CN103721422B - A kind of model airplane remote control handle that can realize attitude and automatically control - Google Patents
A kind of model airplane remote control handle that can realize attitude and automatically control Download PDFInfo
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- CN103721422B CN103721422B CN201310701417.6A CN201310701417A CN103721422B CN 103721422 B CN103721422 B CN 103721422B CN 201310701417 A CN201310701417 A CN 201310701417A CN 103721422 B CN103721422 B CN 103721422B
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- rocking bar
- bar frame
- control handle
- model airplane
- control
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Abstract
The invention discloses a kind of model airplane remote control handle that can realize attitude and automatically control, comprise support, rocking bar frame and antenna, it is characterized in that: support and rocking bar frame are connected as a single entity, and rounding off, be provided with rocking bar locator on rocking bar frame top, middle part is provided with button in enable time, inertial posture measuring sensor and clutch is provided with in rocking bar frame, be connected with rocking bar locator, inertial posture measuring sensor also with receiving terminal wireless connections, support is provided with switching channels and usb communication port.Handle arrangement of the present invention is tight, exquisite appearance, and one-hand operation, to the control of pitching, roll, direction, throttle four passages or more passage, holds easy operation control; Can realize a key and return middle function, the output controlled quentity controlled variable of recovery pitching, roll two passages is neutral value, then using remote-control handle current pose as benchmark, realizes the stable output of gesture stability; Can realize the switching of gesture stability and non-gesture stability, multiple remote-control handle direct channel exports, and can be widely used in model airplane remote controller or current game remote control.
Description
Technical field
The present invention relates to remote controller, specifically a kind of model airplane remote control handle that can realize attitude and automatically control.
Background technology
The fast development of World Economics, more and more people is engaged in the unmanned plane industry relevant with model plane, becomes a kind of trend gradually.Under the present circumstances, more and more higher to the remote control request of unmanned plane and model plane, therefore technology is also in continuous update.
Existing unmanned controller or model airplane remote controller have four key technologies to need to solve: 1, gyroscope is with the problem of temperature drift; 2, attitude algorithm stability; 3, gyro sensitivity adjustment; 4, acceleration transducer proportionality coefficient adjustment.Often because above-mentioned four technology are not resolved, to such an extent as to control accuracy does not reach flight control effects, easily causes various aircraft accident, is unfavorable for very much the real-time control of flying yet.
Summary of the invention
The object of the invention is for overcoming prior art deficiency, and a kind of model airplane remote control handle that can realize attitude and automatically control is provided.The model airplane remote control handle arrangement of this structure is tight, easy operation control.
The technical scheme realizing the object of the invention is:
A kind of model airplane remote control handle that can realize attitude and automatically control, comprise support, rocking bar frame and antenna, unlike the prior art: support and rocking bar frame are connected as a single entity, and rounding off, rocking bar locator is provided with on rocking bar frame top, middle part is provided with button in enable time, the inertial posture measuring sensor and clutch that are connected with rocking bar locator is provided with in rocking bar frame, inertial posture measuring sensor also with receiving terminal wireless connections, support is provided with switching channels and usb communication port, and frame bottom is provided with charge port.
The first stop position, the second stop position and the 3rd stop position that finger stop position when to hold handle with people is corresponding is provided with inside described rocking bar frame, in enable time, button is arranged on the second stop position of rocking bar frame, and in enable time, button is connected with the second stop position of rocking bar frame by spring.
Described rocking bar locator is mushroom head knob rocking bar locator, is prior art.
Described handle is gun shaped or sector structure.
Described switching channels is 2 sections of switching channels, 3 sections of switching channels or knob switch passage.
Described inertial posture measuring sensor is made up of central microprocessor (CPU), attitude transducer, position sensor and user interface, attitude transducer, position sensor, user interface are connected with central microprocessor respectively, for prior art, on the books in Chinese patent CN201561759U.
The present invention is according to the characteristic of inertial posture measuring sensor, this sensor is carried out to the adjustment of acceleration transducer proportionality coefficient and gyro sensitivity parameter, and in the CPU inner parameter according to adjustment, self adaptation dynamic compensation is realized to attitude transducer, the rocker regulation resistance that horizontally slips controls about realizing direction, in controlling to make direction controlling return about unclamping, promote rocker regulation resistance up and down and then realize throttle signal collection.
The use procedure of remote-control handle of the present invention is:
1, user holds remote-control handle, middle finger is for controlling button in enable time, when button is pressed, by the gesture stability of opening remote control handle, with current pose as a reference, just provide the controlled quentity controlled variable of roll left/right when remote-control handle "Left"-deviationist/Right deviation, come back when remote-control handle or when bowing, then provide controlled quentity controlled variable up or down;
2, the thumb of user is for controlling mushroom head knob rocking bar, can realize the control to throttle when pinning mushroom head knob rocking bar up and down during direction, realizes the control to direction to left and right Shi Zeke;
3, with forefinger gauge tap passage, the output of through connect signal is realized.
Advantage of the present invention is:
1, close structure, exquisite appearance, one-hand operation, to the control of pitching, roll, direction, throttle four passages or more passage, holds easy operation control;
2, can realize a key and return middle function, the output controlled quentity controlled variable of recovery pitching, roll two passages is neutral value, then using remote-control handle current pose as benchmark, realizes the stable output of gesture stability;
3, can realize the switching of gesture stability and non-gesture stability, multiple remote-control handle direct channel exports, and can be widely used in model airplane remote controller or current game remote control.
Accompanying drawing explanation
Fig. 1 is the structural representation of model airplane remote control handle of the present invention;
Fig. 2 is fundamental diagram of the present invention.
In figure: 1. button 8. battery charging port in enable time of support 2. rocking bar frame 3. mushroom head knob rocking bar 4. antenna 5.USB COM1 6.3 sections of switching channels 7..
Detailed description of the invention
With reference to Fig. 1, a kind of model airplane remote control handle that can realize attitude and automatically control of the present invention, by support 1, rocking bar frame 2, mushroom head knob rocking bar 3, inertial posture measuring sensor, clutch, antenna 4, usb communication port 5, switching channels 6, in enable time, button 7 and battery charging port 8 form, support 1 and rocking bar frame 2 are connected as a single entity, and rounding off, in gun shaped structure, mushroom head knob rocking bar 3 is arranged on rocking bar frame 2 top, and be connected with the inertial posture measuring sensor be arranged in rocking bar frame 2, inertial posture measuring sensor and receiving terminal wireless connections, when mushroom head knob rocking bar 3 swings, inertial posture measuring sensor perception will go out the pitching of rocking bar frame 2 at that time and the angle of roll, the first stop position that finger stop position when to hold handle with people is corresponding is provided with inside rocking bar frame 2, second stop position and the 3rd stop position, enable attitude is had to shake control effect at the 3rd stop position, in enable time, button 7 is connected with the second stop position of rocking bar frame 7 by spring, user can realize attitude data and exports the respective channel signal of the receiving terminal of remote-control handle by fastening button 7 in enable time, unclamp button 7 in enable time and automatically restore to neutral value state.Be connected by spring between button 7 with rocking bar frame 2 in enable time, control by spring the large low-force that user fastens button 7 pairs of rocking bar framves in enable time.Clutch is arranged in rocking bar frame 2 and is connected with mushroom head knob rocking bar, and produce suitable resistance when this rocking bar is stirred in left and right, support 1 is provided with 3 sections of switching channels 6, antenna 4 and usb communication port 5, and battery charging port 8 is arranged on bottom support 1.
With reference to Fig. 2, operation principle of the present invention is: the attitude data that inertial posture measuring sensor transmits by CPU mono-aspect carries out data fusion and attitude algorithm, the pitching in attitude data and roll is exported as remote signal, receive the aileron that mushroom head knob rocker regulation resistance transmits on the other hand, lifting, throttle, direction and the magnitude of voltage on other accessory channels, and sample in CPU inside, analog-to-digital conversion (analog-to-digital conversion module utilizing CPU inside to carry is changed) and filtering, wherein filtering algorithm removes maximum and the sliding window filtering of minimum of a value, transmitted by 2.4G wireless data transmission module, by aileron, lifting, throttle, the analog signal of direction and other accessory channels converts data signal to, and convert remote signal to, also can be connected with computer by USB data line, realize on-line communication, the transmission protocol data of PWM wave control signal and customization that the agreement of transmission is carried out the standard that converts to by receiving terminal exports.
Claims (4)
1. the model airplane remote control handle that can realize attitude and automatically control, comprise support, rocking bar frame and antenna, it is characterized in that: support and rocking bar frame are connected as a single entity, and rounding off, be provided with rocking bar locator on rocking bar frame top, middle part is provided with button in enable time, inertial posture measuring sensor and clutch is provided with in rocking bar frame, be connected with rocking bar locator, inertial posture measuring sensor also with receiving terminal wireless connections, support is provided with switching channels and usb communication port;
Be provided with the first stop position, the second stop position and the 3rd stop position that finger stop position when to hold handle with people is corresponding inside described rocking bar frame, in enable time, button is connected with the second stop position of rocking bar frame by spring.
2. model airplane remote control handle according to claim 1, is characterized in that: described rocking bar locator is mushroom head knob rocking bar locator.
3. model airplane remote control handle according to claim 1, is characterized in that: described handle is gun shaped or sector structure.
4. model airplane remote control handle according to claim 1, is characterized in that: described switching channels is 2 sections of switching channels, 3 sections of switching channels or knob switch passage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310701417.6A CN103721422B (en) | 2013-12-19 | 2013-12-19 | A kind of model airplane remote control handle that can realize attitude and automatically control |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310701417.6A CN103721422B (en) | 2013-12-19 | 2013-12-19 | A kind of model airplane remote control handle that can realize attitude and automatically control |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103721422A CN103721422A (en) | 2014-04-16 |
| CN103721422B true CN103721422B (en) | 2016-03-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201310701417.6A Active CN103721422B (en) | 2013-12-19 | 2013-12-19 | A kind of model airplane remote control handle that can realize attitude and automatically control |
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| CN (1) | CN103721422B (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016086346A1 (en) | 2014-12-02 | 2016-06-09 | 深圳市大疆创新科技有限公司 | Shifter lever structure and remote controller adopting same |
| CN105788225A (en) * | 2016-03-04 | 2016-07-20 | 铱格斯曼航空科技集团有限公司 | System for converting remote control unit signals into 232 signals |
| US10133271B2 (en) * | 2016-03-25 | 2018-11-20 | Qualcomm Incorporated | Multi-axis controlller |
| CN106155046A (en) * | 2016-06-17 | 2016-11-23 | 深圳市元征科技股份有限公司 | Rocker assembly, remote control unit and flight system |
| CN110465075B (en) * | 2016-12-30 | 2023-04-28 | 大连大学 | Handle rocker system for implementing method for acquiring rocker position based on sensor mpu6050 acquisition signal |
| CN107705530A (en) * | 2017-10-10 | 2018-02-16 | 深圳市前海深蕾技术服务有限公司 | A kind of general remote controller device |
| CN110764629B (en) * | 2018-07-10 | 2023-10-20 | 杭州海康威视数字技术股份有限公司 | Method and device for managing rocker status |
| CN108888970B (en) * | 2018-09-18 | 2023-10-27 | 高岩 | Fixed wing model aeroplane and model ship convenient to take off and land training |
| CN109326112A (en) * | 2018-11-19 | 2019-02-12 | 广州极飞科技有限公司 | A kind of aircraft remote control device and remote control method |
| CN112800571A (en) * | 2019-11-14 | 2021-05-14 | 广州极飞科技股份有限公司 | Rocker centering dead zone determining method, rocker centering determining method and related device |
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| WO2013095391A1 (en) * | 2011-12-20 | 2013-06-27 | Regal Elite, Inc. | Controller for an external device |
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| JPH10192559A (en) * | 1997-01-14 | 1998-07-28 | Touno:Kk | Radio control apparatus for model plane |
| US7374489B2 (en) * | 2003-05-28 | 2008-05-20 | Charles Sexton | Steering wheel adapted for connection to finger dial of RC control unit |
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| CN2416935Y (en) * | 2000-04-11 | 2001-01-31 | 魏孟余 | Rocking rod |
| CN201561759U (en) * | 2009-10-18 | 2010-08-25 | 魏承赟 | Inertial attitude and azimuth measuring device |
| CN102380216A (en) * | 2011-10-10 | 2012-03-21 | 汕头市博意玩具有限公司 | Method for remotely controlling toy plane and swing remote controller |
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| CN103721422A (en) | 2014-04-16 |
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Address after: 541004, Guilin, the Guangxi Zhuang Autonomous Region, Seven Star Road, Chaoyang Road, information industry park D-12, Guilin electricity supplier Valley B block 3 Building Patentee after: Guilin Feiyu Polytron Technologies Inc Address before: 541004 the Guangxi Zhuang Autonomous Region Guilin Qixing District Chaoyang Road Information Industrial Park Yu technology building four floor tejet Feiyu Technology Patentee before: Guilin Feiyu Electronic Technology Co.,Ltd. |