CN106730900A - The motion sensing control handle and its control method of a kind of unmanned vehicle - Google Patents
The motion sensing control handle and its control method of a kind of unmanned vehicle Download PDFInfo
- Publication number
- CN106730900A CN106730900A CN201611192558.XA CN201611192558A CN106730900A CN 106730900 A CN106730900 A CN 106730900A CN 201611192558 A CN201611192558 A CN 201611192558A CN 106730900 A CN106730900 A CN 106730900A
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- aircraft
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- handle
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H30/00—Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
- A63H30/02—Electrical arrangements
- A63H30/04—Electrical arrangements using wireless transmission
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/60—Control of cameras or camera modules
- H04N23/66—Remote control of cameras or camera parts, e.g. by remote control devices
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Mechanical Control Devices (AREA)
Abstract
The present invention relates to technical field of flight control, a kind of motion sensing control handle of unmanned vehicle, including housing and the battery compartment for being arranged at housing are disclosed, it is characterised in that：The housing is provided with switch controlling device, signal processing apparatus and distant bar controlling, the switch controlling device, distant bar controlling are electrically connected with signal processing apparatus, signal processing apparatus are provided with the electrolevel for detecting housing attitude, the signal processing apparatus are electrically connected with battery compartment, handle of the invention not only simple structure and also suitable for beginner manipulate aircraft, operation is easy, controls simpler；And present invention also offers a kind of joystick control method of unmanned vehicle, this control method can make aircraft keep continuous side to fly state, make aircraft when temporarily by obstacle is inclined, it appears be more prone to.
Description
Technical field
The present invention relates to technical field of flight control, more particularly to a kind of unmanned vehicle motion sensing control handle and its control
Method processed.
Background technology
As the demand of unmanned vehicle is increasing, substantial amounts of unmanned vehicle manufacturer has been occurred in that now, these
Unmanned vehicle mainly includes：Spiral paddle, four rotary wind types etc., existing unmanned vehicle are required for using control end and flight
Device sets up flight control connection, and operator is used to control the flight attitude of aircraft on ground i.e. control end.
For especially for quadrotor, existing control mode is often joystick, using its rocking bar with
The cooperation of potentiometer such as realizes accelerating, turns at the elemental motion, when needing to keep continuous side to fly shape control quadrotor
During state, then generally require very skilled operator's ability discontinuous and complete, it is clear that for unskilled or skilled operator
For, it is difficult to reach the holding that continuous side flies state, in view of this, inventor has made new innovation and creation.
The content of the invention
The purpose of the present invention is to solve the shortcomings of the prior art, there is provided a kind of motion sensing control handle of unmanned vehicle,
This joystick has the advantages that simple structure, easily operation and controls；Present invention also offers a kind of control of unmanned vehicle
Handle control method processed, using this control method, can make unmanned plane keep the winged state in continuous side.
To achieve the above object, a kind of motion sensing control handle of unmanned vehicle of the invention, including housing and it is arranged at
The battery compartment of housing, the housing is provided with switch controlling device, signal processing apparatus and distant bar controlling, the switch control
Device processed, distant bar controlling are electrically connected with signal processing apparatus, and signal processing apparatus are provided with for detecting housing appearance
The electrolevel of state, the signal processing apparatus are electrically connected with battery compartment.
Further, the switch controlling device include the first pcb board, first pcb board be provided with power switch and
Body-sensing trigger switch, is provided with the first through hole that power supply source switch stretches out, the anterior setting of the housing at the top of the housing
There is the second through hole that donor sense trigger switch is stretched out, first pcb board is electrically connected with signal processing apparatus.
Preferably, first pcb board is additionally provided with camera control switch, and the front portion of the housing is provided with for camera control
System switch stretches out and three through holes.
Further, the signal processing apparatus include the second pcb board, and second pcb board is connected with MCU, signal and connects
Receiving apparatus and the sender unit for the signal of compiling to be sent to aircraft, the signal receiving device and electronic horizon
Instrument is electrically connected with, and the signal receiving device is electrically connected with by the second pcb board and MCU, and the sender unit is by the
Two pcb boards are electrically connected with MCU.
Further, the signal processing apparatus are also associated with for making the vibrating motor of hull vibration.
Preferably, the distant bar controlling includes control seat and the control-rod being flexibly connected with control seat, the control
Seat is electrically connected with signal processing apparatus, and fourth hole is provided with the top of the housing, and the control-rod passes through fourth hole.
Further, the signal processing apparatus are additionally provided with the micromatic setting of the motor rotary speed for controlling aircraft.
Preferably, the micromatic setting includes that the first trim button, the second trim button, the 3rd trim button and the 4th are micro-
Button is adjusted, is provided with the top of the housing for the first trim button, the second trim button, the 3rd trim button and the 4th fine setting
The fifth hole of button.
A kind of joystick control method of unmanned vehicle of the invention, when body-sensing presses switch to open, electrolevel
The attitude of front handle is detected,
If front handle is left side state, then left side signal L is sent to signal processing apparatus by electrolevel, by
Signal processing means processes signal is simultaneously sent to aircraft by sender unit, and aircraft is left side state；
If front handle is right side heeling condition, then left side signal L is sent to signal processing apparatus by electrolevel, by
Signal processing means processes signal is simultaneously sent to aircraft by sender unit, and aircraft is right side heeling condition；
If front handle is heeling condition under front end, then left side signal L is sent to signal processing apparatus by electrolevel,
Aircraft, aircraft forward flight are sent to by signal processing means processes signal and by sender unit；
If front handle is heeling condition on front end, then left side signal L is sent to signal processing apparatus by electrolevel,
Aircraft is sent to by signal processing means processes signal and by sender unit, aircraft flies backward；
When body-sensing button is closed, aircraft current flight state reverts to floating state.
Further improved, when handle starts motion sensing control, handle at least occurs once to vibrate.
Beneficial effects of the present invention：Compared with prior art, the motion sensing control handle of a kind of unmanned vehicle of the invention,
This joystick detects the attitude of front handle using electrolevel, so as to this attitude signal is sent into signal processing device
The control signal for being processed as aircraft reception is put, operator can hold portion's handle using the hand of itself completely, then by hand
The current pose of direct joystick, is detected by electrolevel immediately, and just corresponding signal is sent to signal processing device
Put and be processed as corresponding flying vehicles control signal, this mode for directly entering line tilt handle using hand control aircraft with
Obtain the corresponding attitude of aircraft, handle of the invention not only simple structure but also manipulates aircraft, operation suitable for beginner
Easily, control simpler；And present invention also offers a kind of joystick control method of unmanned vehicle, this control method
Aircraft can be made to keep continuous side to fly state, make aircraft when temporarily by obstacle is inclined, it appears be more prone to.
Brief description of the drawings
Fig. 1 is the front view of handle of the present invention.
Fig. 2 is the structural decomposition diagram of handle of the present invention.
Fig. 3 is the top view of handle of the present invention.
Fig. 4 is the full sectional view of handle of the present invention.
Reference：
Housing -- 1, drain pan -- 11, face-piece -- 12,
Battery compartment -- 13, switch controlling device -- 2, the first pcb board -- 21,
Power switch -- 22, body-sensing trigger switch -- 23, camera control switch -- 24,
Signal processing apparatus -- 3, the second pcb board -- 31, distant bar controlling -- 4,
Control seat -- 41, control-rod -- 42, electrolevel -- 5,
Vibrating motor -- 6, micromatic setting -- 7, the first trim button -- 71,
Second trim button -- 72, the 3rd trim button -- 73, the 4th trim button -- 74.
Specific embodiment
The present invention will be described in detail below in conjunction with the accompanying drawings.
Referring to Fig. 1 to Fig. 4, the present invention provides a kind of motion sensing control handle of unmanned vehicle, including housing 1 and is arranged at
The battery compartment 13 of housing 1, battery compartment 13 is used to install common battery, wherein, housing 1 includes drain pan 11 and face-piece 12, face-piece
12 is fixed by screw etc. with drain pan 11, and battery compartment 13 can preferably be arranged at the bottom surface of drain pan 11, and the housing 1 is provided with
Switch controlling device 2, signal processing apparatus 3 and distant bar controlling 4, the switch controlling device 2, distant bar controlling 4 are equal
It is electrically connected with signal processing apparatus 3, signal processing apparatus 3 are provided with the electrolevel 5 for detecting the attitude of housing 1, institute
Signal processing apparatus 3 are stated to be electrically connected with battery compartment 13.The operation principle of this motion sensing control handle is：Switch controlling device 2 is led
It is used for the power supply of joystick, and controls being turned on and off for motion sensing control function, is opened when motion sensing control function is in
When opening state, electrolevel 5 detects the attitude of front handle, for example：When front handle is left side state, electronic horizon
Instrument 5 transmits a signal to signal processing apparatus 3, and the Electric signal processing of electrolevel 5 is aircraft institute energy by signal processing apparatus 3
The remote signal of reception, and sent remote signal by sender unit, received by aircraft and be changed aircraft
Current pose be left side state.
It can thus be seen that this joystick detects the attitude of front handle using electrolevel 5, so as to by this appearance
State signal is sent to the control signal that signal processing apparatus 3 are processed as aircraft reception, and operator can utilize itself completely
Hand holds portion's handle, then by the current pose of the direct joystick of hand, is detected by electrolevel 5 immediately, just right
The signal answered is sent to signal processing apparatus 3 and is processed as corresponding flying vehicles control signal, this directly to be inclined using hand
The mode of oblique handle controls aircraft to obtain the corresponding attitude of aircraft, handle of the invention not only simple structure but also
Aircraft is manipulated suitable for beginner, operation is easy, controls simpler.
Generally, aircraft before flight is prepared, it is necessary to limited the relevant control of joystick, in the technical program
In, the switch controlling device 2 includes the first pcb board 21, and first pcb board 21 is provided with power switch 22 and body-sensing triggering
Switch 23, the top of the housing 1 is provided with the first through hole that power supply source switch 22 stretches out, and the front portion of the housing 1 is provided with
The second through hole that donor sense trigger switch 23 is stretched out, first pcb board 21 is electrically connected with signal processing apparatus 3.Power supply is opened
The effect for closing 22 is the power supply for controlling whole handle, when aircraft needs to take off, the power switch 22 is opened, using handle
Distant bar controlling 4 aircraft takeoff is risen in floating state, when needing to adjust the attitude of aircraft or carry out level
During flight, user can directly utilize finger down body-sensing trigger switch 23, and at this moment, the motion sensing control of this handle is activated, electricity
Sub- level meter 5 detects the attitude of front handle, when operator needs the aircraft to carry out left side flight, operator only need to by
Handle is inclined to the left, while the front end of front hand grip is downward-sloping, at this moment, electrolevel 5 will corresponding signal send by believing
Number processing unit 3 is processed, and is sent by sender unit, is received so as to the synchronous left side for realizing aircraft by aircraft
Lateral attitude, and aircraft forward flight, and when user's releaser sense trigger switch 23, by electrolevel 5 no longer
The attitude of front handle is detected, aircraft is in default floating state automatically.
Same principle is：When needing adjustment aircraft with right side lateral attitude flight forward, user can be directly sharp
Press...with one's finger lower body sense trigger switch 23, and at this moment, the motion sensing control of this handle is activated, the detection front handle of electrolevel 5
Attitude, operator need aircraft carry out right side incline flight, operator only needs to the right incline handle, while remote holder
The front end of handle is downward-sloping, at this moment, electrolevel 5 will corresponding signal send and processed by signal processing apparatus 3, and by
Sender unit sends, and is received so as to the synchronous right side lateral attitude for realizing aircraft, while aircraft is forward by aircraft
Flight.
If necessary to aircraft with right side lateral attitude or left side attitude backward flight when, i.e., under heeling condition fall
Fly, user can directly utilize finger down body-sensing trigger switch 23, and at this moment, the motion sensing control of this handle is activated, electronic water
Level 5 detects the attitude of front handle, and operator needs that aircraft carries out right side inclination or left side is flown, and operator only needs
Handle is inclined or left side to the right, while the front end of front hand grip is inclined upwardly, at this moment, electrolevel 5 will be right
The signal answered send and is processed by signal processing apparatus 3, and is sent by sender unit, is received so as to synchronous real by aircraft
The right side of existing aircraft inclines or left side attitude, while aircraft flies backward, i.e. inverted flight under heeling condition.
Now, most unmanned vehicle can install camera, and in the technical program, first pcb board 21 also sets
Camera control switch 24 is equipped with, the front portion of the housing 1 is provided with stretched out for camera control switch 24 and three through holes.The phase
Machine controlling switch 24 not necessarily only controls camera, and it can also directly control the imaging devices such as video camera, and by the camera control
System switch 24 is arranged at the front portion of housing 1, is conducive to hand in gripping handle, and the camera can be easily pressed using finger
Controlling switch 24, also meets the design of ergonomics.
In the technical program, the signal processing apparatus 3 include the second pcb board 31, and second pcb board 31 is connected with
MCU, signal receiving device and the sender unit for the signal of compiling to be sent to aircraft, the signal receiving device
It is electrically connected with electrolevel 5, electrolevel 5 can be fixed using the second pcb board 31, the signal receiving device
It is electrically connected with MCU by the second pcb board 31, the sender unit is electrically connected with by the second pcb board 31 with MCU.Letter
Number reception device carries out relaying to the electric signal of electrolevel 5 and sends MCU to, and the effect of sender unit is by MCU
The remote signal of the 2.4GHz of reason is sent out outside handle, so that aircraft can receive this wishes control signal from a great distance, signal is received
Device directly uses existing mature technology scheme with sender unit, therefore, the present invention is not repeated.
In most cases, whether people easily forget press some function buttons when various control ends are operated,
So, often there is the operation of repeatability, to cause the error in flight, therefore, in the technical program, at the signal
Reason device 3 is also associated with the vibrating motor 6 for vibrating housing 1.When signal processing apparatus 3 receive various shift knob letters
Number when, signal processing apparatus 3 send signal, and control vibrating motor 6 works 0.5 ~ 2 second, so, can reach prompting effector
Effect.
In the technical program, the distant bar controlling 4 includes control seat 41 and the control being flexibly connected with control seat 41
Bar processed 42, the control seat 41 is electrically connected with signal processing apparatus 3, and the top of the housing 1 is provided with fourth hole, described
Control-rod 42 passes through fourth hole.It is single potentiometer in control seat 41, this distant bar controlling 4 is mainly aircraft to be needed
Fly when, push lever 42 forward so that aircraft rise be in floating state；When aircraft needs landing, control is promoted
Bar processed 42 backward so that aircraft down drops back to ground；When aircraft in floating state when needing, control is promoted
Bar processed 42 to the left so that aircraft realize turn to the left；When aircraft in floating state when needing to turn right, control is promoted
Bar processed 42 to the right so that aircraft realize turn to the right；Regardless of whether be control-rod 42 forward, backward, to the left or to the right after,
Can be resetted automatically.
For quadrotor, the rotating speed control of four motors having seems and is even more important, and to realize flight
The smooth flight of device is, it is necessary to the rated speed tolerance value of four motors reaches minimum, it is generally the case that four specified turn of motor
Speed is respectively provided with different tolerance values, in order that when four motors are controlled, obtaining more accurate rotating speed control；In this programme
In, the signal processing apparatus 3 are additionally provided with the micromatic setting 7 of the motor rotary speed for controlling aircraft.Filled using the fine setting
Put 7 volume step rotating speeds that can be respectively to different motors to be adjusted, be particularly conducive to aircraft when flight is inclined, motor is exported
Rotating speed stabilization improving the holding of aircraft lateral attitude.
For micromatic setting 7, the micromatic setting 7 includes that the first trim button 71, the second trim button the 72, the 3rd are finely tuned
The trim button 74 of button 73 and the 4th, the top of the housing 1 be provided with for the first trim button 71, the second trim button 72,
The fifth hole of the 3rd trim button 73 and the 4th trim button 74.First trim button 71, the second trim button the 72, the 3rd are micro-
The trim button 74 of button 73 and the 4th is adjusted to correspond to one motor control of aircraft of control, for example：Assuming that the volume of the first motor
Determine rotating speed to need the rated speed of the 95%, second motor that voltage is predeterminated voltage V to need voltage is the 90% of predeterminated voltage V, the
It is default electricity that the rated speed of three motors needs the rated speed of the 105%, the 4th motor that voltage is predeterminated voltage V to need voltage
The 100% of pressure V, then adjusted, the second trim button 72, the 3rd trim button 73 and the 4th fine setting are pressed using the first trim button 71
Button 74 is finely adjusted to it respectively, so, you can the initial speed of motor is approached to greatest extent, then leads to again
Cross the percentage of control voltage to realize the accurate manipulation of motor, to reach the precise control of aircraft.
A kind of joystick control method of unmanned vehicle of the invention, when body-sensing presses switch to open, electrolevel 5
The attitude of front handle is detected,
When manipulator needs aircraft with left side state, front handle is set to left side state, then electronic horizon
Left side signal L is sent to signal processing apparatus 3 by instrument 5, by the process signal of signal processing apparatus 3 and by sender unit
Aircraft is sent to, aircraft is left side state；
When manipulator needs aircraft with right side heeling condition, front handle is set to right side heeling condition, then electronic horizon
Left side signal L is sent to signal processing apparatus 3 by instrument 5, by the process signal of signal processing apparatus 3 and by sender unit
Aircraft is sent to, aircraft is right side heeling condition；
When aircraft needs aircraft forward flight in floating state, and manipulator, front handle is set to front end and is had a down dip
Ramp-like state, then electrolevel 5 left side signal L is sent to signal processing apparatus 3, process letter by signal processing apparatus 3
Number and aircraft, aircraft forward flight are sent to by sender unit；
When manipulator needs aircraft flight backward, front handle is set to heeling condition on front end, then electrolevel 5 will
Left side signal L is sent to signal processing apparatus 3, is sent by the process signal of signal processing apparatus 3 and by sender unit
To aircraft, aircraft flies backward.
And be more importantly, it is necessary to when aircraft is with left side or right side heeling condition flight forward, such as incite somebody to action current
Handle is set to left side state, meanwhile, the front end of handle is set to downward-sloping state, now, aircraft is left side
State and flight forward state is kept, the state that this holding inclines flight forward has continuity, and can grasp temporarily
Control makes aircraft realize inclining；Such as by front handle be set to right side heeling condition, meanwhile, make handle front end be set to it is downward-sloping
State, now, aircraft is right side heeling condition and keeps flight forward state, and this holding inclines the state of flight forward
With continuity, and can manipulate temporarily makes aircraft realize inclining.
When needing manipulation aircraft with left side or right side heeling condition flight backward, front handle is such as set to a left side
Side heeling condition, meanwhile, the front end of handle is set to the state of being inclined upwardly, now, aircraft is left side state and protects
Hold state of flight backward, i.e. left side inverted flight；Front handle is such as set to right side heeling condition, meanwhile, make the front end of handle
The state of being inclined upwardly is set to, now, aircraft is right side heeling condition and keeps state of flight backward, i.e., right side inclines
Fly, this state for keeping flight tilted backwards has continuity, and can manipulate temporarily makes aircraft realize inclining, and makes to fly
Row device is when temporarily by obstacle is inclined, it appears be more prone to.
When body-sensing button is closed, aircraft current flight state reverts to floating state.
Certainly, in order that manipulator obtains more preferably operating experience, as more excellent control method,
When handle starts motion sensing control, handle at least occurs once to vibrate.So, by operator under the prompting of vibration,
Under can accurately knowing currently to have switched to motion sensing control state.
Above content is only presently preferred embodiments of the present invention, for one of ordinary skill in the art, according to of the invention
Thought, will change in specific embodiments and applications, and this specification content should not be construed as to the present invention
Limitation.
Claims (10)
1. a kind of motion sensing control handle of unmanned vehicle, including housing and the battery compartment for being arranged at housing, it is characterised in that：Institute
State housing and be provided with switch controlling device, signal processing apparatus and distant bar controlling, the switch controlling device, the control of distant bar
Device is electrically connected with signal processing apparatus, and signal processing apparatus are provided with the electrolevel for detecting housing attitude,
The signal processing apparatus are electrically connected with battery compartment.
2. the motion sensing control handle of a kind of unmanned vehicle according to claim 1, it is characterised in that：The switch control
Device includes the first pcb board, and first pcb board is provided with power switch and body-sensing trigger switch, is set at the top of the housing
It is equipped with the power supply first through hole stretched out of source switch, the front portion of the housing is provided with second that donor sense trigger switch stretches out and leads to
Hole, first pcb board is electrically connected with signal processing apparatus.
3. the motion sensing control handle of a kind of unmanned vehicle according to claim 2, it is characterised in that：First PCB
Plate is additionally provided with camera control switch, and the front portion of the housing is provided with stretched out for camera control switch and three through holes.
4. the motion sensing control handle of a kind of unmanned vehicle according to claim 1, it is characterised in that：The signal transacting
Device includes the second pcb board, and second pcb board is connected with MCU, signal receiving device and for the signal of compiling to be sent to
The sender unit of aircraft, the signal receiving device is electrically connected with electrolevel, and the signal receiving device leads to
Cross the second pcb board to be electrically connected with MCU, the sender unit is electrically connected with by the second pcb board with MCU.
5. the motion sensing control handle of a kind of unmanned vehicle according to claim 1, it is characterised in that：The signal transacting
Device is also associated with for making the vibrating motor of hull vibration.
6. the motion sensing control handle of a kind of unmanned vehicle according to claim 5, it is characterised in that：The distant bar control
Device includes control seat and the control-rod being flexibly connected with control seat, and the control seat is electrically connected with signal processing apparatus, institute
State and fourth hole is provided with the top of housing, the control-rod passes through fourth hole.
7. the motion sensing control handle of a kind of unmanned vehicle according to claim 1, it is characterised in that：The signal transacting
Device is additionally provided with the micromatic setting of the motor rotary speed for controlling aircraft.
8. the motion sensing control handle of a kind of unmanned vehicle according to claim 7, it is characterised in that：The micromatic setting
Including the first trim button, the second trim button, the 3rd trim button and the 4th trim button, it is provided with the top of the housing
For the fifth hole of the first trim button, the second trim button, the 3rd trim button and the 4th trim button.
9. the joystick control method of a kind of unmanned vehicle, it is characterised in that：When body-sensing presses switch to open, electrolevel
The attitude of front handle is detected,
If front handle is left side state, then left side signal L is sent to signal processing apparatus by electrolevel, by
Signal processing means processes signal is simultaneously sent to aircraft by sender unit, and aircraft is left side state；
If front handle is right side heeling condition, then left side signal L is sent to signal processing apparatus by electrolevel, by
Signal processing means processes signal is simultaneously sent to aircraft by sender unit, and aircraft is right side heeling condition；
If front handle is heeling condition under front end, then left side signal L is sent to signal processing apparatus by electrolevel,
Aircraft, aircraft forward flight are sent to by signal processing means processes signal and by sender unit；
If front handle is heeling condition on front end, then left side signal L is sent to signal processing apparatus by electrolevel,
Aircraft is sent to by signal processing means processes signal and by sender unit, aircraft flies backward；
When body-sensing button is closed, aircraft current flight state reverts to floating state.
10. the motion sensing control handle of a kind of unmanned vehicle according to claim 9, it is characterised in that：When handle starts
During motion sensing control, handle at least occurs once to vibrate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611192558.XA CN106730900A (en) | 2016-12-21 | 2016-12-21 | The motion sensing control handle and its control method of a kind of unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611192558.XA CN106730900A (en) | 2016-12-21 | 2016-12-21 | The motion sensing control handle and its control method of a kind of unmanned vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN106730900A true CN106730900A (en) | 2017-05-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611192558.XA Withdrawn CN106730900A (en) | 2016-12-21 | 2016-12-21 | The motion sensing control handle and its control method of a kind of unmanned vehicle |
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| CN (1) | CN106730900A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107272724A (en) * | 2017-08-04 | 2017-10-20 | 南京华捷艾米软件科技有限公司 | A kind of body-sensing flight instruments and its control method |
| 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 |
-
2016
- 2016-12-21 CN CN201611192558.XA patent/CN106730900A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107272724A (en) * | 2017-08-04 | 2017-10-20 | 南京华捷艾米软件科技有限公司 | A kind of body-sensing flight instruments and its control method |
| 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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Application publication date: 20170531 |