be stablized；2) under the environment that texture on the ground is smudgy, unmanned plane is clapped
The ground image taken the photograph is unsharp, and the mobile status of unmanned plane can not be accurately confirmed according to the texture on ground.
Under above two ambient condition, the hovering effect extreme difference of unmanned plane, shooting effect is extremely unstable, can not play the work of itself
With, service efficiency is low, in emergency situations, results even in serious safety consequences, delay rescue or other events when
Between.
Utility model content
The utility model provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, it is intended to solves existing unmanned plane and exists
Ground environment it is dim it is unsharp in the case of can not steadily hovering the problem of.
The utility model, which is achieved in that, provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, including
Disc main body, several rotor arms, flight remote control and high-definition shooting machine, one end clutch disk shape main frame of rotor arm
Body, the other end of rotor arm are provided with rotor, and high-definition shooting machine is located on the lower surface of disc main body, in addition to
The first control unit being located on disc main body and the power for being located at disc main body lower surface circle centre position
Cylinder, the output end of actuating cylinder are connected with Pneumatic clamping jaw, and the first control unit is electric with flight remote control, actuating cylinder respectively
Connection；
The detachable self-induction brightness regulating apparatus being located in Pneumatic clamping jaw, detachable self-induction brightness regulating apparatus it is interior
Portion is provided with the second control unit and power subsystem, and the outside of detachable self-induction brightness regulating apparatus is protected provided with elastic shock attenuation
Shell, the outside of elastic shock attenuation protecting crust are provided with strong adherence layer, and strong adherence layer is provided with light sensor and LED combination pattern
Lamp, the second control unit electrically connect with power subsystem and light sensor respectively, and power subsystem and LED combination pattern lamp are electrically connected
Connect.
The utility model also provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, the LED combination pattern lamp
It is made up of LED installation base plates and several LED lamp beads, LED lamp bead is arranged on LED installation base plates.
The utility model also provides LED combination pattern lamp described in a kind of unmanned plane with auxiliary positioning mechanism easy to identify and sent out
The pattern formed when bright is letter or number.
The utility model also provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, the LED combination pattern lamp
Outside be provided with transparent antifragmentation plates.
The utility model also provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, and the Pneumatic clamping jaw is provided with
2-4 gripping finger.
The utility model also provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, and the detachable self-induction is bright
The cross section for spending adjusting means is quadrangle, and each face of detachable self-induction brightness regulating apparatus is equipped with LED combination figure
Case lamp.
The utility model also provides a kind of unmanned plane with auxiliary positioning mechanism easy to identify, and the quantity of the rotor arm is
4-6.
The beneficial effects of the utility model are：The utility model provides a kind of nothing with auxiliary positioning mechanism easy to identify
It is man-machine, including the first control unit being located on disc main body and the power for being located at disc main body lower surface circle centre position
Cylinder, the output end of actuating cylinder are connected with Pneumatic clamping jaw, and the first control unit is electric with flight remote control, actuating cylinder respectively
Connection；Detachable self-induction brightness regulating apparatus is provided with Pneumatic clamping jaw, actuating cylinder control Pneumatic clamping jaw clamps and releases
Detachable self-induction brightness regulating apparatus, the inside of detachable self-induction brightness regulating apparatus is provided with the second control unit and power supply
Unit, the outside of detachable self-induction brightness regulating apparatus are provided with elastic shock attenuation protecting crust, set on the outside of elastic shock attenuation protecting crust
Have a strong adherence layer, strong adherence layer is provided with light sensor and LED combination pattern lamp, the second control unit respectively with power supply
Unit and light sensor electrical connection, power subsystem and the electrical connection of LED combination pattern lamp；Tied by above-mentioned electrical control and machinery
Under the cooperation of structure, flight remote control the first control unit of remote control, the first control unit control actuating cylinder action and then
Pneumatic clamping jaw is driven to clamp and release detachable self-induction brightness regulating apparatus, under conditions of it need not hover, pneumatic clamps
Pawl is to be in clamped condition, and when unmanned plane needs hovering, Pneumatic clamping jaw unclamps gripping finger under the driving of actuating cylinder, and release can
Self-induction brightness regulating apparatus is dismantled, is manually placed or allow on its freely falling body to ground, shooting environmental is dim or ground line
Under the unclear use occasion of reason, light-sensing signal is transferred to the second control unit, the control of the second control unit by light sensor
LED combination pattern lamp is shinny, and now, it is shinny that the high-definition shooting machine on unmanned plane can clearly absorb the LED combination pattern lamp
Shi Zhanxian pattern-information is simultaneously compared with the picture that is prestored in it, if both are identical, according to LED combination pattern lamp hair
The pattern adjustment posture showed when bright, keeps steadily hovering；In order to prevent that detachable self-induction brightness regulating apparatus is aerial from height
With breakage after the hard hit of ground after freely falling body, elastic shock attenuation protecting crust is provided with the outside of it；In order to ensure detachable self-induction
Answer brightness regulating apparatus freely landing to rapid precisely fixed on ground, it is viscous to be provided with strength in the outside of elastic shock attenuation protecting crust
Layer is connect, the strong adherence layer can quickly form fixed effect with ground, and it will not produce adhesion between Pneumatic clamping jaw and show
As.
Brief description of the drawings
Fig. 1-3 is structural representation of the present utility model；
Fig. 4 is the internal structure schematic diagram of detachable self-induction brightness regulating apparatus in the utility model；
Fig. 5 is detachable self-induction brightness regulating apparatus lateral surface structural representation in the utility model；
Fig. 6-7 is electrical schematic diagram of the present utility model；
In figure：1- disc main bodies；2- rotor arms；3- flight remote controls；4- high-definition shooting machines；5- first controls list
Member；6- actuating cylinders；7- Pneumatic clamping jaws；The detachable self-induction brightness regulating apparatus of 8-；9- elastic shock attenuation protecting crusts；10- strengths
Adhesive linkage；The transparent antifragmentation plates of 11-；21- rotors；71- gripping fingers；The control units of 81- second；82- power subsystems；83- light levels
Device；84-LED combination pattern lamps.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, below in conjunction with accompanying drawing and implementation
Example, the utility model is further elaborated.It should be appreciated that specific embodiment described herein is only explaining
The utility model, it is not used to limit the utility model.
As shown in figs. 1-7, a kind of unmanned plane with auxiliary positioning mechanism easy to identify, including it is disc main body 1, some
Individual rotor arm 2, flight remote control 3 and high-definition shooting machine 4, one end clutch disk shape main body 1 of rotor arm 2, rotor arm 2
The other end is provided with rotor 21, and high-definition shooting machine 4 is located on the lower surface of disc main body 1, and the quantity of rotor arm 2 is 3-6
Individual, it also includes
The first control unit 5 for being located on disc main body 1 and it is located at the dynamic of the lower surface circle centre position of disc main body 1
Strength cylinder 6, the output end of actuating cylinder 6 are connected with Pneumatic clamping jaw 7, the first control unit 5 respectively with flight remote control 3, dynamic
Strength cylinder 6 electrically connects；Pneumatic clamping jaw 7 is structure common in the art；First control unit 5 is PLC；
The detachable self-induction brightness regulating apparatus 8 being located in Pneumatic clamping jaw 7, the second control unit 81 and electricity are provided with it
Source unit 82, power subsystem 82 are lithium battery, and the outside of detachable self-induction brightness regulating apparatus 8 is provided with elastic shock attenuation protecting crust
9, the outside of elastic shock attenuation protecting crust 9 is provided with strong adherence layer 10, and strong adherence layer 10 is provided with light sensor 83 and LED groups
Pattern lamp 84 is closed, the second control unit 81 electrically connects with power subsystem 82 and light sensor 83 respectively, power subsystem 82 and LED
Combination pattern lamp 84 electrically connects.
In a kind of specific embodiment, the LED combination pattern lamp 84 is by LED installation base plates and several LED lamp bead groups
Into LED lamp bead is arranged on LED installation base plates, and wherein LED installation base plates and LED lamp bead belong to common disclosed in prior art
Structure.
In a kind of specific embodiment, the pattern that the LED combination pattern lamp 84 is formed when shinny is letter or number, than
Such as W, M, Z, A, 1,5,8, or other patterns such as animal picture, bust etc..
In a kind of specific embodiment, the outside of the LED combination pattern lamp 84 is provided with transparent antifragmentation plates 11, and this is transparent anti-
LED combination pattern lamp 84 is completely covered in slashings 11, and protection is formed to it.
In a kind of specific embodiment, it is to ensure preferably to catch that the Pneumatic clamping jaw 7, which is provided with 2-4 gripping finger 71,
Detachable self-induction brightness regulating apparatus 8.
In a kind of specific embodiment, the cross section of the detachable self-induction brightness regulating apparatus 8 is quadrangle, in order to
Ensure that its freely falling body has upset or the possibility rolled to ground, in each of detachable self-induction brightness regulating apparatus 8
Face is equipped with LED combination pattern lamp 84, so, even if detachable self-induction brightness regulating apparatus 8 fall can overturn on the ground or
It is mobile, it can also ensure that high-definition shooting machine 4 can accurately be shot.
During work, the taking lens face ground of high-definition shooting machine 4, LED combination pattern lamp is prestored in high-definition shooting machine 4
84 it is shinny when the object of reference that is hovered as unmanned plane of pattern, manual control unmanned plane is flown, when unmanned plane needs to hover
When, the first control unit of remote control 5 of flight remote control 3, the first control unit 5 control action of actuating cylinder 6 is unclamped pneumatic
The gripping finger of clamping jaw 7, detachable self-induction brightness regulating apparatus 8 is discharged, can only due to the length limitation of the output end of actuating cylinder 6
Selection is manually taken or it is freely fallen on ground, and by taking freely falling body as an example, detachable self-induction brightness regulating apparatus 8 falls
Onto ground, it is located at its outermost strong adherence layer 10 and ground is adhesively fixed, it is not occurred because of falling with ground
Overturn after hard hit and mobile, now, light sensor 83 is detected to the environment of surrounding and transmits signals to second
In control unit 81, if bright surroundings are clear, the second control unit 81 control LED combination pattern lamp 84 is not shinny,
The picture that high-definition shooting machine 4 shoots LED combination pattern lamp 84 and prestored is contrasted, and adjusts the posture of unmanned plane；If now
Surrounding environment is dim unclear, then 84 shinny formation pattern of the second control unit 81 control LED combination pattern lamp, high-definition shooting machine 4
To its clear shooting and analysis contrast can be carried out with the picture that prestores, adjust the posture of unmanned plane；The utility model is using electric
Control and the cooperation of mechanical mechanism, realize the steadily hovering of the unmanned plane under dim environment.
Preferred embodiment of the present utility model is these are only, it is all in this practicality not to limit the utility model
All any modification, equivalent and improvement made within new spirit and principle etc., should be included in guarantor of the present utility model
Within the scope of shield.
Claims (7)
1. a kind of unmanned plane with auxiliary positioning mechanism easy to identify, including disc main body (1), several rotor arms (2),
Flight remote control (3) and high-definition shooting machine (4), one end clutch disk shape main body (1) of rotor arm (2), rotor arm (2)
The other end is provided with rotor (21), and high-definition shooting machine (4) is located on the lower surface of disc main body (1), it is characterised in that：Also
Including
The first control unit (5) for being located on disc main body (1) and it is located at disc main body (1) lower surface circle centre position
Actuating cylinder (6), the output end of actuating cylinder (6) are connected with Pneumatic clamping jaw (7), and the first control unit (5) is distant with flight respectively
Control device (3), actuating cylinder (6) electrical connection；
The detachable self-induction brightness regulating apparatus (8) being located in Pneumatic clamping jaw (7), detachable self-induction brightness regulating apparatus
(8) inside is provided with the second control unit (81) and power subsystem (82), the outside of detachable self-induction brightness regulating apparatus (8)
Provided with elastic shock attenuation protecting crust (9), the outside of elastic shock attenuation protecting crust (9) is provided with strong adherence layer (10), strong adherence layer
(10) be provided with light sensor (83) and LED combination pattern lamp (84), the second control unit (81) respectively with power subsystem
(82) electrically connected with light sensor (83) electrical connection, power subsystem (82) and LED combination pattern lamp (84).
A kind of 2. unmanned plane with auxiliary positioning mechanism easy to identify as claimed in claim 1, it is characterised in that：The LED
Combination pattern lamp (84) is made up of LED installation base plates and several LED lamp beads, and LED lamp bead is arranged on LED installation base plates.
A kind of 3. unmanned plane with auxiliary positioning mechanism easy to identify as described in claim 1 or 2, it is characterised in that：Institute
State LED combination pattern lamp (84) it is shinny when the pattern that is formed be letter or number.
A kind of 4. unmanned plane with auxiliary positioning mechanism easy to identify as claimed in claim 1, it is characterised in that：The LED
The outside of combination pattern lamp (84) is provided with transparent antifragmentation plates (11).
A kind of 5. unmanned plane with auxiliary positioning mechanism easy to identify as claimed in claim 1, it is characterised in that：It is described pneumatic
Clamping jaw (7) is provided with 2-4 gripping finger (71).
A kind of 6. unmanned plane with auxiliary positioning mechanism easy to identify as claimed in claim 1, it is characterised in that：It is described removable
The cross section for unloading self-induction brightness regulating apparatus (8) is quadrangle, and each face of detachable self-induction brightness regulating apparatus (8)
It is equipped with LED combination pattern lamp (84).
A kind of 7. unmanned plane with auxiliary positioning mechanism easy to identify as claimed in claim 1, it is characterised in that：The rotor
The quantity of arm (2) is 4-6.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720516372.9U CN206984331U (en) | 2017-05-10 | 2017-05-10 | A kind of unmanned plane with auxiliary positioning mechanism easy to identify |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720516372.9U CN206984331U (en) | 2017-05-10 | 2017-05-10 | A kind of unmanned plane with auxiliary positioning mechanism easy to identify |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206984331U true CN206984331U (en) | 2018-02-09 |
Family
ID=61391154
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720516372.9U Expired - Fee Related CN206984331U (en) | 2017-05-10 | 2017-05-10 | A kind of unmanned plane with auxiliary positioning mechanism easy to identify |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206984331U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110488237A (en) * | 2019-08-01 | 2019-11-22 | 浙江大学 | A method of classified based on frequency modulated continuous wave radar to unmanned plane rotor number |
-
2017
- 2017-05-10 CN CN201720516372.9U patent/CN206984331U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110488237A (en) * | 2019-08-01 | 2019-11-22 | 浙江大学 | A method of classified based on frequency modulated continuous wave radar to unmanned plane rotor number |
| CN110488237B (en) * | 2019-08-01 | 2021-05-07 | 浙江大学 | Method for classifying number of unmanned aerial vehicle rotors based on frequency modulation continuous wave radar |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20180209 Termination date: 20210510 |