KR101688420B1 - Automatic control system for taking off and landing a miniature plane - Google Patents

Abstract

The present invention relates to a taking-off / landing control system for a model airplane to show taking-off / landing of a model airplane similar to taking-off / landing of an actual airplane, on a runway of a miniature model. To this end, the present invention comprises: a model runway which is formed in a miniature model airfield and in which a plurality of infrared sensors for sensing the position of the model airplane are embedded and support member guide grooves are formed along the central portion of a road surface; a model mooring which is formed as a road surface in the miniature model airfield and connected to the model runway to form a closed loop and in which a direction guiding member for guiding the travel of the model airplane is embedded along the central portion of the road surface; the model airplane configured to be movable along the road surface of the model mooring and having a steering member acting on the direction guiding member of the model airplane and a wheel drive motor for driving wheels; a supporting member driving body installed in a supporting member driving body mounting space and providing power for lifting and horizontally moving first and second moving body supporting members; and an automatic taking-off / landing control unit which automatically controls the traveling operation of the model airplane in the model mooring and taking-off / landing operations of the model airplane on the model runway by driving a support member actuator in response to the sensor signals of each of the model runway and the model airplane a key input signal from an operation of a user. Therefore, the present invention is capable of attracting the attention of visitors at various exhibition facilities such as exhibition halls and museums.

Description

[0001] The present invention relates to an automatic control system for taking off and landing a miniature plane,

The present invention relates to an automatic landing / landing control system of a model airplane capable of automatically controlling the takeoff or landing of a model airplane on a runway of a model airfield constructed with a miniature model, Or landing of the runway, so that the takeoff or landing motion of the model airplane on the runway and the corresponding sound and illumination can be produced in a manner similar to the environment when the actual airplanes take off and land on the runway, Landing automation system of a model airplane that enables more dynamic and mobile modeling aircraft landing / landing operations to be carried out in various viewing facilities such as museums.

Generally, model cities and model villages, which are usually made of miniature models, are used as exhibits in various exhibition facilities such as various exhibition halls and museums because they have the advantage of expressing various scenes of cities and villages intensively in a narrow place, In recent years, as the technology of manufacturing such a miniature model has been developed, roads are made in the city of a reduced model and the transportation means (train, automobile, etc.) of the miniature model on the road can be operated in a manner similar to the actual one. To be more concentrated.

In this regard, Korean Patent Laid-Open No. 10-2004-0084423 (published on October 10, 2004; hereinafter referred to as "Patent Document 1") discloses a model car driving apparatus for driving a model car on a road such as a house model exhibit Is known.

According to Patent Document 1, it is possible to attract a consumer's attention by moving a model object such as a model car to a model exhibit such as a house model exhibit along a predetermined traveling path, and in particular, to dynamically display a living space in a housing complex .

In addition, Korean Unexamined Patent Publication No. 10-2010-0121930 (published on November 19, 2010; hereinafter referred to as "Patent Document 2") describes a model in which a model car mounted on a substrate is driven by a traveling device BACKGROUND ART [0002] Techniques relating to a vehicle driving apparatus are known.

According to Patent Document 2, a model car is able to travel along various types of traveling roads, and can also travel on a plane having vertical bends.

However, in the above-described conventional technology, the automobile traveling on the model road continuously runs on the same road in infinite repetition irrespective of the type of the vehicle, so that the automobile crashes, crashes, There is a fear that the vehicle may be damaged, and there is no speed change such as change, stop, or departure of the running route of the model car moving on the model road, so that the dynamic feeling of urgency and the reality are lowered.

In addition, since the transportation means implemented for the automatic traveling device in the conventional miniature model as described above is mainly limited to automobiles and trains that run on ground roads, it is possible to use a ground runway such as a model airplane, The technology for implementing and controlling the takeoff and landing operations of model airplanes that require movement on the ground is not yet developed or applied.

KR 10-2004-0084423 A 2004.10.06. open KR 10-2010-0121930 A 2010.11.19. open

SUMMARY OF THE INVENTION It is therefore an object of the present invention to provide a runway of a reduced scale model having a certain length and width necessary for takeoff or landing of a model airplane, By automatically taking off or landing an airplane, it is possible to control the sound and lighting of the model airplane landing and landing similar to the circumstances when actual airplanes take off and land on the runway, Landing automatic control system of a model airplane which enables to realize a more dynamic and mobile type airplane landing / landing operation and to concentrate the attention of spectators effectively.

According to an aspect of the present invention, there is provided an air conditioner comprising: a plurality of infrared sensors for sensing the position of a model airplane; A model runway formed along the center portion of the road surface, a guide runway formed in the aerodrome of a reduced-scale model in a road surface, connected to the model runway to form a closed loop, and a direction guide member for guiding the runway of the model airplane A model airplane configured to be able to move along a road surface of a model docking station having a steering member for operating a directional guide member of a model dock and a wheel drive motor for driving a wheel, A support member for providing power for lifting and horizontally moving the second moving body supporting member, Landing movement on the model runway of the model airplane by driving the support member actuator according to the sensor signal of the model runway and the model airplane and the key input signal by the user operation, Landing automatic control system, including a landing automatic control unit.

According to the present invention, an automatic takeoff or landing motion of a model airplane and a sound and illumination of a model airplane on / off the runway of a model having a certain length and width necessary for takeoff or landing of the model airplane, It is possible to implement a more dynamic and mobile model airplane landing / landing operation in various viewing facilities such as an exhibition hall and a museum, It is possible to obtain an advantage that the attention of the spectators can be effectively concentrated when the control system of the present invention is installed in the facility.

1 is a block diagram illustrating an overall configuration of an automatic landing / landing control system of a model airplane according to the present invention.
FIGS. 2A and 2B are a schematic plan view of a model runway and a model runway illustrating the automatic landing / landing control system of the model airplane according to the present invention, and an internal construction diagram of the model runway.
FIGS. 3A and 3B are reference views illustrating the take-off process and the landing process performed in the automatic landing / landing control system of the model airplane according to the present invention, respectively.
4 (a) to 4 (c) are a front view, a rear view, and a side view illustrating the support member driving body in an automatic landing / landing control system of a model airplane according to the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, the construction and operation of an automatic landing / landing control system of a model airplane according to a preferred embodiment of the present invention will be described in detail with reference to the accompanying drawings.

It is to be understood that the words or words used in the present specification and claims are not to be construed in a conventional or dictionary sense and that the inventor can properly define the concept of a term in order to describe its invention in the best possible way And should be construed in light of the meanings and concepts consistent with the technical idea of the present invention. Therefore, it should be understood that the embodiments described herein and the configurations shown in the drawings are only the most preferred embodiments of the present invention, and that various equivalents and modifications may be made thereto at the time of the present application shall.

FIG. 1 is a block diagram illustrating an overall configuration of an automatic landing / landing control system of a model airplane according to the present invention. FIGS. 2A and 2B illustrate an automatic landing / FIGS. 3A and 3B are views showing a take-off process and a landing process in the automatic landing / landing control system of the model airplane according to the present invention, respectively, 4 (a) to 4 (c) are a front view, a rear view and a side view exemplified by extracting the support member driving body in the automatic landing / landing control system of the model airplane according to the present invention, The automatic landing / landing control system of the model airplane according to the present invention includes a model runway 10, a model hangar 20, a model airplane 30, a support member driver 40, and an automatic landing / ) .

The model runway 10 is formed of a road surface having a length and width required for realizing landing and landing of a model airplane on a substrate in a reduced model aerodrome. . A plurality of infrared sensors 11a and 11b for sensing the position of the model airplane are embedded in the road surface of the model runway 10 and a plurality of infrared sensors 11a and 11b for detecting the position of the model airplane, The support member guide groove 12 is formed along the longitudinal direction of the model runway along the center portion of the road surface. Preferably, the infrared sensors 11a and 11b are embedded at the start and end points of the model runway 10, respectively, and are installed at positions where the front wheel position of the model airplane can be detected. The support member guide groove 12 is formed along the entire length in the longitudinal direction at the center of the road surface of the model runway 10 and the support member guide groove 12 is formed to be wider than the diameter of the fuselage support members 43a and 43b It is preferable that they are formed at intervals.

The model mooring 20 is formed on the substrate in the aerodrome of the reduced model and connected to the model runway 10 to form a closed loop and is formed of the road surface having the length and width required for mooring the model airplane, And a direction guiding member 21 for guiding traveling of the model airplane 30 is buried along the center portion. The direction guiding member 21 is preferably made of wire or wire capable of reacting with the magnet. The direction guiding member 21 is installed on the center line of the center of the model mooring platform 20 as a whole. In order to reduce the material cost, So that they are spaced apart from each other at regular intervals.

The model airplane 30 is provided with a steering member that works with the directional guide member 21 of the model mooring platform 20 and a wheel drive motor 32 for driving the wheel (which may be preferably a front wheel) And is movable along the road surface of the model hanging platform 20 by the steering operation by the action of the rotation of the front wheel by the operation of the direction guiding member 21 and the steering member. The steering member of the model airplane 30 is not shown in the drawing, but is preferably installed on the front wheel. For example, the steering member may be constructed by attaching an ultra-small magnet to a thin alloy plate.

In addition, the model airplane 30 may further include a plurality of support member detection sensors 31a and 31b, a moving body control unit 33, and a wireless transmission / reception unit 34.

Each of the support member detection sensors 31a and 31b is provided under the fuselage of the model airplane and includes a reed sensor responsive to a magnet to contact and separate the first and second moving body support members 43a and 43b And separates and outputs the mounting completion signal according to the contact or the separation completion signal according to the separation. For example, when the two sensors 31a and 31b are both operated, the support member detection sensors 31a and 31b detect that the mounting between the first and second moving body supporting members 43a and 43b and the model airplane 30 When both of the two sensors 31a and 31b are operated, neither a mounting completion signal nor a separation completion signal is outputted. When the sensors 31a and 31b are operated, the mounting completion signal indicating completion is output to the moving body control unit 33, To the moving body control unit 33, a separation completion signal indicating that the separation between the first and second moving body supporting members 43a and 43b and the body of the model airplane 30 is completed.

The wheel drive motor 32 is controlled by the body control unit 33 to provide or shut off the power for the front wheel rotation and is preferably operated by the body control unit 33 when the first infrared sensor 11a is operated When the second infrared ray sensor 11b is operated while the power source is shut off, the rotation of the wheel is stopped, and the power source is supplied by the body control unit 33 so that the rotation of the wheel is performed. Landing automatic control unit 100 receives the output of the first infrared sensor 11a installed at the start point of the model runway 10 so that the automatic landing / When the motor stop signal is outputted and transmitted through the wireless transmission / reception units 120 and 34, the body control unit 33 stops the operation of the wheel drive motor 32 by the motor stop signal. Landing automatic control unit 100 receives the output of the second infrared sensor 11b installed at the end of the model runway 10 and the motor / And transmits the signal through the wireless transmission / reception units 120 and 34, the body control unit 33 operates the wheel drive motor 32 by the motor drive signal.

The moving body control unit 33 transmits the outputs of the respective support member detection sensors 31a and 31b provided in the body of the model airplane 30 to the landing and landing automatic control unit 100 through the wireless transmitting / And controls the operation of the wheel drive motor 32 in accordance with the control signal received from the automatic landing /

The wireless transmitting / receiving unit 34 performs wireless communication with the wireless transmitting / receiving unit 120 of the automatic landing /

2B, the supporting member driving body 40 is installed in a supporting member driving body installation space formed on the lower surface of the model runway 10, and the first and second moving body supporting members 43a and 43b And provides power for lifting and horizontal movement, respectively. To this end, the supporting member driving body 40 includes a horizontal moving guide member 41, a moving block 42, first and second moving body supporting members 43a and 43b, first to third linear motor driving units 44a to 44c ), A first linear motor (LM1), a second linear motor (LM2), and a third linear motor (LM3).

The horizontal movement guide member 41 is installed on the lower portion of the model runway 10 and is installed entirely along the longitudinal direction of the model runway 10 so that the movement of the movement block 42 in the horizontal direction Guide.

The moving block 42 is supported by the horizontal moving guide member 41 and is provided so as to be able to move in the left and right horizontal directions with the horizontal moving guide member. The first and second moving body supporting members 43a and 43b are vertically (For example, the longitudinal direction of the y-axis). Such a moving block can preferably be implemented with an aluminum profile.

The first and second moving body supporting members 43a and 43b are installed vertically movably with the lower end supported by the moving block 42 so that the body of the model airplane 30 can be supported vertically And magnets for operating the support member detection sensors 31a and 31b mounted on the model airplane 30 are attached to the upper end thereof.

The first to third linear motor driving units 44a to 44c are independently controlled by the on / off automatic control unit 100 to independently drive the first to third linear motors LM1 to LM3.

The first linear motor LM1 and the second linear motor LM2 are respectively driven by the first and second linear motor driving portions 44a and 44b to be forward and reverse rotations respectively and the first and second moving body supporting members 43a, 43b, respectively.

The third linear motor LM3 is driven by the third linear motor driving portion 44c to be forward and reverse, and provides power for horizontal movement of the moving block 42. [

The automatic landing / landing control unit 100 drives the supporting member driving body 40 in accordance with sensor signals of the model runway 10 and the model airplane 30 and a key input signal by a user operation, ) Of the model airplane (30) on the model runway (10) and on the model runway (10) on the model runway (10). For this, the automatic landing / landing control unit 100 may include a key input unit 110, a wireless transceiver unit 120, and an i / landing control unit 130, and may also include an acoustic driver 150 and a light driver 160 ). ≪ / RTI >

The key input unit 110 may be configured to include a plurality of keys for user operation, and may be configured to receive a selection input whether the user performs an automatic landing or a manual landing control.

The wireless transceiver unit 120 wirelessly communicates with the body control unit 33 in the model airplane 30 to receive the operation signals of the support rod detection sensors 31a and 31b or transmit the control signals of the wheel drive motor 32 .

The landing control unit 130 is directly connected to the infrared sensors 11a and 11b embedded in the model runway 10 to receive the position detection signal of the model airplane 30 on the model runway 10, Receiving signal transmitted and received by the model airplane 30 and a key input signal by a user operation to drive the wheel of the model airplane 30 or drive the support member driving body 40 to drive the model aircraft 30 20 and the landing / landing operation on the model runway 10. [0040]

The landing / landing control unit 130 may be equipped with a speed adjusting program. This speed control program divides and sets the entire section of the model runway 10 into a plurality of zones and sets the speed of the first and second moving body supporting members < RTI ID = 0.0 > 43a and 43b and the horizontal moving speed of the moving block 42 by the third linear motor LM3 are mixed and controlled differently in the respective zones so that the model airplane The inclination of the body of the vehicle 30 and the yawing / landing speed of the vehicle 30 can be adjusted by mixing them in different zones.

3A, during the take-off operation of the model airplane 30, the entire section of the model runway 10 is divided into three sections. In the first section, the initial take-off The height of the first moving body supporting member 43a by the first linear motor LM1 and the height of the second moving body supporting member 43b by the second linear motor LM2 are made equal to each other on the ground surface And the ascending speed of the second moving body supporting member 43b by the second linear motor LM2 is gradually increased from the first linear motor LM1 to the first linear motor LM1 by the first linear motor LM1, And the slope of the fuselage of the model airplane 30 is gradually increased toward the third zone.

On the other hand, as illustrated in FIG. 3B, during the landing operation of the model airplane 30, the entire section of the model runway 10 is divided into three sections, and in the first section, The height of the second moving body supporting member 43b by the second linear motor LM2 is made higher than the height of the first moving body supporting member 43a by the first linear motor LM1 And the descending speed of the second moving body supporting member 43b by the second linear motor LM2 is set to the first moving body supporting member 43a by the first linear motor LM1 as it approaches the end point of the model runway 10, The descent speed of the model airplane 30 can be reduced by gradually decreasing the descent speed of the model airplane 30 gradually.

In addition, the speed control program sets the whole section of the model runway 10 into a plurality of zones, and controls the horizontal movement speed of the moving block 42 by the third linear motor LM3 to be controlled differently in each zone So that the horizontally moving speed of the model airplane 30 can be adjusted differently for each zone within the section of the model runway 10. For example, in this speed control program, the horizontal movement speed of the moving block 42 by the third linear motor LM3 is gradually increased toward the end of the model runway 10 during the take-off operation of the model airplane 30 And increases the horizontal movement speed of the model airplane 30 to the third zone so that the third linear motor LM3 moves to the end point of the model runway 10 during the landing operation of the model airplane 30. [ It is possible to reduce the moving speed of the moving block 42 by the moving speed of the model airplane 30 and reduce the traveling speed of the model airplane 30 to the third zone.

Meanwhile, the acoustic driver 150 stores each sound source (for example, an effect sound during takeoff and a reverse sound effect when landing) due to takeoff or landing of the model airplane, and at least one speaker for outputting the sound source And is controlled by the landing / landing control unit 130 to select and output a sound source upon takeoff or landing.

The illumination driving unit 160 includes a model mooring platform 20 at a position where lighting is required when the model airplane is moored or taken off and landed, and a plurality of lighting devices installed on the model runway 10, 130 to select and drive each lighting device, thereby realizing a lighting effect as in actual landing / landing.

The operation of the present invention constituted as described above and its operation and effect will be described as follows.

First, the take-off operation of the model airplane is described as follows. A motor drive signal is transmitted from the landing / landing automatic control unit 100 to the wake-up airplane 30 located at the model mooring station 20, The thin alloy plate and the micro magnet provided on the front wheel of the model airplane 30 act on the direction guiding member 21 of the model mooring platform 20 so that the wheel driving motor 32 can be driven, The model airplane 30 continues to automatically run along the road surface of the model hanging platform 20 to perform the steering operation by the rotation operation of the front wheel by the operation of the direction guide member 21 and the steering member, And becomes movable.

When the model airplane 30 arrives at the first space 10a which is the preparation space for waiting for takeoff or landing of the model runway 10 after leaving the model hangar 20, The first infrared sensor 11a recognizes the front wheel of the model airplane 30 and operates. The output of the first infrared sensor 11a is input to the I / F controller 130.

Therefore, the landing / landing control unit 130 outputs a control signal for stopping the operation of the wheel driving motor 32 and transmits the control signal through the wireless transmitting / receiving units 120 and 34. The moving body control unit 33 in the model airplane 30 , The power of the wheel drive motor 32 is cut off according to a control signal for stopping the operation of the wheel drive motor 32 received from the landing control unit 130 so that the front wheel of the model airplane no longer rotates, .

After the power of the wheel driving motor 32 is cut off, the landing / landing control unit 130 controls the first and second linear motor driving units 44a and 44b of the supporting member driving body 40 to rotate the first and second When the power is supplied to the linear motors LM1 and LM2, the first and second moving body supporting members 43a and 43b, which are supported to be movable up and down by the body of the moving block 42, The support member detection sensors 31a and 31b provided inside the model airplane 30 at the moment when the upper ends of the first and second moving body supporting members 43a and 43b contact the body of the model airplane 30, The first and second moving body supporting members 43a and 43b are brought into close contact with the lower portion of the body of the model airplane 30 while the first and second moving body supporting members 43a and 43b act on the magnets attached to the upper ends of the moving body supporting members 43a and 43b, The support members 43a and 43b can support the model airplane 30 stably.

At this time, in order to implement the initial operation for taking-off or landing the model airplane 30 in the first zone, the landing / landing control unit 130 controls the first moving body supporting member 43a of the second linear motor LM2 and the height of the second moving body supporting member 43b by the second linear motor LM2 are raised to the same height so as to contact the ground surface, The height of the second moving body supporting member 43b by the second linear motor LM2 is raised higher than the height of the moving body supporting member 43a.

When both the first and second moving body supporting members 43a and 43b contact the body of the model airplane 30 and both of the supporting member detecting sensors 31a and 31b are operated, The mounting completion signal corresponding to the contact of the first and second wheels 43a and 43b is transmitted to the body control unit 33 and then transmitted to the landing and landing control unit 130 through the wireless transmitting and receiving units 34 and 120. [

Therefore, the landing / landing control unit 130 recognizes that the mounting between the first and second moving body supporting members 43a and 43b and the body of the model airplane 30 is completed, and the third linear motor driving unit 40, And supplies power to the third linear motor LM3.

When the third linear motor LM3 is driven, the moving block 42 supported horizontally by the horizontal movement guide member 41 moves in the horizontal direction.

When the moving block 42 starts to move in the horizontal direction, the landing / landing control unit 130 performs a take-off operation of the model airplane 30 as shown in FIG. 3A, The rising speed of the second moving body supporting member 43b by the linear motor LM2 is increased stepwise higher than the rising speed of the first moving body supporting member 43a by the first linear motor LM1, The slope of the fuselage of the third linear motor LM3 is gradually increased toward the third zone so that the slope of the slope can be controlled to be the same as when the actual airplane takes off. The moving speed of the moving block 42 by the moving block 42 is also increased stepwise to increase the horizontal moving speed of the model airplane 30 so that the same speed as when the actual airplane takes off can be produced.

3B, the lowering speed of the second moving body supporting member 43b by the second linear motor LM2 is set to be gradually decreased toward the end point of the model runway 10 during the landing operation of the model airplane 30. In this case, 1 linear motor LM1 to gradually decrease the inclination of the body of the model airplane 30 toward the third zone so that when the actual airplane landing And the horizontal movement speed of the moving block 42 by the third linear motor LM3 is also gradually decreased toward the end point of the model runway 10 so that the model airplane 30 ), Thereby making it possible to produce the same speed as when the actual airplane landed.

When the model airplane arrives in the second space 10b, which is a waiting space after completion of takeoff or landing of the model runway 10 after the take-off operation or landing operation of the model airplane is completed, The second infrared sensor 11b recognizes the front wheel of the model airplane 30 and operates again and the output of the second infrared sensor 11b is input to the landing control unit 130.

If the controller 15 controls the first and second linear motor drivers 44a and 44b of the support member driver 40 after receiving the output of the second infrared sensor 11b, The upper ends of the first and second moving body supporting members 43a and 43b supporting the body of the model airplane 30 are moved downward by the upper end of the body plane of the model airplane 30 as the lower body supporting members 43a and 43b descend, The supporting member detecting sensors 31a and 31b installed inside the model airplane 30 are not operated and the first and second moving body supporting members 43a and 43b and the model airplane 30 A separation completion signal indicating that the separation between the two is completed is outputted to the moving body control section 33. [

The landing / landing control unit 130 recognizes that the separation between the first and second moving body supporting members 43a and 43b and the body of the model airplane 30 is completed and recognizes that the third linear motor driving unit 44c to move the moving block 42 back to the starting point on the model runway 10.

In addition, the landing / landing control unit 130 outputs an operation control signal of the wheel driving motor 32 and transmits the operation control signal through the wireless transmitting / receiving units 120 and 34. When the moving body control unit 33 in the model airplane 30 The front wheel of the model airplane is rotated again so that the model airplane 30 is driven by the model driving force of the wheel drive motor 32, The model mooring platform 20 can be automatically driven from the runway 10. When the model airplane 30 enters the starting point of the model runway 10 again via the model mooring station 20, The take-off or landing operation can be controlled repeatedly. The preferred control method is that the takeoff and landing movements of the model airplane are controlled to be alternately repeated one at a time.

According to the present invention, when the model airplane is automatically taken off or landed on a reduced-scale model runway having a predetermined length and width necessary for takeoff or landing of the model airplane, sound and lighting of the model airplane landing / It is possible to implement more dynamic and mobile modeling aircraft landing / landing operations in various viewing facilities such as exhibition halls and museums, effectively concentrating the attention of spectators. Provides an advantage.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the disclosed exemplary embodiments, but, on the contrary, Modification is possible. Accordingly, it is intended that the scope of the invention be defined by the claims appended hereto, and that all equivalent or equivalent variations thereof fall within the scope of the present invention.

10: Model runway 11a, 11b: Infrared sensor
12: Support member guide groove 20: Model dock
21: direction guiding member 30: model airplane
31a, 31b: Support member detection sensor 32: Wheel drive motor
33: Moving body control section 34, 120: Wireless transmission /
40: support member driving body 41: horizontal movement guide member
42: moving block 43a, 43b: moving body supporting member
44a-44c: Linear motor drive unit 100: I /
110: key input unit 130:
150: acoustic driver 160:

Claims (14)

A plurality of infrared sensors 11a and 11b for sensing the position of the model airplane are embedded in the space in the lower surface of the road surface, A model runway 10 in which a support member guide groove 12 for guiding the members 43a and 43b to ascend and descend is formed along a central portion of the road surface;
A model hanging platform (not shown) formed on a substrate in a reduced-scale aerodrome, connected to the model runway 10 to form a closed loop, and a direction guide member 21 for guiding the running of the model airplane 30 along the center of the road 20);
A wheel driving motor 32 for driving the steering wheel and a steering member acting on the direction guiding member 21 of the model hanging frame 20 to rotate the wheel by the wheel driving motor, A model airplane (30) configured to be movable along a road surface of the model dock (20) by a steering operation by the action of a steering member;
A support member driver 40 installed in the support member driver installation space on the road surface of the model runway 10 for providing power for raising and lowering the first and second moving body support members 43a and 43b, ); And
The supporting member driving body 40 is driven according to sensor signals of the model runway 10 and the model airplane 30 and a key input signal by a user operation so that the model aircraft 30 of the model airplane 30, And an automatic landing / landing control unit (100) for automatically controlling the traveling operation and the landing / landing operation on the model runway (10). 2. The apparatus according to claim 1, wherein each of the infrared sensors (11a, 11b)
And is embedded at the start and end points of the model runway (10), respectively. 2. The apparatus according to claim 1, wherein the support member guide groove (12)
And is formed along the entire length in the center of the road surface of the model runway (10). 2. The apparatus according to claim 1, wherein the directional guide member (21)
Landing automatic control system of the model airplane, wherein the landing automation control system is installed in a state of being embedded on the center line of the center portion of the model mooring platform 20 as a whole, but spaced apart at regular intervals along the road surface center line of the mooring platform. The method according to claim 1,
The steering member of the model airplane (30) is mounted on the front wheel and has a magnet attached thereto,
Wherein the direction guiding member (21) is made of wire or wire. 2. The model airplane of claim 1, wherein the model airplane (30)
Support member detection sensors 31a and 31b for detecting contact and separation of the first and second moving body supporting members 43a and 43b;
Landing automatic control unit 100 or receives a control signal from the landing / landing automatic control unit 100 to output the output of each of the support member detection sensors 31a and 31b to the operation of the wheel drive motor 32 A moving body control unit 33 for controlling the moving body; And
And a wireless transmitting / receiving unit (34) for wireless communication with the automatic landing / landing control unit (100). 7. The apparatus according to claim 6, wherein the support member detection sensors (31a, 31b)
And a reed sensor responsive to the magnet,
When both the support member detection sensors 31a and 31b are operated, a signal indicating completion of mounting between the first and second moving body supporting members 43a and 43b and the model body of the model airplane 30 is output. And 31b are not in operation, a signal indicating completion of separation between the first and second moving body supporting members 43a and 43b and the body of the model airplane 30 is output. system. 2. The apparatus according to claim 1, wherein the support member driver (40)
A horizontal movement guide member 41 installed below the model runway 10 and installed entirely along the longitudinal direction of the runway and guiding horizontal movement of the moving block 42;
A moving block (42) supported by the horizontal movement guide member (41) so as to be able to move left and right, and supporting the first and second moving body supporting members (43a, 43b) so as to be able to move up and down;
The support members are supported by the moving block 42 so as to be vertically movable up and down. The support members are vertically installed on the ground so as to support the model airplane from the bottom. The support member detection sensors 31a and 31b First and second moving body supporting members 43a and 43b to which a magnet is attached for acting on the first and second moving body supporting members 43a and 43b;
First to third linear motor driving units 44a to 44c which are respectively controlled by the I / F automatic control unit 100 and independently drive the first to third linear motors;
A first linear motor driven by each of the linear motor driving units 44a through 44c to rotate forward and backward and to provide power for vertical movement of the first and second moving body supporting members 43a and 43b, And a third linear motor (LM3) for providing power for horizontally moving the moving block (42), wherein the first linear motor (LM1), the second linear motor (LM2) Landing automatic control system. The automatic landing / landing control system according to claim 8,
A key input unit 110 for user operation;
A wireless transmitting / receiving unit 120 for wireless communication with the moving body control unit 33 in the model airplane 30;
The infrared ray sensor 11 is directly connected to the infrared sensors 11a and 11b embedded in the model runway 10 to receive the position sensing signal of the model airplane 30 on the model runway 10, Receiving signal and a key input signal by a user operation to drive the wheel of the model airplane 30 or drive the support member driving body 40 to drive the model airplane 30 on the model hanging platform 20 And an i / landing control unit (130) for automatically controlling the operation and landing / landing operations on the model runway (10). 10. The navigation system according to claim 9, wherein the e-landing control unit (130)
The entire section of the model runway 10 is divided into a plurality of sections and the first and second moving body supporting members 43a and 43b are supported by the first linear motor LM1 and the second linear motor LM2, ) Of the model airplane (30) is controlled differently in each zone so that the inclination of the fuselage of the model airplane (30) is controlled differently for each zone within the section of the model runway (10) . 11. The apparatus according to claim 10, wherein the e-landing control unit (130)
The ascending speed of the second moving body supporting member 43b by the second linear motor LM2 is increased by the first linear motor LM1 to the end point of the model runway 10 during the take- Is increased stepwise higher than the ascending speed of the first moving body supporting member (43a) to increase the inclination of the body plane of the model airplane (30)
The lowering speed of the second moving body supporting member 43b by the second linear motor LM2 is lowered by the first linear motor LM2 toward the end point of the model runway 10 during the landing operation of the model airplane 30 Is lowered stepwise more than the descending speed of the first moving body supporting member (43a) to reduce the slope of the body plane of the model airplane (30). 10. The navigation system according to claim 9, wherein the e-landing control unit (130)
The entire section of the model runway 10 is divided into a plurality of zones and the horizontal movement speed of the moving block 42 by the third linear motor LM3 is controlled differently in each zone A model airplane landing / landing automatic control system. 13. The method according to claim 12, wherein the eco-landing control unit (130)
The horizontal movement speed of the moving block 42 by the third linear motor LM3 is increased stepwise to the end point of the model runway 10 during the take-off operation of the model airplane 30, Increasing the horizontal movement speed,
The horizontal movement speed of the moving block 42 by the third linear motor LM3 is gradually decreased as it moves to the end point of the model runway 10 during the landing operation of the model airplane 30, And the speed of the airplane is reduced. The automatic landing / landing control system according to claim 9,
Landing control unit 130 for selecting a sound source for take-off or landing and outputting the sound source for the output of the sound source, An acoustic driver 150;
And a plurality of lighting devices installed on the model runway 10 and a model hanging platform 20 at a position where lighting is required when taking off and landing the model airplane, And an illumination driving unit (160) for selectively driving each of the illumination devices.

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