CN101214430A - Merlin type series tail fin electronic control system - Google Patents
Merlin type series tail fin electronic control system Download PDFInfo
- Publication number
- CN101214430A CN101214430A CNA2007100041571A CN200710004157A CN101214430A CN 101214430 A CN101214430 A CN 101214430A CN A2007100041571 A CNA2007100041571 A CN A2007100041571A CN 200710004157 A CN200710004157 A CN 200710004157A CN 101214430 A CN101214430 A CN 101214430A
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- Prior art keywords
- control
- control system
- attitude
- electronic control
- tail fin
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Abstract
The invention is an aeroplane model radio remote control system. The invention integrates with hawk series rear fin inventions (application number: 200510075628.9; 200510069897.4; 200510074414.X; 200510074415.4; 200510075637.8; 200510085820.6; 200610149175.4), so as to control rotation, reverse rotation and stoppage of an attitude control motor M. Because a receiver circuit directly drives the attitude control motor M, proportional remote control can be used, and a switch remote control circuit can be also used to realize control to the flying attitude of airplanes.
Description
The present invention is a kind of model airplane wireless remote control system.Because of it combines with invention falcon formula series empennage, thus simple in structure, novelty, adaptability is strong, and is of many uses, cheap.
The technique known background is to use the proportional remote control system to combine with steering wheel at present, controls steering wheel and drive rudder face to reach the purpose of controlling the attitude that pushes button flight.The present invention is because of (application number is respectively: 200510075628.9 with the invention of falcon formula series empennage; 200510069897.4; 200510074414.X; 200510074415.4; 200510075637.8; 200510085820.6; 200610149175.4) combine, M just changes to attitude control motor, counter-rotating and the control of stopping, because of receiver circuit directly drives attitude control motor M, and electric current is less, so can the usage ratio remote control, also can use the switch remote control circuit to realize control to aircraft flight attitude, ask for an interview receiver block diagram accompanying drawing 1.
We know three kinds of states control commonly used in the aircraft flight, fly as a left side, and the right side flies, fly nonstop to or face upward and fly, bowing flies, flat flying, and attitude control motor M will have three kinds of states can reach above control purpose equally so, promptly just change, counter-rotating and parking all can reach above purpose when we use motor ratio drive circuit or switch driving circuit, as using motor special IC LG9110, L293, L298 etc. can simple and effectively achieve the above object.
Claims (3)
1. model airplane Radio Control System is characterized in that: (application number is respectively: 200510075628.9 for this Radio Control System and the invention of falcon formula series empennage; 200510069897.4; 200510074414.X; 200510074415.4; 200510075637.8; 200510085820.6; 200610149175.4) combine, M just changes to attitude control motor, and counter-rotating and the control of stopping and then realization are to the control of aircraft flight attitude
2. the Radio Control System of narrating according to claim 1 is characterized in that: (application number is respectively: 200510075628.9 with the invention of falcon formula series empennage; 200510069897.4; 200510074414.X; 200510074415.4; 200510075637.8; 200510085820.6; 200610149175.4) use combines.
3. the Radio Control System of narrating according to claim 1 is characterized in that: radio receiver circuit contains electromotor control circuit (ratio drive circuit or switch driving circuit) and attitude control motor M, realizes the control to aircraft flight attitude.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007100041571A CN101214430A (en) | 2007-01-06 | 2007-01-06 | Merlin type series tail fin electronic control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007100041571A CN101214430A (en) | 2007-01-06 | 2007-01-06 | Merlin type series tail fin electronic control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101214430A true CN101214430A (en) | 2008-07-09 |
Family
ID=39620972
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2007100041571A Pending CN101214430A (en) | 2007-01-06 | 2007-01-06 | Merlin type series tail fin electronic control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101214430A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101941446B (en) * | 2009-07-09 | 2012-08-01 | 北京锦鸿希电信息技术股份有限公司 | Controllable train tail system |
-
2007
- 2007-01-06 CN CNA2007100041571A patent/CN101214430A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101941446B (en) * | 2009-07-09 | 2012-08-01 | 北京锦鸿希电信息技术股份有限公司 | Controllable train tail system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20080709 |