CN106178537B - A kind of force feedback aircraft remote controler - Google Patents
A kind of force feedback aircraft remote controler Download PDFInfo
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- CN106178537B CN106178537B CN201610813131.0A CN201610813131A CN106178537B CN 106178537 B CN106178537 B CN 106178537B CN 201610813131 A CN201610813131 A CN 201610813131A CN 106178537 B CN106178537 B CN 106178537B
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- force feedback
- controller
- remote
- sensor
- select button
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- 230000003993 interaction Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
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- 238000005516 engineering process Methods 0.000 description 1
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- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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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
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- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Selective Calling Equipment (AREA)
Abstract
The invention discloses a kind of force feedback aircraft remote controlers, including remote controller body and internal computing device, the left and right sides of remote controller body be provided be shoulder strap shoulder strap hook, it is equipped with direction controller in the front of remote controller body, left Force Feedback Controller, display, loud speaker, right Force Feedback Controller, it is equipped with USB interface in the bottom of remote controller body, it is from left to right equipped with antenna successively in the front upper of remote controller body, select button one, select button two, select button three, power switch, by tilting remote controler, or operation Force Feedback Controller, the heading and speed of control aircraft can be facilitated according to the degree of force feedback.The configuration of the present invention is simple, it is easy to use, it 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, and in particular to a kind of force feedback aircraft remote controler is arrived, for flying
The straighforward operation of row device.
Background technology
Currently, the aircraft such as quadrotor drone the fields such as are travelled in national defense applications, agricultural plant protection, aerial images, toy
In occupy prodigious market, professional person or fan are keen to the manipulation experience of aircraft, and people not only require remote controler
It is easy to use, and require easy to learn, manipulation simply.The quick-fried manipulation except dangerous unmanned plane is torn open for some, is also required precisely controllable.
However, existing remote controler need to be improved in ease of use, learnability, accuracy etc. on the market, especially in people
The interactive aspect performance of machine is poor.These remote controlers still use aircraft professional person, and standard aircraft is liked
For person, for remote control experience property with regard to barely satisfactory, use is extremely inconvenient.
Invention content
Defect present in for the above-mentioned prior art, the technical problem to be solved by the present invention is to：Overcome the prior art it
Deficiency provides a kind of aircraft remote controler that can be easy to use, and compact-sized, button is few, easy to learn, can realize precisely
Manipulation, human-computer interaction are good.
The technical solution adopted by the present invention to solve the technical problems is：A kind of force feedback aircraft remote controler, including it is distant
Control device ontology and internal computing device, be provided in the left and right sides of remote controller body be shoulder strap shoulder strap hook, distant
The front for controlling device ontology is equipped with direction controller, left Force Feedback Controller, display, loud speaker, right Force Feedback Controller, distant
The bottom for controlling device ontology is equipped with USB interface, and antenna, select button are from left to right equipped with successively in the front upper of remote controller body
One, select button two, select button three, power switch, it is characterized in that：Twoth area of isloation state viewing area and image/video viewing area
The display of display is set to the positive Middle face of remote controller body, is internally provided with the gravitation ball that can move freely and force feedback sensing
The direction controller of device one is set to the top of display, and loud speaker is set to the lower section of display, in the shape and interior of shaking hands
The left side of display is set to equipped with the left Force Feedback Controller of force feedback sensor two, in the shape and built-in strong anti-of shaking hands
The right Force Feedback Controller of infeed sensor device three is set to the right of display.
Further, the left Force Feedback Controller, be additionally provided with spring-damper, Zuo Li inside right Force Feedback Controller
Feedback controller and right Force Feedback Controller can be slided up and down along remote controller body, and sliding distance is bigger, and resistance is bigger, when stopping
When sliding stop, left Force Feedback Controller and right Force Feedback Controller are kept in the center and are set.By sliding up and down left Force Feedback Controller
With right Force Feedback Controller, it is convenient to realize the combinative movements such as left and right turn, the acceleration and deceleration of aircraft or specific action.
Further, protective case lower face is also distinguished on the left Force Feedback Controller, right Force Feedback Controller
Equipped 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 senses
Device three can receive signal and its power and feed back to computing device, to judge that remote control is intended to.
Further, the direction controller is internally provided with a gravitation ball that can move freely in transparent coversheet,
It is equipped with gap between gravitation ball and transparent coversheet, the inner wall of transparent coversheet is provided with eight force feedback sensors one, is being remotely controlled
When device tilts, gravitation ball can collide on the force feedback sensor one of the direction according to inclined direction, and inclined degree is bigger, collision
More violent, internal calculation device can determine rapidly inclined direction.When aircraft grounds position or hovering, remote controler water
Flat, gravitation ball is in middle position；When needing flight forward, remote controler turns forward, and gravitation ball moves forwards, and collides
On the force feedback sensor one of the direction, according to inclined degree, the degree of collision is different, therefore the controllable preceding speed to flight
Degree and distance；Similarly, by remote controler backward, the directions such as left and right tilt, controllable aircraft backward, the directions flight such as left and right.
Further, one shape of select button is set as regular pentagon, and two shape of select button is set as positive three
Angular, the setting of three shape of select button is square.Select button one, select button two, select button three can as needed certainly
Row set-up function, button-shape is different, and user is facilitated to remember and use.
The beneficial effects of the invention are as follows：A kind of force feedback aircraft remote controler, compact-sized, button is few, letter
It is single easy to learn, can realize it is accurate manipulate, human-computer interaction is good, can be according to the use habit of people come into accommodating manipulation：In aircraft
Grounding position or when needing hovering, remote controler is horizontal, and gravitation ball is in middle position；When needing flight forward, remote controler is forward
It tilting, gravitation ball moves forwards, and collides on the force feedback sensor one of the direction, according to inclined degree, collision
Degree is different, therefore controllable preceding speed and distance to flight；Similarly, by remote controler backward, the directions such as left and right tilt, can
Manipulate aircraft backward, the directions such as left and right flight；It, can by sliding up and down left Force Feedback Controller and right Force Feedback Controller
Conveniently realize combinative movements or the specific actions such as left and right turn, the acceleration and deceleration of aircraft.Various compared with existing remote controler driving lever,
Button is complicated, find it difficult to learn it is difficult to control for, the present invention has that manipulation is easy, advantageous effect easy to learn and easy to use.
Description of the drawings
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the structural representation vertical view of the present invention.
Fig. 2 is the bottom 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 views of the present invention.
In figure：1- remote controller bodies；2- shoulder straps；3- direction controllers；The left Force Feedback Controllers of 4-；5- displays；6- is raised
Sound device；The right Force Feedback Controllers of 7-；8-USB interfaces；11- antennas；12- select buttons one；13- select buttons two；14- selections are pressed
Button three；15- power switches；16- shoulder straps are linked up with；31- transparent coversheets；32- gravitation balls；33- force feedbacks sensor one；The gaps 34-；
41- force feedbacks sensor two；The status display areas 51-；52- image/videos viewing area；71- force feedbacks sensor three.
Specific implementation mode
Presently in connection with attached drawing, the present invention is further illustrated.These attached drawings are simplified schematic diagram, only with signal
Mode illustrates the basic structure of the present invention, therefore it only shows the composition relevant to the invention.
As shown in Figure 1 and Figure 2, a kind of force feedback aircraft remote controler, including remote controller body 1 and internal computing device,
The left and right sides of remote controller body 1 be provided be shoulder strap 2 shoulder strap hook 16, the front of remote controller body 1 be equipped with side
To controller 3, left Force Feedback Controller 4, display 5, loud speaker 6, right Force Feedback Controller 7, in the bottom of remote controller body 1
Equipped with USB interface 8, it is from left to right equipped with antenna 11, select button 1, selection successively in the front upper of remote controller body 1
Button 2 13, select button 3 14, power switch 15, it is characterized in that：52 liang of isloation state viewing area 51 and image/video viewing area
The display 5 that area is shown is set to the positive Middle face of remote controller body 1, is internally provided with the gravitation ball 32 that can move freely and power is anti-
The direction controller 3 of infeed sensor device 1 is set to the top of display 5, and loud speaker 6 is set to the lower section of display 5, in holding
The left Force Feedback Controller 4 of hand shape and built-in force feedback sensor 2 41 is set to the left side of display 5, in shape of shaking hands
The right Force Feedback Controller 7 of shape and built-in force feedback sensor 3 71 is set to the right of display 5.Status display area 51
It can be divided into the upper and lower of display 5 or left and right with image/video viewing area 52.
As shown in Figure 1 and Figure 2, the left Force Feedback Controller 4, be additionally provided with spring damping inside right Force Feedback Controller 7
Device, left Force Feedback Controller 4 and right Force Feedback Controller 7 can be slided up and down along remote controller body 1, and sliding distance is bigger, resistance
Power is bigger, and when stopping sliding, left Force Feedback Controller 4 and right Force Feedback Controller 7 are kept in the center and set.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 movements such as left and right turn, the acceleration and deceleration of aircraft
Or specific action.
As shown in Figure 1 and Figure 2, the protective case lower face on the 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 4 of grip pressure, right Force Feedback Controller 7, force feedback sensing
Device 2 41, force feedback sensor 3 71 can receive signal and its power and feed back to computing device, to judge that remote control is intended to.
As shown in Figure 3, Figure 4, the direction controller 3 is internally provided with one in transparent coversheet 31 and can move freely
Gravitation ball 32 is equipped with gap 34, it is anti-that the inner wall of transparent coversheet 31 is provided with eight power between gravitation ball 32 and transparent coversheet 31
Infeed sensor device 1, when remote controler tilts, gravitation ball 32 can collide the force feedback sensor of the direction according to inclined direction
On one 33, inclined degree is bigger, and collision is more violent, and internal calculation device can determine rapidly inclined direction.Stop in aircraft
When flying position or hovering, remote controler is horizontal, and gravitation ball 32 is in middle position；When needing flight forward, remote controler turns forward,
Gravitation ball 32 moves forwards, and collides on the force feedback sensor 1 of the direction, according to inclined degree, the journey of collision
Degree is different, therefore controllable preceding speed and distance to flight；Similarly, by remote controler backward, the directions such as left and right tilt, can grasp
Control aircraft backward, the directions such as left and right flight.
As shown in Figure 1, one 12 shape of select button is set as regular pentagon, 2 13 shape of select button is set as
Equilateral triangle, the setting of 3 14 shape of select button are square.Select button 1, select button 2 13, select button 3 14
Sets itself function, button-shape difference user can be facilitated to remember and use as needed.
The present invention application method be：A kind of force feedback aircraft remote controler when in use carries on the back remote controler
Band hangs on people's shoulder, and remote controler should be at horizontal position in initial position, and both hands hold the right and left force feedback of remote controler
Controller.First, power supply, remote controler Power-On Self-Test and receiver are opened to code, communication, display can show various force feedbacks
The state of sensor, the state etc. of frequency range can send out the sound of " remote controler is ready " after success by loud speaker；Secondly, flying
Row device grounds position or when needing hovering, and remote controler is horizontal, and gravitation ball is in middle position；It is entire distant when needing flight forward
Control device turns forward, and gravitation ball moves forwards, and collides on the force feedback sensor one of the direction, according to inclined journey
Degree, the degree of collision is different, therefore the speed and distance of controllable flight forward, similarly, by remote controler backward, the side such as left and right
To inclination, controllable aircraft backward, the directions 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 the combinative movements such as left and right turn, the acceleration and deceleration of aircraft or specific action；Firmly the left power of grip pressure is anti-
Present controller, right Force Feedback Controller, force feedback sensor two, force feedback sensor three can receive signal and its power and anti-
It is fed to computing device, to judge that remote control is intended to.It is various compared with existing remote controler driving lever, button is complicated, find it difficult to learn it is difficult to control for,
The remote control method of the present invention matches with the various operations of people consciousness, therefore manipulates easy, easy to learn and easy to use.
The technical concepts and features of the above embodiment only to illustrate the invention, its object is to allow be familiar with technique
Personage can understand present disclosure and be implemented, and it is not intended to limit the scope of the present invention, all according to this hair
Equivalent change or modification made by bright Spirit Essence should all cover within the scope of the present invention.
Claims (5)
1. a kind of force feedback aircraft remote controler, including remote controller body（1）With internal computing device, in remote controller body
（1）Left and right sides to be provided be shoulder strap（2）Shoulder strap hook（16）, in remote controller body（1）Front equipped with direction control
Device processed（3）, left Force Feedback Controller（4）, display（5）, loud speaker（6）, right Force Feedback Controller（7）, in remote controller body
（1）Bottom be equipped with USB interface（8）, in remote controller body（1）Front upper from left to right successively be equipped with antenna（11）, choosing
Select button one（12）, select button two（13）, select button three（14）, power switch（15）, it is characterized in that：Isloation state viewing area
（51）With image/video viewing area（52）The display that twoth area are shown（5）It is set to remote controller body（1）Positive Middle face, it is interior
Portion is equipped with the gravitation ball that can move freely（32）With force feedback sensor one（33）Direction controller（3）It is set to display
（5）Top, loud speaker（6）It is set to display（5）Lower section, in shape and the built-in force feedback sensor two of shaking hands
（41）Left Force Feedback Controller（4）It is set to display（5）The left side, in shape and the built-in force feedback sensor of shaking hands
Three（71）Right Force Feedback Controller（7）It is set to display（5）The right.
2. a kind of force feedback aircraft remote controler according to claim 1, it is characterized in that：The left Force Feedback Controller
（4）, right Force Feedback Controller（7）Inside is additionally provided with spring-damper, left Force Feedback Controller（4）With right Force Feedback Controller
（7）It can be along remote controller body（1）It sliding up and down, sliding distance is bigger, and resistance is bigger, when stopping sliding, left force feedback control
Device processed（4）With right Force Feedback Controller（7）It keeps in the center and sets.
3. a kind of force feedback aircraft remote controler according to claim 1, it is characterized in that：In the left force-feedback control
Device（4）, right Force Feedback Controller（7）Upper protective case lower face further respectively has force feedback sensor two（41）, force feedback pass
Sensor three（71）, and force feedback sensor two（41）, force feedback sensor three（71）It can be arranged at one or at two or at three, use
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）It can receive signal and its power and feed back to computing device, to judge that remote control is intended to.
4. a kind of force feedback aircraft remote controler according to claim 1, it is characterized in that：The direction controller（3）
In transparent coversheet（31）It is internally provided with a gravitation ball that can move freely（32）, gravitation ball（32）And transparent coversheet（31）It
Between be equipped with gap（34）, in transparent coversheet（31）Inner wall be provided with eight force feedback sensors one（33）, tilted in remote controler
When, gravitation ball（32）The force feedback sensor one of the direction can be collided according to inclined direction（33）On, inclined degree is bigger, touches
Hit more violent, internal calculation device can determine rapidly inclined direction.
5. a kind of force feedback aircraft remote controler according to claim 1, it is characterized in that：The select button one（12）
Shape is set as regular pentagon, select button two（13）Shape is set as equilateral triangle, select button three（14）Shape is set as
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 |
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| Publication Number | Publication Date |
|---|---|
| CN106178537A CN106178537A (en) | 2016-12-07 |
| CN106178537B true CN106178537B (en) | 2018-09-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610813131.0A Active CN106178537B (en) | 2016-09-09 | 2016-09-09 | A kind of force feedback aircraft remote controler |
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Citations (4)
| 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 |
| 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 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7625287B2 (en) * | 2005-10-05 | 2009-12-01 | Nintendo Co., Ltd. | Driving game steering wheel simulation method and apparatus |
| US7793890B2 (en) * | 2007-01-31 | 2010-09-14 | Patrick L. Scherer | Control system for an aircraft |
-
2016
- 2016-09-09 CN CN201610813131.0A patent/CN106178537B/en active Active
Patent Citations (4)
| 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 |
| 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 |
|---|---|
| CN106178537A (en) | 2016-12-07 |
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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 |