CN104274982A - Model airplane remote controller - Google Patents
Model airplane remote controller Download PDFInfo
- Publication number
- CN104274982A CN104274982A CN201410535869.6A CN201410535869A CN104274982A CN 104274982 A CN104274982 A CN 104274982A CN 201410535869 A CN201410535869 A CN 201410535869A CN 104274982 A CN104274982 A CN 104274982A
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- China
- Prior art keywords
- remote controller
- control
- circuit
- potentiometer
- lift
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Abstract
The invention relates to a model airplane remote controller which mainly structurally comprises a remote controller control box, a lifting force control rocker, a direction control handle, a power switch, a circuit board, a direct-current power supply, a lifting force control potentiometer, a direction control potentiometer, a wireless transmitting antenna, a power indicator lamp and a control panel. The model airplane remote controller has the advantages the remote controller adopts microcomputer control and a design combining machinery and electronics, the remote controller is advanced in design, compact in structure, reasonable in configuration, convenient to mount and use, and safe, stable and reliable, programming and automation of the remote controller are achieved, the flying, recycling and controlling of a model airplane can be completely simply, accurately and fast, and the remote controller is quite ideal.
Description
Technical field
The present invention relates to a kind of model aeroplane remote controller, be specifically related to the technical field of model airplane operation Control and Application.
Background technology
Model airplane aircraft is a kind of sci-tech product of simulated flight, is again a kind of intelligent toy, and remote controller is then the important component part of model airplane aircraft, for controlling the release of aircraft, recovery and flare maneuver, is very important.
At present, model aeroplane remote controller is mostly hand-held, be made up of end box, function button, antenna, lift rocking bar and direction rocking bar, various function is completed with mechanical structure and rocking bar, in use need to hold box at the bottom of remote controller, two hands manipulate plug-type lift rocking bar and direction rocking bar respectively, control lifting, the rotation of model airplane and all around fly, the control mode complex operation that this plug-type rocking bar combines mutually, inaccurate, not easily left-hand seat, operating difficulties during emergency, very easily meet accident, be difficult to meet instructions for use.
Summary of the invention
Goal of the invention
Goal of the invention of the present invention is situation for background technology and deficiency, the design that employing machinery, electronics combine, design the model aeroplane remote controller that a kind of microcomputer controls, make model aeroplane remote controller realize automation, sequencing, with simple and easy, complete the letting fly away of model airplane accurately and quickly, regain and control action.
Technical scheme
Primary structure of the present invention comprises: remote controller control box, lift control rocking bar, direction control handle, power switch, circuit board, dc source, lift control potentiometer, direction controlling potentiometer, wireless transmission antenna, power supply indicator, control panel;
Remote controller control box is rectangle, is control panel, arranges lift control rocking bar, direction control handle, power switch, wireless transmission antenna, power supply indicator on the control panel on the top of remote controller control box; In remote controller control box, centre position is provided with circuit board, is control circuit on circuit boards; Be provided with lift control potentiometer at the upper left quarter of the top inner wall of remote controller control box, lift control potentiometer is connected with the lift control rocking bar on control panel; Be provided with direction controlling potentiometer at the upper right quarter of the top inner wall of remote controller control box, direction controlling potentiometer is connected with the direction control handle on control panel.
Described control circuit, integrated circuit is formed by microcomputer control circuit IC1, the first oscillating crystal IC circuit 2, wireless communication module IC circuit 3, potentiometer array circuit IC4, the second oscillating crystal IC circuit 5, connected by wire between each circuit, VSS end is earth terminal, + 5V end is power end, and ANTEN end is wireless transmission antenna end.
The chip that described microcomputer control circuit IC1 uses is 32 one-chip computers.
Beneficial effect
The present invention has obvious advance compared with background technology, it is the handling characteristics for model aeroplane remote controller, the design that employing machinery, electronics combine, it is the model aeroplane remote controller that a kind of microcomputer controls, this remote controller advanced design, compact conformation, configuration are reasonable, easy to install, safety and stability is reliable, model aeroplane remote controller is made to achieve sequencing, automation, can complete the letting fly away of model airplane simple and easy, accurately and quickly, regain and control action, be very good model aeroplane remote controller.
Accompanying drawing explanation
Fig. 1 is model aeroplane remote controller overall structure figure
Fig. 2 is the A-A profile of Fig. 1
Fig. 3 is circuit board control circuit figure
Shown in figure, list of numerals is as follows:
1, remote controller control box, 2, lift control rocking bar, 3, direction control handle, 4, power switch, 5, circuit board, 6, dc source, 7, lift control potentiometer, 8, direction controlling potentiometer, 9, wireless transmission antenna, 10, power supply indicator, 11, control panel.
IC1, microcomputer control circuit, IC2, the first oscillating crystal circuit, IC3, wireless communication module circuit, IC4, potentiometer array circuit, IC5, the second oscillating crystal circuit.
R, resistor, C, capacitor, X, oscillating crystal, L, inductor, VSS, earth terminal ,+5V, dc source, ANTEN, wireless transmission antenna end.
Detailed description of the invention
Below in conjunction with accompanying drawing, the present invention will be further described:
Shown in Fig. 1,2, be model aeroplane remote controller overall structure figure, each position, annexation want correct, install firmly.
Remote controller control box is rectangle, is control panel 11, control panel 11 arranges lift control rocking bar 2, direction control handle 3, power switch 4, wireless transmission antenna 9, power supply indicator 10 on the top of remote controller control box 1; The position at the middle part in remote controller control box 1 is provided with circuit board 5, circuit board 5 is control circuit; Be provided with lift control potentiometer 7 at the top inner wall upper left quarter of remote controller control box 1, lift control potentiometer 7 is connected with the lift control rocking bar 2 on control panel 11; Be provided with direction controlling potentiometer 8 at the inwall upper right quarter of remote controller control box 1, direction controlling potentiometer 8 is connected with the direction control handle 3 on control panel 11.
Shown in Fig. 3, for circuit board control circuit figure, control circuit forms integrated circuit by microcomputer control circuit IC1, the first oscillating crystal IC circuit 2, wireless communication module IC circuit 3, potentiometer array circuit IC4, the second oscillating crystal IC circuit 5, connected by wire between each circuit, VSS end is earth terminal, + 5V end is power end, and ANTEN end is wireless transmission antenna end.
Control circuit is controlled by microcomputer control circuit IC1 entirety, and each operating function is completed by computer program, and computer program is as follows:
Embodiment
The use method of operating of this model airplane remote controller is as follows:
1. each parts of model aeroplane remote controller are in quasi-operating status;
2. open the power switch 4 on remote controller control panel 11, remote controller is powered;
3., on the basis that remote controller is powered, the lift control rocking bar 2 simultaneously on remote controller control panel 11 and the direction of direction control handle 3 to power switch 4, start aircraft;
4., after aircraft starts, driven forward lift control rocking bar 2 makes aircraft takeoff;
5., in aircraft flight process, push away forward or pull back direction control handle 3 and aircraft can be made to fly forwards, backwards or backward; Waving direction control handle 3 left or to the right can make aircraft fly left or to the right; Turning clockwise or being rotated counterclockwise direction control handle 3 to make aircraft corresponding clockwise or be rotated counterclockwise;
6. after aircraft flight task completes, pull back lift control rocking bar 2, make aircraft drop to ground;
7., behind aircraft landing ground, pull back lift control rocking bar 2 to minimum state and keep more than about 3 seconds time, aircraft then stops action.
Claims (3)
1. a model aeroplane remote controller, it is characterized in that: primary structure comprises remote controller control box, lift control rocking bar, direction control handle, power switch, circuit board, dc source, lift control potentiometer, direction controlling potentiometer, wireless transmission antenna, power supply indicator, control panel;
Remote controller control box is rectangle, is control panel, arranges lift control rocking bar, direction control handle, power switch, wireless transmission antenna, power supply indicator on the control panel on the top of remote controller control box; In remote controller control box, centre position is provided with circuit board, is control circuit on circuit boards; Be provided with lift control potentiometer at the upper left quarter of the top inner wall of remote controller control box, lift control potentiometer is connected with the lift control rocking bar on control panel; Be provided with direction controlling potentiometer at the upper right quarter of the top inner wall of remote controller control box, direction controlling point position device is connected with the direction control handle on control panel.
2. a kind of model aeroplane remote controller according to claim 1, it is characterized in that: described control circuit forms integrated circuit by microcomputer control circuit IC1, the first oscillating crystal IC circuit 2, wireless communication module IC circuit 3, potentiometer array circuit IC4, the second oscillating crystal IC circuit 5, connected by wire between each circuit, VSS end is earth terminal, + 5V end is power end, and ANTEN end is wireless transmission antenna end.
3. a kind of model aeroplane remote controller according to claim 1, is characterized in that: the chip that described microcomputer control circuit IC1 uses is 32 one-chip computers.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410535869.6A CN104274982A (en) | 2014-10-09 | 2014-10-09 | Model airplane remote controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410535869.6A CN104274982A (en) | 2014-10-09 | 2014-10-09 | Model airplane remote controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104274982A true CN104274982A (en) | 2015-01-14 |
Family
ID=52250625
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410535869.6A Pending CN104274982A (en) | 2014-10-09 | 2014-10-09 | Model airplane remote controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104274982A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5628631A (en) * | 1993-07-23 | 1997-05-13 | Futaba Denshi Kogyo Kabushiki Kaisha | Radio control transmitter |
| JP2945358B2 (en) * | 1997-10-21 | 1999-09-06 | 日本遠隔制御株式会社 | Radio control transmitter |
| CN2671647Y (en) * | 2003-12-25 | 2005-01-19 | 上海飞音玩具模型有限公司 | Regulating device capable of randomly regulating turning angle and remote control electric toy with said device |
| CN201279394Y (en) * | 2008-09-21 | 2009-07-29 | 凯文·李 | Remote controller for radio-control toy robot |
| CN202844580U (en) * | 2012-11-06 | 2013-04-03 | 陈链 | Double-mode model airplane remote control |
| CN203400504U (en) * | 2013-07-29 | 2014-01-22 | 杜超 | Model airplane aircraft remote-control unit with high simulation operability |
| CN203400505U (en) * | 2013-07-29 | 2014-01-22 | 杜超 | Model airplane remote control |
| CN204107052U (en) * | 2014-10-09 | 2015-01-21 | 常晓明 | A kind of model aeroplane remote controller |
-
2014
- 2014-10-09 CN CN201410535869.6A patent/CN104274982A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5628631A (en) * | 1993-07-23 | 1997-05-13 | Futaba Denshi Kogyo Kabushiki Kaisha | Radio control transmitter |
| JP2945358B2 (en) * | 1997-10-21 | 1999-09-06 | 日本遠隔制御株式会社 | Radio control transmitter |
| CN2671647Y (en) * | 2003-12-25 | 2005-01-19 | 上海飞音玩具模型有限公司 | Regulating device capable of randomly regulating turning angle and remote control electric toy with said device |
| CN201279394Y (en) * | 2008-09-21 | 2009-07-29 | 凯文·李 | Remote controller for radio-control toy robot |
| CN202844580U (en) * | 2012-11-06 | 2013-04-03 | 陈链 | Double-mode model airplane remote control |
| CN203400504U (en) * | 2013-07-29 | 2014-01-22 | 杜超 | Model airplane aircraft remote-control unit with high simulation operability |
| CN203400505U (en) * | 2013-07-29 | 2014-01-22 | 杜超 | Model airplane remote control |
| CN204107052U (en) * | 2014-10-09 | 2015-01-21 | 常晓明 | A kind of model aeroplane remote controller |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150114 |
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| RJ01 | Rejection of invention patent application after publication |