CN205613032U - Wearable model airplane wireless remote control system - Google Patents
Wearable model airplane wireless remote control system Download PDFInfo
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- CN205613032U CN205613032U CN201620348107.XU CN201620348107U CN205613032U CN 205613032 U CN205613032 U CN 205613032U CN 201620348107 U CN201620348107 U CN 201620348107U CN 205613032 U CN205613032 U CN 205613032U
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- 238000003466 welding Methods 0.000 claims description 2
- 238000013461 design Methods 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000003993 interaction Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 6
- 230000005540 biological transmission Effects 0.000 description 5
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Abstract
The utility model provides a wearable model airplane wireless remote control system, including aircraft, left hand controller, right hand controller and printed circuit board, the aircraft passes through the branch and connects the rotor, installs control box and battery below the aircraft, and the battery is installed in the middle of the control box, and the below of control box is connected with the electric telescopic link, and the inside of electric telescopic link is provided with the relay, and the bottom of electric telescopic link is connected with the gripper; compared with the prior art, the utility model discloses following beneficial effect has: the shape and the control mode of traditional controller have been broken through, a new control interaction mode has been proposed for when the staff operated unmanned aerial vehicle again, the operation mode was more various, and it is more simple and convenient to operate, and the cost of learning and study time are lower simultaneously, and design benefit has improved market competition, has reached simple structure and reasonable in design's purpose.
Description
Technical field
The utility model is a kind of wearable model plane wireless remote-control system, belongs to aircraft devices field.
Background technology
Quadrotor uses four rotors as the direct driving force source of flight, rotor is symmetrically distributed in four direction around body, four rotors are in sustained height plane, and the structure of four rotors is all identical with radius, two rotors rotate counterclockwise, two rotors turn clockwise, and four motors are symmetrically installed on the bracket end of aircraft, and support intermediate space lays flight-control computer and external equipment.
Typical conventional helicopters is equipped with a main rotor and a tail slurry.They are the propeller pitch angles being changed screw by controlling steering wheel, thus control attitude and the position of helicopter.Quadrotor unlike this, is to change variable rotor speed by regulating four motor speeds, it is achieved the change of lift, thus controls attitude and the position of aircraft.
With scientific and technological growing, because quadrotor can on high in the characteristic that flies, quadrotor is more and more used in scientific research aspect, but when actually used, because the most build of controller is small and exquisite, when user after a procedure, it is likely that arbitrarily place, when it wants to find again, cumbersome.
And the remote controller moulding of present controller of aircraft is single, control mode is single.
Utility model content
The deficiency existing for prior art, the utility model purpose is to provide a kind of wearable model plane wireless remote-control system, and to solve the problem proposing in above-mentioned background technology, the utility model is easy to use, it is simple to operation, good stability, and reliability is high.
To achieve these goals, the utility model is to realize by the following technical solutions: a kind of wearable model plane wireless remote-control system, including aircraft, left hand controller, right hand controller and printed circuit board, described aircraft connects rotor by pole, the inside of described rotor is provided with brushless electric machine and electron speed regulator, and described electron speed regulator is electrically connected with brushless electric machine；The lower section of described aircraft is provided with control cabinet and battery, described battery is arranged on the centre of control cabinet, the lower section of described control cabinet is connected with electric power expansion link, described electric power expansion link be internally provided with relay, the bottom of described electric power expansion link is connected with gripper, the top of described gripper is provided with grabs hop controller, be internally provided with microprocessor and the 2.4G wireless messages of described control cabinet receive chip, described microprocessor receives chip data by data wire and 2.4G wireless messages and is connected, described microprocessor passes through data wire and relay, grab hop controller and electron speed regulator electron speed regulator is electrically connected with, described battery is electrically connected with electric power expansion link then by relay；The position, the centre of the palm of described left hand controller is provided with left pressure sensor, the forefinger of described left hand controller is provided with positioner by thumb side, the arm position of described right hand controller is cased with arm ring, described arm ring is internally provided with right pressure sensor, and the position, the centre of the palm of described right hand controller is provided with primary pressure sensor；The centre of the palm of described right hand controller is internally provided with printed circuit board, being welded with single-chip microcomputer, holder, 2.4G wireless information transfer chip, DC-DC power module and gravity acceleration sensor on described printed circuit board, described single-chip microcomputer is electrically connected with left pressure sensor, positioner, right pressure sensor and primary pressure sensor by being electrically connected with line；nullThe described output of left pressure sensor is connected with the input of single-chip microcomputer，The output also with right pressure sensor for the input of described single-chip microcomputer、The output of primary pressure sensor、The output of the output of positioner and gravity acceleration sensor connects，The output of described single-chip microcomputer is connected with the output of 2.4G wireless information transfer chip，The input that the output of described 2.4G wireless information transfer chip receives chip with 2.4G wireless messages is connected，The output that described 2.4G wireless messages receives chip is connected with the input of microprocessor，The output of described microprocessor is connected with the input of relay，The output of described relay is connected with the input of electric power expansion link，The output of described microprocessor is also connected with the input grabbing hop controller，The input of the described output and gripper grabbing hop controller is connected，The output of described microprocessor is also connected with the input of electron speed regulator，The output of described electron speed regulator is connected with the input of brushless electric machine.
Further, described rotor is provided with four, four rotors are connected with aircraft by four poles, and described four rotors and four poles are symmetrically installed on the surrounding of aircraft, are mounted on brushless electric machine and the electron speed regulator being electrically connected with each other inside described four rotors.
Further, described positioner is made up of with flexible button downwards the button that upwards stretches, and described flexible button and the button that stretches downwards are for a kind of push type button member.
Further, it is arranged on the right pressure sensor within arm ring at least provided with one.
Further, described DC-DC power module is electrically connected with single-chip microcomputer, holder, 2.4G wireless information transfer chip and gravity acceleration sensor, and described DC-DC power module is for power supply when single-chip microcomputer, holder, 2.4G wireless information transfer chip and the work of gravity acceleration sensor.
Further, described relay flows through the break-make of electric power expansion link electric current by control battery or size then controls electric power expansion link and stretches.
Further, being bi-directionally connected of welding single-chip microcomputer on a printed circuit board and holder.
Further, described left hand controller is identical with the structure of traditional flat with the structure of right hand controller.
The beneficial effects of the utility model: one of the present utility model wearable model plane wireless remote-control system, breach shape and the control mode of traditional controller, propose a kind of new control interactive mode, when making staff operate unmanned plane again, mode of operation is more various, operates easier, learning cost and learning time are lower simultaneously, design ingenious, improve the market competitiveness, reached simple in construction and purpose reasonable in design.
Brief description
By reading the detailed description made non-limiting example with reference to the following drawings, other features, objects and advantages of the present utility model will become more apparent upon:
Fig. 1 is the structural representation of a kind of wearable model plane wireless remote-control system of the utility model；
Fig. 2 is the front view of a kind of wearable model plane wireless remote-control system of the utility model；
Fig. 3 is the gripper structural representation of a kind of wearable model plane wireless remote-control system of the utility model；
Fig. 4 is the structural representation of the left hand controller of a kind of wearable model plane wireless remote-control system of the utility model and right hand controller；
Fig. 5 is the printed circuit board structural representation of a kind of wearable model plane wireless remote-control system of the utility model；
Fig. 6 is the operation principle block diagram of a kind of wearable model plane wireless remote-control system of the utility model；
nullIn figure: 1-aircraft、2-left hand controller、3-printed circuit board、11-rotor、12-control cabinet、13-pole、14-electric power expansion link、15-gripper、16-battery、17-brushless electric machine、18-electron speed regulator、19-data wire、The left pressure sensor of 21-、22-upwards flexible button、23-flexible button downwards、24-is electrically connected with line、25-arm ring、26-right hand controller、The right pressure sensor of 27-、28-primary pressure sensor、29-positioner、31-single-chip microcomputer、32-holder、33-2.4G wireless information transfer chip、34-DC-DC power module、35-gravity acceleration sensor、121-microprocessor、122-2.4G wireless messages receives chip、141-relay、151-grabs hop controller.
Detailed description of the invention
For make the utility model realize technological means, creation characteristic, reach purpose and be easy to understand with effect, below in conjunction with detailed description of the invention, the utility model is expanded on further.
Refer to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5 and Fig. 6, a kind of technical scheme of the utility model offer: a kind of wearable model plane wireless remote-control system, including aircraft the 1st, left hand controller the 2nd, right hand controller 26 and printed circuit board 3, aircraft 1 connects rotor 11 by pole 13, the inside of rotor 11 is provided with brushless electric machine 17 and electron speed regulator 18, and electron speed regulator 18 is electrically connected with brushless electric machine 17.
nullThe lower section of aircraft 1 is provided with control cabinet 12 and battery 16，Battery 16 is arranged on the centre of control cabinet 12，The lower section of control cabinet 12 is connected with electric power expansion link 14，Electric power expansion link 14 be internally provided with relay 141，The bottom of electric power expansion link 14 is connected with gripper 15，The top of gripper 15 is provided with grabs hop controller 151，The microprocessor 121 and 2.4G wireless messages that is internally provided with of control cabinet 12 receives chip 122，Microprocessor 121 receives chip 122 data cube computation by data wire 19 with 2.4G wireless messages，Microprocessor 121 is by data wire 19 and relay 141、Grab hop controller and electron speed regulator 18 electron speed regulator 18 is electrically connected with，Battery 16 is electrically connected with electric power expansion link 14 then by relay 141.
The position, the centre of the palm of left hand controller 2 is provided with left pressure sensor 21, the forefinger of left hand controller 2 is provided with positioner 29 by thumb side, the arm position of right hand controller 26 is cased with arm ring 25, arm ring 25 is internally provided with right pressure sensor 27, and the position, the centre of the palm of right hand controller 26 is provided with primary pressure sensor 28.
The centre of the palm of right hand controller 26 is internally provided with printed circuit board 3, being welded with single-chip microcomputer the 31st, holder the 32nd, 2.4G wireless information transfer chip the 33rd, DC-DC power module 34 and gravity acceleration sensor 35 on printed circuit board 3, single-chip microcomputer 31 is electrically connected with left pressure sensor the 21st, positioner the 29th, right pressure sensor 27 and primary pressure sensor 28 by being electrically connected with line 24.
nullThe output of left pressure sensor 21 is connected with the input of single-chip microcomputer 31，The output also with right pressure sensor 27 for the input of single-chip microcomputer 31、The output of primary pressure sensor 28、The output of the output of positioner 29 and gravity acceleration sensor 35 connects，The output of single-chip microcomputer 31 is connected with the output of 2.4G wireless information transfer chip 33，The input that the output of 2.4G wireless information transfer chip 33 receives chip 122 with 2.4G wireless messages is connected，The output that 2.4G wireless messages receives chip 122 is connected with the input of microprocessor 121，The output of microprocessor 121 is connected with the input of relay 141，The output of relay 141 is connected with the input of electric power expansion link 14，The output of microprocessor 121 is also connected with the input grabbing hop controller 151，The output grabbing hop controller 151 is connected with the input of gripper 15，The output of microprocessor 121 is also connected with the input of electron speed regulator 18，The output of electron speed regulator 18 is connected with the input of brushless electric machine 17，The single-chip microcomputer 31 being welded on printed circuit board 3 is bi-directionally connected with holder 32.
Rotor 11 is provided with four, four rotors 11 are connected with aircraft 1 by four poles 13, four rotors 11 and four poles 13 are symmetrically installed on the surrounding of aircraft 1, internal brushless electric machine 17 and the electron speed regulator 18 being mounted on being electrically connected with each other of four rotors 11.
Positioner 29 is made up of with flexible button 23 downwards the button 22 that upwards stretches, and upper flexible button 22 and the button 23 that stretches downwards, for a kind of push type button member, are arranged on the right pressure sensor 27 within arm ring 25 at least provided with one.
DC-DC power module 34 and single-chip microcomputer the 31st, holder the 32nd, 2.4G wireless information transfer chip 33 and gravity acceleration sensor 35 are electrically connected with, power supply when DC-DC power module 34 works for single-chip microcomputer the 31st, holder the 32nd, 2.4G wireless information transfer chip 33 and gravity acceleration sensor 35.
Relay 141 flows through the break-make of electric power expansion link 14 electric current by control battery 16 or size then controls electric power expansion link 14 and stretches, and left hand controller 2 is identical with the structure of traditional flat with the structure of right hand controller 26.
nullAs an embodiment of the present utility model: first staff dresses left hand controller 2 and right hand controller 26 on left hand and the right hand，When actually used，Gravity acceleration sensor 35 in right hand controller 26 can detect the state of the right hand palm，And send and further process to single-chip microcomputer 31，If gravity acceleration sensor 35 detects the right hand, the palm is in horizontal positioned，Then the transmission of this information is received in chip 122 to 2.4G wireless messages by single-chip microcomputer 31 by 2.4G wireless information transfer chip 33，Microprocessor 121 receives chip 122 by 2.4G wireless messages and receives this information，Then by control electron speed regulator 18，Then control brushless electric machine 17 thus control rotor 11 and rotate，Aircraft 1 is made to hover，Roll about the right hand palm if gravity acceleration sensor 35 detects，Under identical principle，Aircraft about 1 translates，Roll under right hand palm if gravity acceleration sensor 35 detects，Under identical principle，The corresponding anterior-posterior translation of aircraft 1.
nullBefore actual use，Staff can input the critical value of a right pressure in holder 32，When actually used，Right pressure sensor 27 can detect user and is applied to the pressure information on arm ring 25 and transmits to single-chip microcomputer 31，Single-chip microcomputer 31 calculates and after process further，By contrasting with the right pressure threshold being stored in holder 32，If being higher than this critical value，Gravity acceleration sensor 35 detects and rolls about the right hand palm simultaneously，Then the transmission of this information is received in chip 122 to 2.4G wireless messages by single-chip microcomputer 31 by 2.4G wireless information transfer chip 33，Microprocessor 121 receives chip 122 by 2.4G wireless messages and receives this information，Then by control electron speed regulator 18，Then control brushless electric machine 17 thus control rotor 11 left and right turn.
Before actual use, staff can input the critical value of a principal pressure in holder 32, when actually used, primary pressure sensor 28 can detect pressure information when user clenches fist and transmit to single-chip microcomputer 31, single-chip microcomputer 31 calculates and after process further, by contrasting with the principal pressure critical value being stored in holder 32, if being higher than this critical value, then this information transmission to 2.4G wireless messages is received in chip 122 by 2.4G wireless information transfer chip 33 by single-chip microcomputer 31, microprocessor 121 receives chip 122 by 2.4G wireless messages and receives this information, then by control electron speed regulator 18, then control brushless electric machine 17 thus control aircraft 1 and move up and down.
Before actual use, staff can input the critical value of a left pressure in holder 32, when actually used, left pressure sensor 21 can detect pressure information when user's left hand grasps fist and transmit to single-chip microcomputer 31, single-chip microcomputer 31 calculates and after process further, by contrasting with the left pressure threshold being stored in holder 32, if being higher than this critical value, then this information transmission to 2.4G wireless messages is received in chip 122 by 2.4G wireless information transfer chip 33 by single-chip microcomputer 31, microprocessor 121 receives chip 122 by 2.4G wireless messages and receives this information, grab hop controller 151 by control then to control gripper 15 and grab conjunction.
Staff sends control instruction by pressing up flexible button 22 or the button 23 that stretches downwards, this command information can transmit to single-chip microcomputer 31, single-chip microcomputer 31 calculates and after process further, then by 2.4G wireless information transfer chip 33, this information transmission to 2.4G wireless messages is received in chip 122, microprocessor 121 receives chip 122 by 2.4G wireless messages and receives this information, by control relay 141, then control electric power expansion link 14 and stretch.
Of the present utility model general principle and principal character and of the present utility model advantage have more than been shown and described, to those skilled in the art, obvious the utility model is not limited to the details of above-mentioned one exemplary embodiment, and in the case of without departing substantially from spirit or essential attributes of the present utility model, the utility model can be realized in other specific forms.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that include all changes falling in the implication of equivalency and scope of claim in the utility model.Any reference in claim should be considered as limiting involved claim.
In addition, should be understood, although this specification is been described by according to embodiment, but not each embodiment only comprises an independent technical scheme, this narrating mode of specification is only for clarity sake, those skilled in the art should be using specification as an entirety, and the technical scheme in each embodiment also can form, through appropriately combined, other embodiments that it will be appreciated by those skilled in the art that.
Claims (8)
1. a wearable model plane wireless remote-control system, including aircraft, left hand controller, right hand controller and printed circuit board, it is characterized in that: described aircraft connects rotor by pole, the inside of described rotor is provided with brushless electric machine and electron speed regulator, and described electron speed regulator is electrically connected with brushless electric machine；
The lower section of described aircraft is provided with control cabinet and battery, described battery is arranged on the centre of control cabinet, the lower section of described control cabinet is connected with electric power expansion link, described electric power expansion link be internally provided with relay, the bottom of described electric power expansion link is connected with gripper, the top of described gripper is provided with grabs hop controller, be internally provided with microprocessor and the 2.4G wireless messages of described control cabinet receive chip, described microprocessor receives chip data by data wire and 2.4G wireless messages and is connected, described microprocessor passes through data wire and relay, grab hop controller and electron speed regulator electron speed regulator is electrically connected with, described battery is electrically connected with electric power expansion link then by relay；
The position, the centre of the palm of described left hand controller is provided with left pressure sensor, the forefinger of described left hand controller is provided with positioner by thumb side, the arm position of described right hand controller is cased with arm ring, described arm ring is internally provided with right pressure sensor, and the position, the centre of the palm of described right hand controller is provided with primary pressure sensor；
The centre of the palm of described right hand controller is internally provided with printed circuit board, being welded with single-chip microcomputer, holder, 2.4G wireless information transfer chip, DC-DC power module and gravity acceleration sensor on described printed circuit board, described single-chip microcomputer is electrically connected with left pressure sensor, positioner, right pressure sensor and primary pressure sensor by being electrically connected with line；
nullThe described output of left pressure sensor is connected with the input of single-chip microcomputer，The output also with right pressure sensor for the input of described single-chip microcomputer、The output of primary pressure sensor、The output of the output of positioner and gravity acceleration sensor connects，The output of described single-chip microcomputer is connected with the output of 2.4G wireless information transfer chip，The input that the output of described 2.4G wireless information transfer chip receives chip with 2.4G wireless messages is connected，The output that described 2.4G wireless messages receives chip is connected with the input of microprocessor，The output of described microprocessor is connected with the input of relay，The output of described relay is connected with the input of electric power expansion link，The output of described microprocessor is also connected with the input grabbing hop controller，The input of the described output and gripper grabbing hop controller is connected，The output of described microprocessor is also connected with the input of electron speed regulator，The output of described electron speed regulator is connected with the input of brushless electric machine.
2. one according to claim 1 wearable model plane wireless remote-control system, it is characterized in that: described rotor is provided with four, four rotors are connected with aircraft by four poles, described four rotors and four poles are symmetrically installed on the surrounding of aircraft, are mounted on brushless electric machine and the electron speed regulator being electrically connected with each other inside described four rotors.
3. one according to claim 1 wearable model plane wireless remote-control system, it is characterised in that: described positioner is made up of with flexible button downwards the button that upwards stretches, and described flexible button and the button that stretches downwards are for a kind of push type button member.
4. one according to claim 1 wearable model plane wireless remote-control system, it is characterised in that: it is arranged on the right pressure sensor within arm ring at least provided with one.
5. one according to claim 1 wearable model plane wireless remote-control system, it is characterized in that: described DC-DC power module is electrically connected with single-chip microcomputer, holder, 2.4G wireless information transfer chip and gravity acceleration sensor, described DC-DC power module is for power supply when single-chip microcomputer, holder, 2.4G wireless information transfer chip and the work of gravity acceleration sensor.
6. one according to claim 1 wearable model plane wireless remote-control system, it is characterised in that: described relay flows through the break-make of electric power expansion link electric current by control battery or size then controls electric power expansion link and stretches.
7. one according to claim 1 wearable model plane wireless remote-control system, it is characterised in that: welding single-chip microcomputer on a printed circuit board is bi-directionally connected with holder.
8. one according to claim 1 wearable model plane wireless remote-control system, it is characterised in that: described left hand controller is identical with the structure of traditional flat with the structure of right hand controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620348107.XU CN205613032U (en) | 2016-04-25 | 2016-04-25 | Wearable model airplane wireless remote control system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620348107.XU CN205613032U (en) | 2016-04-25 | 2016-04-25 | Wearable model airplane wireless remote control system |
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| CN205613032U true CN205613032U (en) | 2016-10-05 |
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| CN201620348107.XU Withdrawn - After Issue CN205613032U (en) | 2016-04-25 | 2016-04-25 | Wearable model airplane wireless remote control system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105749563A (en) * | 2016-04-25 | 2016-07-13 | 电子科技大学中山学院 | Wearable model airplane wireless remote control system |
| CN107132922A (en) * | 2017-05-15 | 2017-09-05 | 华南理工大学 | A kind of Wearable operation control system based on gesture identification |
| WO2018072155A1 (en) * | 2016-10-19 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Wearable device for controlling unmanned aerial vehicle and unmanned aerial vehicle system |
-
2016
- 2016-04-25 CN CN201620348107.XU patent/CN205613032U/en not_active Withdrawn - After Issue
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105749563A (en) * | 2016-04-25 | 2016-07-13 | 电子科技大学中山学院 | Wearable model airplane wireless remote control system |
| CN105749563B (en) * | 2016-04-25 | 2017-11-07 | 电子科技大学中山学院 | Wearable model airplane wireless remote control system |
| WO2018072155A1 (en) * | 2016-10-19 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Wearable device for controlling unmanned aerial vehicle and unmanned aerial vehicle system |
| CN107132922A (en) * | 2017-05-15 | 2017-09-05 | 华南理工大学 | A kind of Wearable operation control system based on gesture identification |
| CN107132922B (en) * | 2017-05-15 | 2020-06-19 | 华南理工大学 | Wearable operation control system based on gesture recognition |
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Granted publication date: 20161005 Effective date of abandoning: 20171107 |
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| AV01 | Patent right actively abandoned |
Granted publication date: 20161005 Effective date of abandoning: 20171107 |