CN106178537A - A kind of force feedback aircraft remote controller - Google Patents
A kind of force feedback aircraft remote controller Download PDFInfo
- Publication number
- CN106178537A CN106178537A CN201610813131.0A CN201610813131A CN106178537A CN 106178537 A CN106178537 A CN 106178537A CN 201610813131 A CN201610813131 A CN 201610813131A CN 106178537 A CN106178537 A CN 106178537A
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- China
- Prior art keywords
- force feedback
- remote controller
- controller
- select button
- sensor
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- 230000001133 acceleration Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
Abstract
The invention discloses a kind of force feedback aircraft remote controller, including remote controller body and internal calculating device, left and right sides at remote controller body be provided be braces braces hook, it is provided with direction controller in the front of remote controller body, left Force Feedback Controller, display, speaker, right Force Feedback Controller, it is provided with USB interface in the bottom of remote controller body, front upper at remote controller body is from left to right sequentially provided with antenna, select button one, select button two, select button three, on and off switch, by tilting remote controller, or operating physical force feedback controller, degree according to force feedback just can conveniently control heading and the speed of aircraft.Present configuration is simple, easy to use, can be widely applied to the convenient remote control of aircraft.
Description
Technical field
The present invention relates to aircraft field of remote-control unit, be specifically related to a kind of force feedback aircraft remote controller, for flying
The remote manipulation of row device.
Background technology
At present, the aircraft such as four rotor wing unmanned aerial vehicles the field such as is travelled at national defense applications, agricultural plant protection, aerial images, toy
In occupy the biggest market, professional person or fan hanker after aircraft manipulation experience, people not only require remote controller
Convenient use, and require easy to learn, manipulation is simple.Some are torn open quick-fried except the manipulation of danger unmanned plane, also require the most controlled.
But, the most existing remote controller need to improve, particularly people at aspects such as ease of use, learnability, accuracy
Machine interactive aspect poor-performing.These remote controllers still can use for aircraft professional person, likes for standard aircraft
For person, its remote control experience property is the most barely satisfactory, uses extremely inconvenience.
Summary of the invention
For defect present in above-mentioned prior art, the technical problem to be solved in the present invention is: overcome prior art it
Not enough, it is provided that a kind of aircraft remote controller that can conveniently use, its compact conformation, button is few, easy to learn, can realize precisely
Manipulation, human-computer interaction is good.
The technical solution adopted for the present invention to solve the technical problems is: a kind of force feedback aircraft remote controller, including distant
Control device body and internal calculating device, it is the braces hook of braces that the left and right sides at remote controller body are provided with, distant
The front of control device body is provided with direction controller, left Force Feedback Controller, display, speaker, right Force Feedback Controller, distant
The bottom of control device body is provided with USB interface, and the front upper at remote controller body is from left to right sequentially provided with antenna, select button
One, select button two, select button three, on and off switch, is characterized in that: point status display area and image/video viewing area two district
The display of display is arranged at the positive Middle face of remote controller body, and inside is provided with the gravitation ball that can move freely and force feedback sensing
The direction controller of device one is arranged at the top of display, and speaker is arranged at the lower section of display, in shaking hands shape and interior
Left Force Feedback Controller equipped with force feedback sensor two is arranged at the left side of display, in shaking hands shape and built-in strong anti-
The right Force Feedback Controller of infeed sensor device three is arranged at the right of display.
Further, it is additionally provided with spring-damper, Zuo Li inside described left Force Feedback Controller, right Force Feedback Controller
Feedback controller and right Force Feedback Controller all can slide up and down along remote controller body, and sliding distance is the biggest, and resistance is the biggest, when stopping
During sliding stop, left Force Feedback Controller and right Force Feedback Controller are kept in the center and are put.By sliding up and down left Force Feedback Controller
With right Force Feedback Controller, it is convenient to realize combinative movement or the specific actions such as the left and right turn of aircraft, acceleration and deceleration.
Further, on described left Force Feedback Controller, right Force Feedback Controller, protection set lower face is also distinguished
It is provided with force feedback sensor two, force feedback sensor three, and force feedback sensor two, force feedback sensor three can be arranged at one
Or at two or at three, the firmly left Force Feedback Controller of grip pressure, right Force Feedback Controller, force feedback sensor two, force feedback sensing
Device three can receive signal and power thereof and feed back to calculate device, thus judges that remote control is intended to.
Further, described direction controller is internally provided with a gravitation ball that can move freely in transparent coversheet,
Being provided with space between gravitation ball and transparent coversheet, the inwall in transparent coversheet is provided with eight force feedback sensors one, in remote control
When device tilts, gravitation ball can collide on the force feedback sensor one of the direction according to incline direction, and inclined degree is the biggest, collision
The most violent, internal calculation device just can determine rapidly incline direction.When aircraft grounding position or hovering, remote controller water
Flat, gravitation ball is in middle position；When needs flight forward, remote controller turns forward, and gravitation ball forwards moves, and collides
On the force feedback sensor one of the direction, according to the degree tilted, the degree of collision is different, therefore can control the speed of forward direction flight
Degree and distance；In like manner, by remote controller backward, the direction such as left and right tilt, controllable aircraft backward, the direction flight such as left and right.
Further, described select button one profile is set to regular pentagon, and select button two profile is set to positive three
Dihedral, select button three profile is set to square.Select button one, select button two, select button three can as required certainly
Row set-up function, its button-shape is different, facilitates user to remember and uses.
The invention has the beneficial effects as follows: described a kind of force feedback aircraft remote controller, its compact conformation, button is few, letter
Single easy to learn, precisely manipulation can be realized, human-computer interaction is good, conveniently can manipulate according to the use habit of people: at aircraft
The grounding position or need hovering time, remote controller level, gravitation ball is in middle position；When needs flight forward, remote controller is forward
Tilting, gravitation ball forwards moves, and collides on the force feedback sensor one of the direction, according to the degree tilted, collision
Degree is different, therefore can control speed and the distance of forward direction flight；In like manner, by remote controller backward, the direction such as left and right tilt, can
Manipulation aircraft backward, the direction such as left and right flight；By sliding up and down left Force Feedback Controller and right Force Feedback Controller, can
Conveniently realize combinative movement or the specific actions such as the left and right turn of aircraft, acceleration and deceleration.Various compared with existing remote controller driving lever,
For button complexity, the difficult control that finds it difficult to learn, the present invention has the beneficial effect that manipulation is easy, easy to learn and easy to use.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the structural representation top view of the present invention.
Fig. 2 is the polycrystalline substance schematic diagram of the present invention.
Fig. 3 is the direction controller structure enlarged diagram of the present invention.
Fig. 4 is the direction controller P-P cross-sectional view of the present invention.
In figure: 1-remote controller body；2-braces；3-direction controller；The left Force Feedback Controller of 4-；5-display；6-raises
Sound device；The right Force Feedback Controller of 7-；8-USB interface；11-antenna；12-select button one；13-select button two；14-selects to press
Button three；15-on and off switch；16-braces is linked up with；31-transparent coversheet；32-gravitation ball；33-force feedback sensor one；34-space；
41-force feedback sensor two；51-status display area；52-image/video viewing area；71-force feedback sensor three.
Detailed description of the invention
Presently in connection with accompanying drawing, the present invention is further illustrated.These accompanying drawings are the schematic diagram of simplification, only with signal
Mode illustrates the basic structure of the present invention, and therefore it only shows the composition relevant with the present invention.
As shown in Figure 1 and Figure 2, a kind of force feedback aircraft remote controller, including remote controller body 1 and internal calculating device,
Left and right sides at remote controller body 1 be provided be braces 2 braces hook 16, in the front side of being provided with of remote controller body 1
To controller 3, left Force Feedback Controller 4, display 5, speaker 6, right Force Feedback Controller 7, in the bottom of remote controller body 1
Being provided with USB interface 8, the front upper at remote controller body 1 is from left to right sequentially provided with antenna 11, select button 1, selects
Button 2 13, select button 3 14, on and off switch 15, is characterized in that: point status display area 51 and 52 liang, image/video viewing area
The display 5 that district shows is arranged at the positive Middle face of remote controller body 1, and inside is provided with the gravitation ball 32 that can move freely and power is anti-
The direction controller 3 of infeed sensor device 1 is arranged at the top of display 5, and speaker 6 is arranged at the lower section of display 5, in holding
Hand shape and the left Force Feedback Controller 4 built with force feedback sensor 2 41 are arranged at the left side of display 5, in shape of shaking hands
Shape and the right Force Feedback Controller 7 built with force feedback sensor 3 71 are arranged at the right of display 5.Status display area 51
With image/video viewing area 52 can be divided into display 5 up and down or left and right.
As shown in Figure 1 and Figure 2, described left Force Feedback Controller 4, right Force Feedback Controller 7 inside are additionally provided with spring damping
Device, left Force Feedback Controller 4 and right Force Feedback Controller 7 all can slide up and down along remote controller body 1, and sliding distance is the biggest, resistance
Power is the biggest, and when stopping sliding, left Force Feedback Controller 4 and right Force Feedback Controller 7 are kept in the center and put.By sliding up and down a left side
Force Feedback Controller 4 and right Force Feedback Controller 7, it is convenient to realize the combinative movement such as the left and right turn of aircraft, acceleration and deceleration
Or specific action.
As shown in Figure 1 and Figure 2, protection set lower face on described left Force Feedback Controller 4, right Force Feedback Controller 7
Further respectively have force feedback sensor 2 41, force feedback sensor 3 71, and force feedback sensor 2 41, force feedback sensor
3 71 can be arranged at one or at two or at three, firmly the left Force Feedback Controller of grip pressure 4, right Force Feedback Controller 7, and force feedback senses
Device 2 41, force feedback sensor 3 71 can receive signal and power thereof and feed back to calculate device, thus judges that remote control is intended to.
As shown in Figure 3, Figure 4, described direction controller 3 is internally provided with one in transparent coversheet 31 and can move freely
Gravitation ball 32, is provided with space 34 between gravitation ball 32 and transparent coversheet 31, it is anti-that the inwall in transparent coversheet 31 is provided with eight power
Infeed sensor device 1, when remote controller tilts, gravitation ball 32 can collide the force feedback sensor of the direction according to incline direction
On one 33, inclined degree is the biggest, collides the most violent, and internal calculation device just can determine rapidly incline direction.Stop at aircraft
When flying position or hovering, remote controller level, gravitation ball 32 is in middle position；When needs flight forward, remote controller turns forward,
Gravitation ball 32 forwards moves, and collides on the force feedback sensor 1 of the direction, according to the degree tilted, the journey of collision
Degree difference, therefore can control speed and the distance of forward direction flight；In like manner, by remote controller backward, the direction such as left and right tilt, can grasp
Control aircraft backward, the direction such as left and right flight.
As it is shown in figure 1, described select button 1 profile is set to regular pentagon, select button 2 13 profile is set to
Equilateral triangle, select button 3 14 profile is set to square.Select button 1, select button 2 13, select button 3 14
Can sets itself function as required, its button-shape is different, facilitates user to remember and uses.
The using method of the present invention is: described a kind of force feedback aircraft remote controller, in use, is carried on the back by remote controller
Band hangs on people's shoulder, and remote controller should be at horizontal level at initial position, and both hands hold the right and left force feedback of remote controller
Controller.First, power-on, remote controller Power-On Self-Test, and receptor can show various force feedback to code, communication, display
The state of sensor, the state etc. of frequency range, after success, the sound of " remote controller is ready " can be sent by speaker；Secondly, flying
Row device the grounding position or need hovering time, remote controller level, gravitation ball is in middle position；When needs flight forward, whole distant
Control device turns forward, and gravitation ball forwards moves, and collides on the force feedback sensor one of the direction, according to the journey tilted
Degree, the degree of collision is different, therefore can control speed and the distance of flight forward, in like manner, by remote controller backward, the side such as left and right
To inclination, controllable aircraft backward, the direction such as left and right flight；By sliding up and down left Force Feedback Controller and right force feedback
Controller, it is convenient to realize combinative movement or the specific actions such as the left and right turn of aircraft, acceleration and deceleration；Firmly the left power of grip pressure is anti-
Feedback controller, right Force Feedback Controller, force feedback sensor two, force feedback sensor three can receive signal and strong and weak and anti-
It is fed to calculate device, thus judges that remote control is intended to.Various compared with existing remote controller driving lever, button is complicated, for the difficult control that finds it difficult to learn,
The remote control method of the present invention matches with the various operation consciousness of people, therefore manipulates simplicity, easy to learn and easy to use.
Above-mentioned embodiment only for technology design and the feature of the present invention are described, its object is to allow and is familiar with technique
Personage will appreciate that present disclosure and is carried out, and can not limit the scope of the invention with this, all according to this
The equivalence that bright spirit is made changes or modifies, and all should contain within the scope of the present invention.
Claims (5)
1. a force feedback aircraft remote controller, including remote controller body (1) and internal calculating device, at remote controller body
(1) left and right sides be provided be braces (2) braces hook (16), be provided with in the front of remote controller body (1) direction control
Device processed (3), left Force Feedback Controller (4), display (5), speaker (6), right Force Feedback Controller (7), at remote controller body
(1) bottom is provided with USB interface (8), and the front upper at remote controller body (1) is from left to right sequentially provided with antenna (11), choosing
Select button one (12), select button two (13), select button three (14), on and off switch (15), it is characterized in that: point status display area
(51) and the display (5) that shows of image/video viewing area (52) two district is arranged at the positive Middle face of remote controller body (1), interior
Portion is provided with the direction controller (3) of gravitation ball (32) and the force feedback sensor one (33) that can move freely and is arranged at display
(5) top, speaker (6) is arranged at the lower section of display (5), in shaking hands shape and built with force feedback sensor two
(41) left Force Feedback Controller (4) is arranged at the left side of display (5), in shaking hands shape and built with force feedback sensor
The right Force Feedback Controller (7) of three (71) is arranged at the right of display (5).
A kind of force feedback aircraft remote controller the most according to claim 1, is characterized in that: described left Force Feedback Controller
(4), right Force Feedback Controller (7) is internal is additionally provided with spring-damper, left Force Feedback Controller (4) and right Force Feedback Controller
(7) all can slide up and down along remote controller body (1), sliding distance is the biggest, and resistance is the biggest, when stopping sliding, and left force feedback control
Device processed (4) and right Force Feedback Controller (7) are kept in the center and are put.
A kind of force feedback aircraft remote controller the most according to claim 1, is characterized in that: at described left force-feedback control
Device (4), right Force Feedback Controller (7) upper protection set lower face further respectively has force feedback sensor two (41), force feedback passes
Sensor three (71), and force feedback sensor two (41), force feedback sensor three (71) can arrange at one or at two or at three, uses
The left Force Feedback Controller of power grip pressure (4), right Force Feedback Controller (7), force feedback sensor two (41), force feedback sensor three
(71) signal and power thereof can be received and feed back to calculate device, thus judging that remote control is intended to.
A kind of force feedback aircraft remote controller the most according to claim 1, is characterized in that: described direction controller (3)
Transparent coversheet (31) be internally provided with a gravitation ball that can move freely (32), gravitation ball (32) and transparent coversheet (31) it
Between be provided with space (34), the inwall in transparent coversheet (31) is provided with eight force feedback sensors one (33), remote controller tilt
Time, gravitation ball (32) can collide on the force feedback sensor one (33) of the direction according to incline direction, and inclined degree is the biggest, touches
Hitting the most violent, internal calculation device just can determine rapidly incline direction.
A kind of force feedback aircraft remote controller the most according to claim 1, is characterized in that: described select button one (12)
Profile is set to regular pentagon, and select button two (13) profile is set to equilateral triangle, and select button three (14) profile is set to
Square.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610813131.0A CN106178537B (en) | 2016-09-09 | 2016-09-09 | A kind of force feedback aircraft remote controler |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610813131.0A CN106178537B (en) | 2016-09-09 | 2016-09-09 | A kind of force feedback aircraft remote controler |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106178537A true CN106178537A (en) | 2016-12-07 |
| CN106178537B CN106178537B (en) | 2018-09-25 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610813131.0A Active CN106178537B (en) | 2016-09-09 | 2016-09-09 | A kind of force feedback aircraft remote controler |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1531913A (en) * | 2003-03-26 | 2004-09-29 | 韩国科学技术院 | Wheel chair control sensor controlled by shoulder movement and wheel chair controller |
| US20080180272A1 (en) * | 2007-01-31 | 2008-07-31 | Scherer Patrick L | Control System for an Aircraft |
| CN101815561A (en) * | 2007-07-02 | 2010-08-25 | 雷泽亚太有限公司 | Game controller with clickable trackball |
| CN102375581A (en) * | 2010-08-11 | 2012-03-14 | 深圳富泰宏精密工业有限公司 | Touch type electronic device and method for improving touch accuracy of touch type electronic device |
| US20140004946A1 (en) * | 2005-10-05 | 2014-01-02 | Nintendo Co., Ltd. | Game object control using pointing inputs to rotate a displayed virtual object control device |
| CN206027091U (en) * | 2016-09-09 | 2017-03-22 | 西安航空学院 | Force feedback aircraft remote controller |
-
2016
- 2016-09-09 CN CN201610813131.0A patent/CN106178537B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1531913A (en) * | 2003-03-26 | 2004-09-29 | 韩国科学技术院 | Wheel chair control sensor controlled by shoulder movement and wheel chair controller |
| US20140004946A1 (en) * | 2005-10-05 | 2014-01-02 | Nintendo Co., Ltd. | Game object control using pointing inputs to rotate a displayed virtual object control device |
| US20080180272A1 (en) * | 2007-01-31 | 2008-07-31 | Scherer Patrick L | Control System for an Aircraft |
| CN101815561A (en) * | 2007-07-02 | 2010-08-25 | 雷泽亚太有限公司 | Game controller with clickable trackball |
| CN102375581A (en) * | 2010-08-11 | 2012-03-14 | 深圳富泰宏精密工业有限公司 | Touch type electronic device and method for improving touch accuracy of touch type electronic device |
| CN206027091U (en) * | 2016-09-09 | 2017-03-22 | 西安航空学院 | Force feedback aircraft remote controller |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106178537B (en) | 2018-09-25 |
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Effective date of registration: 20230925 Address after: 710000 B2-216, 7th Floor, Xixian Talent Building, Century Building, Fengdong New City, Xi'an City, Shaanxi Province Patentee after: Xi'an Chenzhen Zhishan Information Technology Co.,Ltd. Address before: 710077 No. 259, West Second Ring Road, Lianhu District, Xi'an, Shaanxi Patentee before: XI'AN AERONAUTICAL University |