CN205594353U - UAV controller - Google Patents
UAV controller Download PDFInfo
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- CN205594353U CN205594353U CN201620411724.XU CN201620411724U CN205594353U CN 205594353 U CN205594353 U CN 205594353U CN 201620411724 U CN201620411724 U CN 201620411724U CN 205594353 U CN205594353 U CN 205594353U
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Abstract
The utility model discloses a UAV controller for remote control unmanned aerial vehicle, including controller main body and wrist strap, controller main body's inside is provided with battery, control module and signal transmission receiving module, and controller main body's upper surface is provided with the display screen, the key that hovers, key, decline key, navigation key and mode key rise, signal transmission receiving module, display screen, the key that hovers, rise key, decline key, navigation key and mode key respectively through wire and control module in succession, the battery be control module, signal transmission receiving module and display screen and supplies power. UAV controller the farthest is 400 meters with unmanned aerial vehicle's radio communication distance. Dressing UAV controller in operator's wrist, pressing the button through a hand and reach the accurate control to unmanned aerial vehicle, watch control body is long -pending little, and convenient operation. Through the flight of pressing a plurality of key control unmanned aerial vehicle, convenient operation, flexibility, and control accuracy is high.
Description
Technical field
This utility model belongs to unmanned aerial vehicle (UAV) control technical field, is specifically related to a kind of unmanned aerial vehicle (UAV) control device.
Background technology
Unmanned plane is made earnest efforts as by vast airborne vehicle fan, and current most of unmanned planes use hand-held remote control
Device, volume is relatively large, needs operator's two-hand control, operation to control inconvenience, particularly some motions
Fan, wants to control unmanned plane in motor process, if using both hands to control, very inconvenient.
Summary of the invention
The purpose of this utility model is to provide a kind of unmanned aerial vehicle (UAV) control device, solves unmanned aerial vehicle (UAV) control in prior art
Device volume is big, and controls the technical problem of inconvenience.
In order to solve above-mentioned technical problem, this utility model adopts the following technical scheme that
A kind of unmanned aerial vehicle (UAV) control device, for remotely pilotless machine, including controller main body and wrist strap, described controller
Main body be internally provided with battery, control module and signal transmission/reception module, the upper surface of controller main body
It is provided with display screen, hovering key, lifting key, decline key, navigation key and mode key；Described signal sends/receives
Module, display screen, hovering key, lifting key, decline key, navigation key and mode key are respectively by wire and control
In succession, battery is that control module, signal transmission/reception module and display screen are powered to module.Unmanned aerial vehicle (UAV) control device with
The wireless communication distance of unmanned plane the most far 400 meters.Unmanned aerial vehicle (UAV) control device is worn on wrist or the arm of operator
On arm, generally right hand wrist, carry out depresses button by another hands and arrive the accurate control to unmanned plane, this
Plant unmanned aerial vehicle (UAV) control body and amass little, and easy to operate.
Improving further, described display location, in the middle part of the upper surface of controller main body, is positioned on the right side of display screen,
Navigation key is between lifting key, decline key, and the plurality of button is arranged in the position of controller body upper surface
Meet Human Engineering Principle, facilitate operator to implement manipulation.
Improving further, described navigation key is rocker structure, and navigation key can be to four, front, rear, left and right side
To rotation, and can automatically return, easy to operate, flexible.
Improving further, described battery is rechargeable battery, and the side of controller main body or the back side arrange promising battery
The socket of charging.In the case of watch is closed, short pressing hovering key, display screen will show current time and electricity
Pond dump energy.When cell voltage is less than 3.55V, unmanned aerial vehicle (UAV) control device automatic shutdown, then must be by filling
Electrical equipment is battery charging.Current electric quantity directly can also be observed at flight interface.The application specify short by for 20-
80ms, length is pressed as 300-600ms.
Improving further, described signal transmission/reception module is communicated with unmanned plane by 2.4G radiofrequency signal,
The timing of unmanned aerial vehicle (UAV) control device sends data to unmanned plane, after unmanned plane receives the information that unmanned aerial vehicle (UAV) control device sends
Make response and feed back to unmanned aerial vehicle (UAV) control device, if unmanned aerial vehicle (UAV) control device does not receives the return path signal of unmanned plane,
Then acquiescence unmanned aerial vehicle (UAV) control device is connected disconnection with the radio communication of unmanned plane.
The process being controlled unmanned plane by unmanned aerial vehicle (UAV) control device is as follows: first pass through short hovering key of pressing, longer by this
Key enters flight interface, between now showing screen display unmanned plane residual non-uniformity, unmanned plane and making a return voyage a little
Vertical dimension, unmanned plane and the horizontal range between making a return voyage a little, battery current electric quantity, unmanned plane current flight
Vertical speed, the horizontal velocity of unmanned plane current flight and unmanned plane and watch control radio communication and be connected shape
The isoparametric instantaneous value of state.
When display screen display flight interface, by stirring to the right navigation key twice, enter state interface, now
Connection status and the unmanned plane of electricity, unmanned plane and unmanned aerial vehicle (UAV) control device that display screen display unmanned plane is current are worked as
Front gps satellite number.The current state of unmanned plane is understood in real time, in order to operator is timely by these parameters
Make next step operation.
Unmanned plane is in normal condition and during with unmanned aerial vehicle (UAV) control device radio communication good connection, in flight circle
Under surface state, stir to the right a navigation key, select " taking off " option, if GPS successfully positions, then unmanned
Machine will rise to the height set, and next step order of wait of hovering.Then under flight interface state, to
A navigation key is stirred on the right side, selects " manipulation unmanned plane " option, enters unmanned plane during flying pose adjustment interface,
Direction and the adjustment of height of unmanned plane is realized the most again by stirring navigation key, pressing lifting key and decline key,
It is short-and-medium by lifting key, and unmanned plane can vertical ascent；Short pressing decline key, unmanned plane can vertically decline.When unmanned
When machine is positioned at certain altitude, respectively forwardly, rear, left and right stir navigation key, then unmanned plane will the most forward,
Afterwards, left and right flight.The shortest press hovering key, unmanned plane during flying pose adjustment interface can be exited, return flight
Interface.
When needs landing unmanned plane, under flight interface state, stir to the right a navigation key, select " fall
Fall " option, and confirm, then unmanned plane drop to ground.After flight terminates, under flight interface state, to
A navigation key is stirred on the right side, selects " shutdown " option, closes unmanned aerial vehicle (UAV) control device.
When running into emergency, as unmanned plane is uncontrolled, for avoiding it to cause bigger danger, pressing is outstanding simultaneously
Stopping key and decline key, the then motor stalls of unmanned plane, unmanned plane will directly fall.
Compared with prior art, this utility model has the advantages that
1, this unmanned aerial vehicle (UAV) control device, volume is little, and easy to operate, and operator is worn in wrist, by one
Hands just can control the flight of unmanned plane.
2, described display location is in the middle part of the upper surface of controller main body, and hovering key, mode key are positioned at display screen
Left side, lifting key, decline key, navigation key and be positioned on the right side of display screen, navigation key be positioned at lifting key,
Declining between key, the plurality of button arranges in the position of controller body upper surface and meets man-machine work
Cheng Xue principle, facilitates operator to implement manipulation.
3, described navigation key is rocker structure, navigation key can to forward and backward, left, have four direction to rotate, and
In can automatically returning, easy to operate, flexible, and control accuracy is high.
4, described battery is rechargeable battery, when electricity deficiency by charger be battery charge, easy to operate.
Accompanying drawing explanation
Fig. 1 is the structural representation of the novel described unmanned aerial vehicle (UAV) control device of this reality.
Fig. 2 is the structural representation of the novel described controller main body of this reality.
Fig. 3 is the structured flowchart of the novel described unmanned aerial vehicle (UAV) control device of this reality.
Detailed description of the invention
In order to be more fully understood that this utility model, explain of the present utility model interior further below in conjunction with embodiment
Hold, but content of the present utility model is not limited solely to the following examples.
As shown in Figure 1, 2, a kind of unmanned aerial vehicle (UAV) control device, for remotely pilotless machine, including controller main body 1 He
Wrist strap 2, be internally provided with battery 18, control module 10 and the signal of described controller main body 1 send/receive
Module 17, the upper surface of controller main body 1 is provided with display screen 11, hovering key 12, lifting key 14, declines
Key 16, navigation key 15 and mode key 13；Described signal transmission/reception module 17, display screen 11, hovering key
12, lifting key 14, decline key 16, navigation key 15 and mode key 13 are respectively by wire and control module 10
In succession, battery 18 is that control module 10, signal transmission/reception module 17 and display screen 11 are powered.Unmanned plane
Controller and the wireless communication distance the most far 400 meters of unmanned plane.Unmanned aerial vehicle (UAV) control device is worn on operator's
In wrist or arm, generally right hand wrist, carry out depresses button by another hands and arrive accurate to unmanned plane
Controlling, its volume of this unmanned aerial vehicle (UAV) control is little, and easy to operate.In the present embodiment, controller main body 1 is square
Shape, wrist strap 2 is rotationally connected with controller main body 2, and wrist strap 2 is formed by two sections, wherein offers on one section many
Individual adjustment hole, the other end is provided with table away from one end of controller main body 1 and buckles, according to the thickness of operator's wrist
The size coordinating adjustment wrist strap buckled by adjustment hole and table, the suitability is strong and easy to operate.Implement at other
In example, controller main body 1 can be that circle waits other shapes.
In the present embodiment, described display screen 11 is positioned at the middle part of the upper surface of controller main body 1, the key 12 that hovers,
Mode key 13 is positioned at the left side of display screen 11, and lifting key 14, decline key 16, navigation key 15 are positioned at display screen
The right side of 11, navigation key 15 is between lifting key 14, decline key 16, and the plurality of button is at controller
The position of body upper surface arranges and meets Human Engineering Principle, facilitates operator to implement manipulation.Implement at other
In example, the position of hovering key 12, lifting key 14, decline key 16, navigation key 15 and mode key 13 does not limit
In this, hovering key 12, lifting key 14, decline key 16, navigation key 15 and mode key 13 can also be arranged on
The both sides of controller main body 1.The application is worn on the right finesse of operator with this unmanned aerial vehicle (UAV) control device, and
When being positioned at operator front, the dead ahead of operator is front, carrys out regulation front, rear, left and right four direction successively.
In the present embodiment, described navigation key 15 is rocker structure, and navigation key 15 can be to front, rear, left and right
Four direction rotates, and can automatically return, easy to operate, flexible.
In the present embodiment, described battery 18 is rechargeable battery, and side or the back side of controller main body 1 are provided with
Socket for battery charging.Unmanned aerial vehicle (UAV) control device close in the case of, short press hovering key 12, display screen 11
Current time and battery dump energy will be shown.When battery electric quantity is less than how many times, it is battery by charger
18 chargings.Current electric quantity directly can also be observed at flight interface.
In the present embodiment, described signal transmission/reception module 17 is led to unmanned plane by 2.4G radiofrequency signal
Letter, the timing of unmanned aerial vehicle (UAV) control device sends data to unmanned plane, and unmanned plane receives the letter that unmanned aerial vehicle (UAV) control device sends
Make response after breath and feed back to unmanned aerial vehicle (UAV) control device, if unmanned aerial vehicle (UAV) control device does not receives the passback of unmanned plane
Signal, then acquiescence unmanned aerial vehicle (UAV) control device is connected disconnection with the radio communication of unmanned plane.
The process being controlled unmanned plane by unmanned aerial vehicle (UAV) control device is as follows: first pass through the short key 12 that hovers of pressing, then length is pressed
This key enters flight interface, now shows unmanned plane residual non-uniformity, unmanned plane and makes a return voyage on display screen 11
Vertical dimension between point, unmanned plane and the horizontal range between making a return voyage a little, battery 18 current electric quantity, unmanned
The vertical speed of machine current flight, the horizontal velocity of unmanned plane current flight and unmanned plane control wireless with watch
The isoparametric instantaneous value of communication connection status.
When display screen 11 shows flight interface, by stirring to the right continuously navigation key, enter state 15 twice
Interface, the connection status of the now display screen display current electricity of unmanned plane, unmanned plane and unmanned aerial vehicle (UAV) control device with
And the gps satellite number that unmanned plane is current.The current state of unmanned plane is understood in real time by these parameters, in order to
Operator makes next step operation in time.
Unmanned plane is in normal condition and during with unmanned aerial vehicle (UAV) control device radio communication good connection, in flight circle
Under surface state, stir to the right a navigation key 15, select " taking off " option, if GPS successfully positions, then
Unmanned plane will rise to the height set, and next step order of wait of hovering.Then under flight interface state,
Stir to the right a navigation key 15, select " manipulation unmanned plane " option, enter unmanned plane during flying pose adjustment circle
Face, realizes the side of unmanned plane the most again by stirring navigation key 15, pressing lifting key 14 and decline key 16
To the adjustment with height, it is short-and-medium by lifting key 14, and unmanned plane can vertical ascent；Short pressing declines key 16, nothing
People's chance vertically declines.When unmanned plane is positioned at certain altitude, respectively forwardly, rear, left and right stir navigation key
15, then unmanned plane will fly to front, rear, left and right accordingly.The shortest press hovering key 12, can exit unmanned
Machine flight attitude adjusts interface, returns to flight interface.
When needs landing unmanned plane, under flight interface state, stir to the right a navigation key 15, select " fall
Fall " option, and confirm, then unmanned plane drop to ground.After flight terminates, under flight interface state, to
A navigation key 15 is stirred on the right side, selects " shutdown " option, closes unmanned aerial vehicle (UAV) control device.
When running into emergency, as unmanned plane is uncontrolled, for avoiding it to cause bigger danger, pressing is outstanding simultaneously
Stopping key 12 and decline key 16, the then motor stalls of unmanned plane, unmanned plane will directly fall.
This utility model does not does illustrate be prior art or can be realized by prior art,
And be embodied as case described in this utility model and be only preferable case study on implementation of the present utility model, and
Non-being used for limits practical range of the present utility model.The most all content institutes according to this utility model claim
Equivalence change and the modification made, all should be used as technology category of the present utility model.
Claims (5)
1. a unmanned aerial vehicle (UAV) control device, for remotely pilotless machine, including controller main body and wrist strap, its feature exists
It is internally provided with battery, control module and signal transmission/reception module, controller in, described controller main body
The upper surface of main body is provided with display screen, hovering key, lifting key, decline key, navigation key and mode key；Described
Signal transmission/reception module, display screen, hovering key, lifting key, decline key, navigation key and mode key lead to respectively
Crossing wire with control module in succession, battery is that control module, signal transmission/reception module and display screen are powered.
Unmanned aerial vehicle (UAV) control device the most according to claim 1, it is characterised in that described display location is in control
The middle part of the upper surface of device main body, hovering key, mode key be positioned at the left side of display screen, lifting key, decline key,
Navigation key is positioned on the right side of display screen, and navigation key is between lifting key, decline key.
Unmanned aerial vehicle (UAV) control device the most according to claim 1 and 2, it is characterised in that described navigation key is
Rocker structure, navigation key can rotate to front, rear, left and right four direction, and can automatically return.
Unmanned aerial vehicle (UAV) control device the most according to claim 3, it is characterised in that described battery is charged electrical
Pond, the side of controller main body or the back side arrange the socket of promising battery charging.
Unmanned aerial vehicle (UAV) control device the most according to claim 4, it is characterised in that described signal sends/receives
Module passes through 2.4G radiofrequency signal and UAV Communication.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620411724.XU CN205594353U (en) | 2016-05-09 | 2016-05-09 | UAV controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620411724.XU CN205594353U (en) | 2016-05-09 | 2016-05-09 | UAV controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205594353U true CN205594353U (en) | 2016-09-21 |
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ID=56930479
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| CN201620411724.XU Active CN205594353U (en) | 2016-05-09 | 2016-05-09 | UAV controller |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106547277A (en) * | 2017-01-16 | 2017-03-29 | 广东容祺智能科技有限公司 | A kind of wearable MAV system based on Internet of Things |
| CN106774292A (en) * | 2016-12-30 | 2017-05-31 | 歌尔科技有限公司 | The wrist-watch and a kind of method of control unmanned plane of a kind of control unmanned plane |
| WO2018053845A1 (en) * | 2016-09-26 | 2018-03-29 | 深圳市大疆创新科技有限公司 | Method and system for controlling unmanned aerial vehicle, and user terminal |
| CN108791880A (en) * | 2018-05-04 | 2018-11-13 | 国电锅炉压力容器检验中心 | A kind of pressure vessel inspection unmanned plane |
| CN113518747A (en) * | 2019-02-22 | 2021-10-19 | 株式会社尼罗沃克 | Unmanned aerial vehicle manipulator and program for manipulation |
-
2016
- 2016-05-09 CN CN201620411724.XU patent/CN205594353U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018053845A1 (en) * | 2016-09-26 | 2018-03-29 | 深圳市大疆创新科技有限公司 | Method and system for controlling unmanned aerial vehicle, and user terminal |
| CN106774292A (en) * | 2016-12-30 | 2017-05-31 | 歌尔科技有限公司 | The wrist-watch and a kind of method of control unmanned plane of a kind of control unmanned plane |
| CN106774292B (en) * | 2016-12-30 | 2023-11-24 | 歌尔科技有限公司 | Watch for controlling unmanned aerial vehicle and method for controlling unmanned aerial vehicle |
| CN106547277A (en) * | 2017-01-16 | 2017-03-29 | 广东容祺智能科技有限公司 | A kind of wearable MAV system based on Internet of Things |
| CN108791880A (en) * | 2018-05-04 | 2018-11-13 | 国电锅炉压力容器检验中心 | A kind of pressure vessel inspection unmanned plane |
| CN113518747A (en) * | 2019-02-22 | 2021-10-19 | 株式会社尼罗沃克 | Unmanned aerial vehicle manipulator and program for manipulation |
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