CN105561598A - Novel direction control system flexible to manipulate - Google Patents
Novel direction control system flexible to manipulate Download PDFInfo
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- CN105561598A CN105561598A CN201410545496.0A CN201410545496A CN105561598A CN 105561598 A CN105561598 A CN 105561598A CN 201410545496 A CN201410545496 A CN 201410545496A CN 105561598 A CN105561598 A CN 105561598A
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- control system
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- steering wheel
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Abstract
The invention provides a novel direction control system flexible to manipulate. The direction control system is composed of a framework provided with a manipulation panel and an integrated circuit board arranged in the framework. The panel is provided with a working mode displayer and multiple mode switching buttons. An inductor and a controller of the novel direction control system flexible to manipulate are combined, and a debugging mode of a steering engine is selected through a working state adjusting knob. The novel direction control system is small in size, low in weight and capable of effectively reducing flight energy consumption and prolonging endurance time.
Description
Technical field
The present invention relates to a kind of model plane product, relate to the novel maneuverable azimuth control system on a kind of model copter specifically.
Background technology
When model copter is in hover state aloft, be subject to blowing of crosswind sometimes, now the afterbody steering wheel of helicopter can produce the phenomenon of horizontal direction skew, for correcting this shift phenomenon, the azimuth control system meeting sending control signal being installed on helicopter afterbody steering wheel, to afterbody steering wheel, resists the skew of afterbody steering wheel with contrary direction.When afterbody steering wheel stops skew, the control signal of azimuth control system also disappears thereupon.If when crosswind blows helicopter constantly, afterbody steering wheel can be caused constantly to offset, now azimuth control system can resist the skew of afterbody steering wheel always, until afterbody steering wheel moves to leeward, weathercock effect that Here it is, thus cause afterbody steering wheel to produce shift phenomenon, and original position cannot be kept; Secondly, tradition azimuth control system only has when the afterbody steering wheel of helicopter moves, and just meeting sending control signal is to afterbody steering wheel steering wheel, when afterbody steering wheel stops mobile, control signal also makes zero thereupon, thus causes azimuth control system cannot control afterbody steering wheel steering wheel in time; In addition, traditional azimuth control system volume is comparatively large, and heavier-weight, can consume energy during helicopter flight, thus decreases the flight time of helicopter.
Therefore, in order to overcome the many disadvantages of traditional azimuth control system, urgently providing a kind of and control flexibly, mobility is high, and modest, the lightweight novel maneuverable azimuth control system of volume.
Summary of the invention
The object of this invention is to provide a kind of to control flexibly, mobility is high, and modest, the lightweight novel maneuverable azimuth control system of volume.
The invention provides a kind of novel maneuverable azimuth control system, it has the manipulation skeleton of plate by one and the surface-mounted integrated circuit be built in wherein forms, panel is provided with mode of operation display and multiple mode switch button, function key comprises steering angle vector control apparatus, duty adjusting knob, forward and direction rotating control key and inductor error size adjustment button, and each function key is electrically connected with surface-mounted integrated circuit.
This novel maneuverable azimuth control system also comprises the afterbody servos control serial line interface and afterbody rudder control interface of being drawn by surface-mounted integrated circuit further.
Model copter is provided with further the receiving system and afterbody steering wheel that receive remote controller control signal, receiving system is provided with afterbody steering wheel channel, and described afterbody rudder control interface is electrically connected with the afterbody steering wheel channel of receiving system; Described afterbody steering wheel machine controls serial line interface and is electrically connected with afterbody steering wheel.This novel maneuverable azimuth control system is by bolt or electric welding or be installed on model copter by the mode of screw riveted, vertical with the main shaft of model copter bottom the installation of this novel maneuverable azimuth control system.
Model copter is also provided with motor further, and the distance of this novel maneuverable azimuth control system and motor is not less than 15cm.
Compared with prior art, novel maneuverable azimuth control system of the present invention has the following advantages:
(1) volume slight of stature, lighter in weight, and can effectively reduce flight energy consumption, extend cruising time;
(2) inductor and controller are combined as a whole, by the operator scheme of the changeable selection steering wheel of AVCS duty adjusting knob, when in a locked mode, novel maneuverable azimuth control system meeting auto modification afterbody steering wheel, when being in general modfel, manually can control the mode of remote controller, adjustment afterbody steering wheel length of connecting rod, makes model copter afterbody steering wheel when hover can not produce any skew;
(3) sensitivity of adjustable novel maneuverable azimuth control system, the sensitivity of novel maneuverable azimuth control system and the rotating speed direct proportionality of afterbody steering wheel and host wing, the sensitivity regulating novel maneuverable azimuth control system can be passed through, to control the rotating speed of afterbody steering wheel and host wing.
For making the present invention easier to understand, set forth the specific embodiment of a kind of novel maneuverable azimuth control system of the present invention further below in conjunction with accompanying drawing.
Accompanying drawing explanation
Fig. 1 is the operating surface structural representation of the novel maneuverable azimuth control system of the present invention;
Fig. 2 is the intention that the novel maneuverable azimuth control system of the present invention and afterbody steering wheel and receiving system are electrically connected.
Detailed description of the invention
Illustrated novel maneuverable azimuth control system, adopt steering angle vector control apparatus, aiming at mould rises designed by machine, inductor and controller are combined, effect due to novel maneuverable azimuth control system is to adjust steering wheel, the mainly skew of afterbody steering wheel, turning to of auxiliary adjustment mould aircraft, makes its flight control more accurate.
As depicted in figs. 1 and 2, novel maneuverable azimuth control system has the manipulation skeleton of plate 100 by one and the surface-mounted integrated circuit (not shown) be built in wherein forms, function key on manipulation plate 100 is electrically connected to the corresponding functional module on surface-mounted integrated circuit respectively, surface-mounted integrated circuit electrical connection afterbody steering wheel and receiving system, wherein, the signal of telecommunication of remote controller is sent to novel maneuverable azimuth control system by receiving system, novel maneuverable azimuth control system sends and controls signal to afterbody steering wheel, the skew of adjustment afterbody steering wheel.
The panel of novel maneuverable azimuth control system is provided with mode of operation display 10 and several function keys, wherein, function key comprises duty adjusting knob 11, forward and direction rotating control key 12 and inductor error size adjustment button 13, and the surface-mounted integrated circuit be built in skeleton also connects afterbody rudder control interface 14 by cable and afterbody steering wheel machine controls serial line interface 15.Mode of operation display 10 is located at the top of middle panel, duty adjusting knob 11 is positioned at the below of mode of operation display 10, forward and direction rotating control key 12 are positioned at the below of AVCS duty adjusting knob 11, and the middle upper position of panel is provided with inductor error size adjustment button 13.Each function key is electrically connected with the corresponding functional module on surface-mounted integrated circuit, by each function key on control panel, realizes the various function point analysis of novel maneuverable azimuth control system.
Mode of operation display 10 is generally LED, for showing the duty of this novel maneuverable azimuth control system.When its fast blink, after representing power-on, novel maneuverable azimuth control system is carrying out the initialized program of data; When its permanent bright time, represent that novel maneuverable azimuth control system initializes and complete, be positioned at locking mode; When it extinguishes, represent that power supply has been closed or novel maneuverable azimuth control system is positioned at general modfel; When it glimmers at a slow speed, represent that novel maneuverable azimuth control system does not receive the afterbody servos control signal sent by remote controller, now afterbody steering wheel steering wheel cannot operate; Glimmer twice expression when locking mode, the afterbody servos control signal received at present is different from the neutrality point signal being stored in novel maneuverable azimuth control system, all there will be this lamp flicker twice: a) stirring afterbody steering wheel rocking bar in following situation; B) central point of afterbody steering wheel offsets, and must reset central point.
Duty adjusting knob 11, by switching AVCS duty adjusting knob, select the operator scheme of novel maneuverable azimuth control system: locking mode or general modfel, to coordinate the various situations of model copter to carry out the debugging adapted, substantially increase practicality.If selected lock mould-fixed, novel maneuverable azimuth control system meeting auto modification afterbody steering wheel, makes the afterbody steering wheel of helicopter can not produce any skew, but cannot check that whether the length of afterbody steering wheel connecting rod is correct; General in maiden flight or when reinstalling afterbody steering wheel connecting rod, adopt general modfel to test, to adjust afterbody steering wheel length of connecting rod, make model copter when hover state, afterbody steering wheel can not produce any skew.If afterbody steering wheel only has skew slightly, then can use the adjustment of afterbody steering wheel.General recommendations, just adopts general modfel during debugging; Locking mode is adopted during state of flight.
Forward and direction rotating control key 12 for the controlling party that switches novel maneuverable azimuth control system to, user can do correct switching according to the direction of the host wing direction of rotation of model helicopter and afterbody steering wheel connecting rod.
Inductor error size adjustment button 13 is for adjusting the induction sensitivity of novel maneuverable azimuth control system, rotate clockwise knob, increase induction sensitivity, rotate counterclockwise knob and reduce induction sensitivity, the induction sensitivity size of novel maneuverable azimuth control system can because of afterbody steering wheel and the different of model copter difference to some extent.
Afterbody rudder control interface 14, is drawn by the surface-mounted integrated circuit of novel maneuverable azimuth control system, and is electrically connected with the afterbody steering wheel channel of the receiving system of model copter.
Model copter is provided with afterbody steering wheel 2 further, afterbody steering wheel machine controls serial line interface 15, drawn by the surface-mounted integrated circuit of novel maneuverable azimuth control system, and be electrically connected with the afterbody steering wheel steering wheel 2 of model copter, for controlling direction and the fine setting of afterbody steering wheel.
Novel maneuverable azimuth control system can be pasted or weld or be installed on model copter by the mode of screw riveted, and the bottom of this novel maneuverable azimuth control system must be vertical with the main shaft of helicopter, otherwise left and right can be affected sidewinder and the direction of somersault; When being installed on electric model helicopter by this novel maneuverable azimuth control system, the spacing between this novel maneuverable azimuth control system and motor of model copter must be equal to or greater than 15cm, disturbs to avoid producing with motor.
When the afterbody steering wheel of model copter be subject to crosswind blow and produce the phenomenon of skew time, novel maneuverable azimuth control system can resist the skew of afterbody steering wheel, novel maneuverable azimuth control system can calculate the angle of skew simultaneously, and continue sending control signal to resist crosswind, even if when therefore crosswind ceaselessly blows helicopter, afterbody steering wheel still can not produce skew.In other words, novel maneuverable azimuth control system meeting auto modification is because of the afterbody steering wheel skew caused by crosswind.By the switching of pattern, select the adjustment modes adapted with model copter state.Increase the sensitivity of novel maneuverable azimuth control system gradually, and then increase the time postponed, tracking phenomenon can be eliminated.In addition, this novel maneuverable azimuth control system compact, lighter in weight, is convenient to be installed on helicopter, and can effectively reduce flight energy consumption, extends the flight time.
A kind of preferred embodiment being suitable for aviation aircraft position controller of the above disclosed the present invention of being only, certainly the interest field of the present invention can not be limited with this, therefore according to the equivalent variations that the present patent application the scope of the claims is done, the scope that the present invention is contained still is belonged to.
Claims (5)
1. a novel maneuverable azimuth control system, be arranged on model copter, it has the manipulation skeleton of plate by one and the surface-mounted integrated circuit be built in wherein forms, it is characterized in that: panel is provided with mode of operation display and multiple mode switch button, function key comprises steering angle vector control apparatus, duty adjusting knob, forward and direction rotating control key and inductor error size adjustment button, and each function key is electrically connected with surface-mounted integrated circuit.
2. novel maneuverable azimuth control system according to claim 1, is characterized in that: this novel maneuverable azimuth control system also comprises the afterbody servos control serial line interface of being drawn by surface-mounted integrated circuit further.
3. novel maneuverable azimuth control system according to claim 1, is characterized in that: this novel maneuverable azimuth control system also comprises the afterbody rudder control interface of being drawn by surface-mounted integrated circuit further.
4. novel maneuverable azimuth control system according to claim 3, it is characterized in that: model copter is provided with further the receiving system receiving remote controller control signal, receiving system is provided with afterbody steering wheel channel, and described afterbody rudder control interface is electrically connected with the afterbody steering wheel channel of receiving system.
5. novel maneuverable azimuth control system according to claim 2, is characterized in that: model copter is provided with further afterbody steering wheel steering wheel, and described afterbody steering wheel machine controls serial line interface and is electrically connected with afterbody steering wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410545496.0A CN105561598A (en) | 2014-10-15 | 2014-10-15 | Novel direction control system flexible to manipulate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410545496.0A CN105561598A (en) | 2014-10-15 | 2014-10-15 | Novel direction control system flexible to manipulate |
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| Publication Number | Publication Date |
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| CN105561598A true CN105561598A (en) | 2016-05-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410545496.0A Pending CN105561598A (en) | 2014-10-15 | 2014-10-15 | Novel direction control system flexible to manipulate |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105771274A (en) * | 2014-12-25 | 2016-07-20 | 许美兰 | Novel flexible-to-operate azimuth control system |
| CN105807782A (en) * | 2014-12-31 | 2016-07-27 | 马铿杰 | Remote control system with function of displaying work state in real time |
| CN106621382A (en) * | 2015-11-04 | 2017-05-10 | 许美兰 | Novel direction control system flexible to manipulate |
-
2014
- 2014-10-15 CN CN201410545496.0A patent/CN105561598A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105771274A (en) * | 2014-12-25 | 2016-07-20 | 许美兰 | Novel flexible-to-operate azimuth control system |
| CN105807782A (en) * | 2014-12-31 | 2016-07-27 | 马铿杰 | Remote control system with function of displaying work state in real time |
| CN106621382A (en) * | 2015-11-04 | 2017-05-10 | 许美兰 | Novel direction control system flexible to manipulate |
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Application publication date: 20160511 |