CN207941199U - A kind of novel unmanned controller - Google Patents
A kind of novel unmanned controller Download PDFInfo
- Publication number
- CN207941199U CN207941199U CN201721823815.5U CN201721823815U CN207941199U CN 207941199 U CN207941199 U CN 207941199U CN 201721823815 U CN201721823815 U CN 201721823815U CN 207941199 U CN207941199 U CN 207941199U
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- China
- Prior art keywords
- fuselage
- motor
- box body
- unmanned plane
- signal booster
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Abstract
The utility model discloses a kind of novel unmanned controllers, its structure includes charging socket, indicator light, fuselage, Signal Booster, derailing switch, rocking bar, motor, head cover, telecontrol antenna, the fuselage front surface is equipped with round charging socket, fuselage roof section welding cap base section, sets that there are five round indicator lights on the head cover top nose.A kind of novel unmanned controller of the utility model, equipped with Signal Booster, when unmanned plane will carry out distance flight, the motor first passed through in Signal Booster starts filter using switch knob, remove electric current unstable in circuit, and unstable electric current improvement is being adjusted to normal current, then in the reception signal for enhancing unmanned plane using signal amplifier, unmanned plane is allow to carry out distance flight, facilitate remote probe, allow staff that can learn the shape of mountain of distant place well, to effectively raise the detection visual field of unmanned plane.
Description
Technical field
The utility model is a kind of novel unmanned controller, belongs to air vehicle technique field.
Background technology
Fly control subsystem be unmanned plane completion take off, airflight, execution task and give an encore recycling etc. entire flight course
Core system, flying control, to be equivalent to driver for unmanned plane man-machine for playing the role of, it is believed that is that unmanned plane is most crucial
One of technology.It is main that winged control generally comprises sensor, airborne computer and servo start equipment three parts, the function of realization
There are unmanned plane attitude stabilization and control, unmanned plane task device management and emergency flight control three categories.
Prior art discloses application No. is：A kind of novel unmanned controller of CN201620314385.3, feature are
It is provided on remote controler shell and determines height/GPS mode selector switch, offline mode without a head switching switch ,/landing mode switching of taking off
It switchs and the switch that makes a return voyage, and the control module by being set to remote controler enclosure interior, includes GPS positioning module, electronics
Compass, gyroscope, large barometer component realize a variety of flight functions of unmanned plane, and the opposite ground for the quality that ensures to take photo by plane is quiet
Only flight function, the flight function of redefining unmanned plane during flying direction, control and allow unmanned plane automatic takeoff and landing function
One key of unmanned plane returns to the function for front position of taking off；Unmanned controller display module can show that unmanned controller receives
Signal strength, unmanned plane and remote controler GPS receive the number of star, unmanned plane with a distance from takeoff point, drone flying height, unmanned plane
And remote controller battery electricity, unmanned plane video shooting duration, the instant operating mode of remote controler and remote controller battery electricity.But
Disadvantage is that dtr signal, unmanned plane cannot carry out distance flight.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of novel unmanned controller, with solution
The problem of certainly above equipment dtr signal, unmanned plane cannot carry out distance flight.
To achieve the goals above, the utility model is to realize by the following technical solutions：A kind of novel unmanned plane
Remote controler, structure include charging socket, indicator light, fuselage, Signal Booster, derailing switch, rocking bar, motor, head cover, remote control day
Line, the fuselage front surface are equipped with round charging socket, fuselage roof section welding cap base section, the head cover
It is set on top nose there are five round indicator light, the fuselage is used with Signal Booster and is fitting to connection, in the fuselage top surface
Centre is equipped with round derailing switch, and with cylinder rocking bar using being flexibly connected, the fuselage interior is fixedly connected the fuselage roof
Machine, the motor is by being electrically connected two telecontrol antennas；The Signal Booster is by circuit board, switch knob, data device, adjusting
Device, data jack, Wiring port, signal amplifier, motor, filter, box body composition, the box body front surface are equipped with circle
Switch knob, for the box body front surface with data device rear surface using being fitting to connection, the half of the adjuster rear end is embedded in box
In body, the box body front surface is equipped with data jack, Wiring port, and the box body is internally provided with circuit board, the circuit board
By being electrically connected motor, the motor is electrically connected signal amplifier, filter.
Further, the derailing switch connects indicator light by fuselage.
Further, the cylinder rocking bar is altogether equipped with two and equilateral in the same size.
Further, the telecontrol antenna generally cylindrical structure.
Further, the motor passes through fuselage connection signal booster.
Further, there are five the round indicator light is set altogether and equilateral in the same size.
Further, the head cover can maximize the shock dynamics for mitigating exotic.
Advantageous effect
A kind of novel unmanned controller of the utility model is equipped with Signal Booster, distance flight is carried out in unmanned plane
When, the motor first passed through in Signal Booster starts filter using switch knob, removes electric current unstable in circuit, and inciting somebody to action
Unstable electric current improvement is adjusted to normal current, then in the reception signal for enhancing unmanned plane using signal amplifier so that
Unmanned plane can carry out distance flight, facilitate remote probe, allow staff that can learn the shape of mountain of distant place well, to have
The detection visual field for improving unmanned plane of effect.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of novel unmanned controller of the utility model；
Fig. 2 is the Signal Booster schematic diagram of the utility model；
Fig. 3 is the rocker structure structural schematic diagram of the utility model.
In figure：Charging socket -1, indicator light -2, fuselage -3, Signal Booster -4, circuit board -401, switch knob -402, number
According to device -403, adjuster -404, data jack -405, Wiring port -406, signal amplifier -407, motor -408, filter -
409, box body -410, derailing switch -5, rocking bar -6, motor -7, head cover -8, telecontrol antenna -9.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below
In conjunction with specific implementation mode, the utility model is expanded on further.
- Fig. 3 is please referred to Fig.1, the utility model provides a kind of technical solution：A kind of novel unmanned controller, structure
Including charging socket 1, indicator light 2, fuselage 3, Signal Booster 4, derailing switch 5, rocking bar 6, motor 7, head cover 8, telecontrol antenna 9,
3 front surface of the fuselage is equipped with round charging socket 1, and 3 top cross-section of the fuselage welds 8 bottom section of head cover, the top
It is set on 8 top nose of lid there are five round indicator light 2, the fuselage 3 is used with Signal Booster 4 and is fitting to connection, the fuselage 3
Top surface center is equipped with round derailing switch 5, and 3 top of the fuselage is used with cylinder rocking bar 6 to be flexibly connected, in the fuselage 3
Portion is fixedly connected with machine 7, and the motor 7 is by being electrically connected two telecontrol antennas 9；The Signal Booster 4 by circuit board 401, open
Close button 402, data device 403, adjuster 404, data jack 405, Wiring port 406, signal amplifier 407, motor 408, filter
Wave device 409, box body 410 form, and 410 front surface of the box body is equipped with round switch knob 402,410 front surface of the box body with
403 rear surface of data device is using being fitting to connection, and the half of 404 rear end of the adjuster is embedded in box body 410, the box body
410 front surfaces are equipped with data jack 405, Wiring port 406, and the box body 410 is internally provided with circuit board 401, the circuit
Plate 401 is electrically connected signal amplifier 407, filter 409 by being electrically connected motor 408, the motor 408.
403 hand-held data gathering device of data device described in this patent, also known as make an inventory machine, palm PC.It is to sweep bar code
Imaging apparatus, RFID technique is integrated with data terminal, with battery can off-line operation terminal computer equipment.Have and adopts in real time
Collect, be automatically stored, instant playback, immediate feedback, automatically processing, automatic transmission function.For field data authenticity, effectively
Property, real-time, availability provide guarantee.It is suitable for hand with integraty, mobility, small, light-weight, high-performance
The features such as holding, the signal amplifier 407 are that Miniature repeater is called mobile phone signal amplifier, are also company of handset, be for
A kind of sci-tech product of amplified signal.There are many type of signal amplifier, such as TV signal amplifiers, receiver amplifier
Deng having signal amplifier inside, all receivers.
It is carrying out in use, using 3 connection signal booster 4 of fuselage first, when unmanned plane will carry out distance flight, first
Start filter 409 using switch knob 402 by the motor 408 in Signal Booster 4, remove electric current unstable in circuit,
And unstable electric current improvement is being adjusted to normal current, then in the reception for enhancing unmanned plane using signal amplifier 407
Signal so that unmanned plane can carry out distance flight, facilitate remote probe, allow staff that can learn the landform shape of distant place well
Shape, to effectively raise the detection visual field of unmanned plane.
The utility model solves the problems, such as it is dtr signal, and unmanned plane cannot carry out distance flight, and the utility model passes through
Above-mentioned component is combined with each other, and is first passed through in Signal Booster equipped with Signal Booster when unmanned plane will carry out distance flight
Motor start filter using switch knob, remove unstable electric current in circuit, and unstable electric current is being improved into adjustment
For normal current, then enhance the reception signal of unmanned plane in use signal amplifier so that unmanned plane can remotely be flown
Row, facilitates remote probe, allows staff that can learn the shape of mountain of distant place well, to effectively raise the spy of unmanned plane
Survey the visual field.It is described in detail below:
410 front surface of the box body is equipped with round switch knob 402,410 front surface of the box body and table after data device 403
Face is using being fitting to connection, and the half of 404 rear end of the adjuster is embedded in box body 410, and 410 front surface of the box body is equipped with
Data jack 405, Wiring port 406, the box body 410 are internally provided with circuit board 401, and the circuit board 401 passes through electrical connection
Motor 408, the motor 408 are electrically connected signal amplifier 407, filter 409.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (6)
1. a kind of novel unmanned controller, structure includes charging socket (1), indicator light (2), fuselage (3), Signal Booster
(4), derailing switch (5), rocking bar (6), motor (7), head cover (8), telecontrol antenna (9), fuselage (3) front surface are equipped with circle
Charging socket (1), fuselage (3) top cross-section weld head cover (8) bottom section, and head cover (8) top nose is equipped with
Five round indicator lights (2), it is characterised in that：
For the fuselage (3) with Signal Booster (4) using being fitting to connection, fuselage (3) the top surface center is equipped with round switch
Using being flexibly connected, machine is fixedly connected with inside the fuselage (3) with cylinder rocking bar (6) for device (5), fuselage (3) top
(7), the motor (7) is by being electrically connected two telecontrol antennas (9)；
The Signal Booster (4) is inserted by circuit board (401), switch knob (402), data device (403), adjuster (404), data
Hole (405), Wiring port (406), signal amplifier (407), motor (408), filter (409), box body (410) composition, institute
It states box body (410) front surface and is equipped with round switch knob (402), box body (410) front surface and data device (403) rear surface
Using fitting connection, the half of adjuster (404) rear end is embedded in box body (410), in box body (410) front surface
Equipped with data jack (405), Wiring port (406), the box body (410) is internally provided with circuit board (401), the circuit board
(401) by being electrically connected motor (408), the motor (408) is electrically connected signal amplifier (407), filter (409).
2. a kind of novel unmanned controller according to claim 1, it is characterised in that：The derailing switch (5) passes through machine
Body (3) connects indicator light (2).
3. a kind of novel unmanned controller according to claim 1, it is characterised in that：The cylinder rocking bar (6) is altogether
It is equipped with two and equilateral in the same size.
4. a kind of novel unmanned controller according to claim 1, it is characterised in that：The telecontrol antenna (9) is whole
For cylindrical structure.
5. a kind of novel unmanned controller according to claim 1, it is characterised in that：The motor (7) passes through fuselage
(3) connection signal booster (4).
6. a kind of novel unmanned controller according to claim 1, it is characterised in that：The circle indicator light (2) is altogether
It is there are five and if equilateral in the same size.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721823815.5U CN207941199U (en) | 2017-12-24 | 2017-12-24 | A kind of novel unmanned controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721823815.5U CN207941199U (en) | 2017-12-24 | 2017-12-24 | A kind of novel unmanned controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207941199U true CN207941199U (en) | 2018-10-09 |
Family
ID=63704611
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721823815.5U Expired - Fee Related CN207941199U (en) | 2017-12-24 | 2017-12-24 | A kind of novel unmanned controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207941199U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109754587A (en) * | 2018-12-26 | 2019-05-14 | 天长市志铖电子科技有限公司 | The method and remote controler of a kind of pair of unmanned plane and remote controler pairing |
-
2017
- 2017-12-24 CN CN201721823815.5U patent/CN207941199U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109754587A (en) * | 2018-12-26 | 2019-05-14 | 天长市志铖电子科技有限公司 | The method and remote controler of a kind of pair of unmanned plane and remote controler pairing |
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| 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 |
Granted publication date: 20181009 Termination date: 20181224 |
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| CF01 | Termination of patent right due to non-payment of annual fee |