CN109326112A - A kind of aircraft remote control device and remote control method - Google Patents
A kind of aircraft remote control device and remote control method Download PDFInfo
- Publication number
- CN109326112A CN109326112A CN201811377811.8A CN201811377811A CN109326112A CN 109326112 A CN109326112 A CN 109326112A CN 201811377811 A CN201811377811 A CN 201811377811A CN 109326112 A CN109326112 A CN 109326112A
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- communication unit
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- remote control
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
- H04W4/80—Services using short range communication, e.g. near-field communication [NFC], radio-frequency identification [RFID] or low energy communication
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- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Selective Calling Equipment (AREA)
Abstract
The invention discloses a kind of aircraft remote control device and remote control methods.The device includes: controlling equipment, and the controlling equipment includes the first operational module, the second operational module and the first communication unit, and first communication unit is used to receive the operation signal that the first operational module and/or the second operational module generate；Equipment is controlled, the control equipment includes main control module and the second communication unit；Wherein, second communication unit is connect with first communication unit communication, and the main control module is used to obtain operation signal from second communication unit and be handled, and forms control instruction；The control instruction is sent to aircraft by the second communication unit, to realize the control to aircraft.It may be implemented to redesign the structure of remote controler by the device, to achieve the purpose that really to meet one-handed performance.
Description
Technical field
The present embodiments relate to unmanned vehicle technical field more particularly to a kind of aircraft remote control device and remote control sides
Method.
Background technique
With popularizing for unmanned vehicle, more and more users begin to use unmanned vehicle to carry out various fly
Row operation.
In the prior art, general remote controler needs user's both hands to operate, with reference to Fig. 1, for example, publication No. is
The patent of CN207799884U discloses a kind of remote controler and unmanned flight's system.The controller includes: remote controler main body 10, should
Various cases are provided in controller main body 10, for example, needing to be set in advance when being operated there are two operating stick 16
It sets and learns, it is more demanding for the professional knowledge of operator.Meanwhile the remote controler is also required to both hands and carries out gripping operation,
It may result in both hands while carrying out different operation and causing the operational issue interfered with each other.
Summary of the invention
The present invention provides a kind of aircraft remote control device and remote control method, is set again with realizing to the structure of remote controler
Meter, to achieve the purpose that really to meet one-handed performance.
In a first aspect, the embodiment of the invention provides
A kind of aircraft remote control device characterized by comprising
Controlling equipment, the controlling equipment includes the first operational module, the second operational module and the first communication unit, described
First communication unit is used to receive the operation signal that the first operational module and/or the second operational module generate；Wherein, described first
Operational module and the second operational module include the key that operation signal is generated by pressing；
Cylindricality grip part, the controlling equipment are set to one end of the grip part；
Equipment is controlled, the control equipment includes main control module and the second communication unit；Wherein, second communication unit
It is connect with first communication unit communication, the main control module is used to obtain operation signal from second communication unit and go forward side by side
Row processing, forms control instruction；The control instruction is sent to aircraft by the second communication unit, to realize to aircraft
Control.
Second aspect, the embodiment of the invention also provides a kind of aircraft remote control methods, and the embodiment of the present invention is used to mention
The aircraft remote control device of confession executes, which comprises
It controls equipment and is based on communication mode, receive operation signal；
Control equipment handles the operation signal, forms control instruction, and will generate by the second communication unit
Control instruction pass to aircraft, to control the aircraft.
The present invention solves general aircraft not by the way that mutually contradictory the first operational module and the second operational module is arranged
The problem of energy one-handed performance, the one-handed performance remote control equipment under grip state is realized, under the premise of guaranteeing flight reappearance, reduces and fly
The difficulty of study and the operation of hand improves the beneficial effect for flying the manipulation experience of hand.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of aircraft remote control device in the prior art；
Fig. 2 is a kind of structural schematic diagram for aircraft remote control device that the embodiment of the present invention one provides；
Fig. 3 A is a kind of positive structure schematic of aircraft remote control device provided by Embodiment 2 of the present invention；
Fig. 3 B is a kind of structure schematic diagram of aircraft remote control device provided by Embodiment 2 of the present invention；
Fig. 3 C is a kind of structural schematic diagram of the bottom case of aircraft remote control device provided by Embodiment 2 of the present invention；
Fig. 3 D is a kind of structural schematic diagram of the face-piece of aircraft remote control device provided by Embodiment 2 of the present invention；
Fig. 3 E is a kind of explosive view of aircraft remote control device provided by Embodiment 2 of the present invention；
Fig. 4 is a kind of flow chart for aircraft remote control method that the embodiment of the present invention three provides.
Specific embodiment
The present invention is described in further detail with reference to the accompanying drawings and examples.It is understood that this place is retouched
The specific embodiment stated is used only for explaining the present invention rather than limiting the invention.It also should be noted that in order to just
Only the parts related to the present invention are shown in description, attached drawing rather than entire infrastructure.
Embodiment one
Fig. 2 is a kind of structural schematic diagram for aircraft remote control device that the embodiment of the present invention one provides.Aircraft remote control
Device is for controlling aircraft flight.But it is understood that the technical program is readily applicable in other application scenarios, only
To exist and need to operate a certain equipment by the key module on remote-control handle.In conjunction with Fig. 2, one kind provided in this embodiment
Aircraft remote control device, comprising:
Controlling equipment 100, the controlling equipment 100 include the first operational module 110, the second operational module 120 and first
Communication unit 130, first communication unit 130 are produced for receiving the first operational module 110 and/or the second operational module 120
Raw operation signal.
Wherein, operational module is made of key, and the concrete shape and number of key are with no restrictions.First operational module 110
Including multiple keys, the second operational module 120 also includes multiple keys, the first operational module 110 and the second operational module 120
Case key is independently arranged.First operational module 110 is arranged with second operational module 120 opposition, so that the two modules can
To be operated simultaneously in the case where being hold by one hand remote control device.Communication unit is for acquiring the first operational module 110 and second
The operation signal (electric signal) that the key of operational module 120 generates when being pressed.
Equipment 200 is controlled, the control equipment 200 includes main control module 210 and the second communication unit 220；Wherein, described
Second communication unit 220 is communicated to connect with first communication unit 130, and the main control module 210 is used for logical from described second
Letter unit 220 obtains operation signal and is handled, and forms control instruction；The control instruction passes through the second communication unit 220
It is sent to aircraft, to realize the control to aircraft.
Wherein, main control module 210 is one piece of control chip, can be used for handling operation signal, while can be to behaviour
It is handled as signal, forms control instruction.Second communication unit 220 and the first communication unit 130 communicate to connect, and pass through second
The information between the first operational module 110, the second operational module 120 may be implemented in communication unit 220 and the first communication unit 130
Interaction.Control instruction can be passed to aircraft by way of wireless connection by the second communication unit, to the aircraft
It is controlled.
Specifically, generating its correspondence when the key in the first operational module 110 or the second operational module 120 is pressed
Operation signal, and send the first communication unit 130 for operation signal.First communication unit 130 and the second communication unit 220
Communication connection.Main control module 210 receives the operation signal in the first communication unit 130 by the second communication unit 220, and to behaviour
It is handled as signal, forms control instruction.Control instruction is sent to winged by main control module 210 by the second communication unit 220
Row device, control aircraft fly according to control instruction.
The embodiment of the present invention solves general fly by the way that mutually contradictory the first operational module and the second operational module is arranged
The problem of row device is unable to one-handed performance realizes the one-handed performance remote control equipment under grip state, under the premise of guaranteeing flight reappearance,
The difficulty for flying study and the operation of hand is reduced, the beneficial effect for flying the manipulation experience of hand is improved.
Embodiment two
Fig. 3 A is a kind of positive structure schematic of aircraft remote control device provided by Embodiment 2 of the present invention.Fig. 3 B is this
A kind of structure schematic diagram for aircraft remote control device that inventive embodiments two provide.Fig. 3 C be second embodiment of the present invention provides
A kind of aircraft remote control device bottom case structural schematic diagram.Fig. 3 D is that a kind of aircraft provided by Embodiment 2 of the present invention is distant
Control the structural schematic diagram of the face-piece of device.Fig. 3 E is a kind of explosion of aircraft remote control device provided by Embodiment 2 of the present invention
Figure.The present embodiment is the refinement carried out on the basis of example 1, and the first operational module and the second manipulation mould is described in detail
The structure of block.It is specific with reference to Fig. 3 A, Fig. 3 B, Fig. 3 C, Fig. 3 D and Fig. 3 E:
Remote control device further includes cylindricality grip part 300, and one end of the cylindricality grip part 300 is provided with the manipulation and sets
Standby, one end of the cylindricality grip part 300 is provided with power key 400.
Wherein, cylindricality grip part 300 can be cylinder, or polygon.Knot of the present embodiment to grip part 300
Structure is not specifically limited, as long as meeting manpower gripping.Power key 400 is the key for opening remote control device.
Specifically, remote control device includes grip part 300, one end of grip part 300 is power switch, and power switch is for controlling
Battery processed is remote control device power supply, and the other end of grip part 300 is remote control device, the first operational module 110 of remote control device with
The opposition of second operational module 120 setting.
On the basis of the above embodiments, the first operational module 110 includes: the mobile key for generating movable signal；
The mobile key is connect with the first communication unit communication, for believing to the first communication unit transmitting movable signal as operation
Number.
Specifically, mobile key translates key 1111, right translation key 1112, rear translation key 1113 and a left side before including:
Translate key 1114.Preceding translation key 1111 is used to generate the movable signal moved forward, right translation key 1112 for generating
Movable signal, the rear translation key 1113 to move right is used for generating the movable signal moved backward, left key 1114
In the movable signal that generation is moved to the left.Mobile key is connect with the first communication unit communication, and the first communication unit is for receiving
Forward, movable signal to the right, backward or to the left.
On the basis of the above embodiments, the first operational module 110 includes: the rotating key for generating rotating signal；
The rotating key is connect with the first communication unit communication, for believing to the first communication unit transmitting rotating signal as operation
Number.
Specifically, rotating key includes: right rotation key 1121 and anticlockwise key 1122.Right rotation key 1121 is used for
Dextrorotary movable signal, anticlockwise key 1122 are generated for generating the movable signal rotated to the left.Rotating key and the
The connection of one communication unit communication, the first communication unit are used to receive rotating signal to the right or to the left.
On the basis of the above embodiments, the first operational module 110 includes: the speed key for generating speed signal；
The speed key is connect with the first communication unit communication, for believing to the first communication unit transmission speed signal as operation
Number.
Specifically, speed key includes: that speed adds key 1131 and speed to subtract key 1132.Speed adds key 1131 to be used for
It generates and the speed signal of flight, speed is accelerated to subtract key 1132 for generating the speed signal of decelerating flight.Speed key and
The connection of one communication unit communication, the first communication unit are used to receive the speed signal of acceleration or deceleration.
On the basis of the above embodiments, the first operational module 110 includes: the sprinkling key for generating sprinkling signal；
The sprinkling key is connect with the first communication unit communication, for transmitting sprinkling signal as operation letter to the first communication unit
Number.
Specifically, sprinkling key includes: that sprinkling plus key 1141 and sprinkling subtract key 1142.Sprinkling plus key 1141 are used for
Generate the sprinkling signal for increasing sprinkling amplitude, sprinkling subtracts key 1142 for generating the sprinkling signal for reducing sprinkling amplitude.Sprinkling
Key is connect with the first communication unit communication, and the first communication unit is used to receive the sprinkling signal for increasing or reducing sprinkling amplitude.
On the basis of the above embodiments, the second operational module 120 includes: the throttle key for generating throttle signal；
The throttle key is connect with the first communication unit communication, for believing to the first communication unit transmitting throttle signal as operation
Number.
Specifically, throttle key includes: that throttle adds key 1211 and throttle to subtract key 1212.Throttle adds key 1211 to be used for
Throttle signal, the throttle for generating increase flying height subtract key 1212 for reducing the throttle signal of flying height.Throttle key
It is connect with the first communication unit communication, the first communication unit is for connecing the throttle signal for increasing or decreasing flying height.
On the basis of the above embodiments, remote control device includes: bottom case 500, is equipped with first in the bottom case 500 and accommodates
Slot；Face-piece 700, is equipped with the second holding tank in the face-piece 700, the face-piece 700 with after the bottom case 500 assembling, described the
One holding tank and the second holding tank collectively form the accommodating chamber for accommodating controlling equipment and controlling equipment.
On the basis of the above embodiments, several card line plates, institute are provided in the first holding tank or second holding tank
It states and opens up cable clamping interface 600 on card line plate.
The embodiment of the present invention is by being arranged mutually contradictory the first operational module and the second operational module, and detailed description
The structure of first operational module and the second operational module.It solves the problems, such as that general aircraft is unable to one-handed performance, realizes
The one-handed performance remote control equipment under grip state under the premise of guaranteeing flight reappearance, reduces the difficulty for flying study and the operation of hand, mentions
The beneficial effect that the manipulation of hand of soaring is experienced.
Embodiment three
Fig. 4 is a kind of flow chart for aircraft remote control method that the embodiment of the present invention three provides.The present embodiment is applicable to
Aircraft remote control device is used to control the scene of aircraft flight.But it is understood that the technical program is readily applicable to
In other application scenarios, simply by the presence of needing to operate a certain equipment by key module on remote-control handle.With reference to Fig. 4,
The present embodiment specifically comprises the following steps:
S110, control equipment are based on communication mode, receive operation signal.
Specifically, generating its corresponding operation when the key in the first operational module or the second operational module is pressed
Signal, and the first communication unit is sent by operation signal.First communication unit is connect with the second communication unit communication.Master control mould
Block receives the operation signal in the first communication unit by the second communication unit.
S120, control equipment handle the operation signal, form control instruction, and will by the second communication unit
The control instruction of generation passes to aircraft, to control the aircraft.
Wherein, the control instruction of generation is passed to aircraft by the second communication unit can be by bluetooth, wirelessly
Electricity or other modes establish connection.Optionally, the connection that the second communication unit and unmanned plane can be established by radio station, so that nothing
The man-machine button operation that can receive is instructed and is executed, i.e., the real-time control to unmanned plane is realized based on button operation.
Wherein, the movable signal that control equipment is generated according to mobile key, generates the forward movement with directionality instruction
Instruction, backward move, left-hand move or dextrad move carry out corresponding operating for controlling unmanned plane；
Wherein, the rotating signal that control equipment is generated according to rotating key, generates the left-handed rotation with directionality instruction
Instruction or dextrad rotation instruction, carry out corresponding operating for controlling unmanned plane；
Wherein, the speed signal that control equipment is generated according to speed key, generates assisted instruction or deceleration instruction, for controlling
Unmanned plane processed carries out corresponding operating；
Wherein, the sprinkling signal that control equipment is generated according to sprinkling key, generation, which adds sprinkling instruction or subtracts sprinkling, to be instructed, use
Corresponding operating is carried out in control unmanned plane；
Wherein, the throttle signal that control equipment is generated according to throttle key generates open out instruction or subtracts throttle commands, uses
Corresponding operating is carried out in control unmanned plane.
Specifically, control equipment handles the operation signal received by the second communication channel, forms control and refer to
It enables.Control instruction is sent to aircraft by the second communication unit by control equipment, and control aircraft is carried out according to control instruction
Flight.
Note that the above is only a better embodiment of the present invention and the applied technical principle.It will be appreciated by those skilled in the art that
The invention is not limited to the specific embodiments described herein, be able to carry out for a person skilled in the art it is various it is apparent variation,
It readjusts and substitutes without departing from protection scope of the present invention.Therefore, although being carried out by above embodiments to the present invention
It is described in further detail, but the present invention is not limited to the above embodiments only, without departing from the inventive concept, also
It may include more other equivalent embodiments, and the scope of the invention is determined by the scope of the appended claims.
Claims (12)
1. a kind of aircraft remote control device characterized by comprising
Controlling equipment, the controlling equipment include the first operational module, the second operational module and the first communication unit, described first
Communication unit is used to receive the operation signal that the first operational module and/or the second operational module generate；Wherein, first manipulation
Module and the second operational module include the key that operation signal is generated by pressing；
Cylindricality grip part, the controlling equipment are set to one end of the grip part；
Equipment is controlled, the control equipment includes main control module and the second communication unit；Wherein, second communication unit and institute
The connection of the first communication unit communication is stated, the main control module from second communication unit for from obtaining operation signal and carry out
Reason forms control instruction；The control instruction is sent to aircraft by the second communication unit, to realize the control to aircraft
System.
2. remote control device according to claim 1, which is characterized in that the other end of the cylindricality grip part is provided with power supply
Key.
3. remote control device according to claim 2, which is characterized in that first operational module and the second manipulation mould
Block opposition setting.
4. remote control device according to claim 1, which is characterized in that first operational module includes: for generating shifting
The mobile key of dynamic signal；The mobile key is connect with the first communication unit communication, is moved for transmitting to the first communication unit
Signal is moved as operation signal.
5. remote control device according to claim 1, which is characterized in that first operational module includes: for generating rotation
The rotating key of rotaring signal；The rotating key is connect with the first communication unit communication, is revolved for transmitting to the first communication unit
Rotaring signal is as operation signal.
6. remote control device according to claim 1, which is characterized in that first operational module includes: for generating speed
Spend the speed key of signal；The speed key is connect with the first communication unit communication, for transmitting speed to the first communication unit
Signal is spent as operation signal.
7. remote control device according to claim 1, which is characterized in that first operational module includes: for generating spray
Spill the sprinkling key of signal；The sprinkling key is connect with the first communication unit communication, is sprayed for transmitting to the first communication unit
Signal is spilt as operation signal.
8. remote control device according to claim 1, which is characterized in that second operational module includes: for generating oil
The throttle key of gate signal；The throttle key is connect with the first communication unit communication, for transmitting oil to the first communication unit
Gate signal is as operation signal.
9. remote control device according to claim 1 characterized by comprising
Bottom case, the bottom case is interior to be equipped with the first holding tank；
Face-piece, is equipped with the second holding tank in the face-piece, after the face-piece and bottom case assembling, first holding tank and the
Two holding tanks collectively form the accommodating chamber for accommodating controlling equipment and controlling equipment.
10. remote control device according to claim 9, which is characterized in that first holding tank or second holding tank
Several card line plates are inside provided with, open up cable clamping interface on the card line plate.
11. a kind of aircraft remote control method uses any aircraft remote control device of claim 1-10 to execute,
It is characterized in that, which comprises
It controls equipment and is based on communication mode, receive operation signal；
Control equipment handles the operation signal, forms control instruction, and passes through the second communication unit for the control of generation
System instruction passes to aircraft, to control the aircraft.
12. according to the method for claim 11, which is characterized in that the control equipment to the acquisition information at
Reason forms control instruction, including at least one of following:
The movable signal that the control equipment is generated according to mobile key, generate the forward movement instruction with directionality instruction,
Backward move, left-hand move or dextrad move carry out corresponding operating for controlling unmanned plane；
The rotating signal that is generated according to rotating key of control equipment, generate have the left-handed rotation of directionality instruction instruct or
Dextrad rotation instruction carries out corresponding operating for controlling unmanned plane；
The speed signal that the control equipment is generated according to speed key, generates assisted instruction or deceleration instruction, for controlling nothing
Man-machine carry out corresponding operating；
The sprinkling signal that the control equipment is generated according to sprinkling key generates and adds sprinkling instruction or subtract sprinkling instruction, for controlling
Unmanned plane processed carries out corresponding operating；
The throttle signal that the control equipment is generated according to throttle key generates open out instruction or subtracts throttle commands, for controlling
Unmanned plane processed carries out corresponding operating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811377811.8A CN109326112A (en) | 2018-11-19 | 2018-11-19 | A kind of aircraft remote control device and remote control method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811377811.8A CN109326112A (en) | 2018-11-19 | 2018-11-19 | A kind of aircraft remote control device and remote control method |
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| CN109326112A true CN109326112A (en) | 2019-02-12 |
Family
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|---|---|---|---|
| CN201811377811.8A Pending CN109326112A (en) | 2018-11-19 | 2018-11-19 | A kind of aircraft remote control device and remote control method |
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| CN112799423A (en) * | 2019-10-24 | 2021-05-14 | 广州极飞科技股份有限公司 | Control components and plant protection systems |
| WO2022261857A1 (en) * | 2021-06-16 | 2022-12-22 | 深圳市大疆创新科技有限公司 | Somatosensory remote controller and remote control system |
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| CB02 | Change of applicant information |
Address after: 510000 No. 1, Si Cheng Road, Gaotang Software Park, Tianhe District, Guangzhou, Guangdong 3A01 Applicant after: XAG Co., Ltd. Address before: 510000 No. 1, Si Cheng Road, Gaotang Software Park, Tianhe District, Guangzhou, Guangdong 3A01 Applicant before: Guangzhou Xaircraft Technology Co.,Ltd. |
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Application publication date: 20190212 |
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