KR102441077B1 - Apparatus for controlling taking off and landing of a dron in a vehicle and method thereof - Google Patents

Abstract

The present invention relates to an apparatus and method for controlling a drone landing in a vehicle, and when a drone is landed on a take-off and landing apparatus mounted on the roof of a vehicle, the intensity of magnetic force is adjusted according to the distance from the drone to turn the drone into a take-off and landing apparatus. An object of the present invention is to provide a vehicle drone landing control apparatus and method that can safely land a drone even while the vehicle is driving by safely guiding it.
To this end, the present invention provides a drone takeoff and landing control apparatus for a vehicle, comprising: a communication unit for transmitting vehicle location information as landing point information to a drone and receiving identification information of the drone; a distance measuring unit for measuring a separation distance from the drone; a magnetic force generating unit for generating a magnetic force; and a control unit that identifies whether the drone is a target drone, and controls the magnetic force generator to generate a magnetic force corresponding to a separation distance from the target drone if the drone is the target drone.

Description

Apparatus for controlling take-off and landing of a vehicle and a method therefor

The present invention relates to an apparatus for controlling take-off and landing of a vehicle and a method therefor, and more particularly, to a technology capable of safely taking-off and landing while a vehicle equipped with a drone take-off and landing apparatus on a roof is driving.

In recent years, various studies have been conducted on the use of small unmanned aerial vehicles such as multi-copters. Here, the unmanned aerial vehicle refers to a vehicle that can take off, fly, and land automatically to achieve a specific purpose without human intervention according to a programmed control method or a control signal transmitted from the outside, and is also called a drone. The use of drones is endless, from military reconnaissance drones to common fields such as unmanned camera and unmanned delivery service. In particular, with the development of technology, the weight of the drone itself has become lighter, the distance traveled has increased, and the role of the drone is becoming more diversified as various sensors are installed.

On the other hand, most vehicles are equipped with navigation, which makes it very easy to determine your current location or check the route to your destination. The navigation system not only provides route information, but also provides information on whether or not the flow of traffic is smooth, so the driver can control the operation of the vehicle according to the road conditions.

Most navigation systems can indicate the location of a car by receiving GPS position coordinates over time from GPS satellites. That is, various types of information are provided to the user based on the map information built into the navigation system and the signal transmitted from the satellite. In addition, some of the navigation systems include a function of providing a real-time CCTV image provided on the road to the driver through streaming for traffic condition monitoring.

However, the real-time CCTV image information available to drivers is extremely limited. First of all, the number of CCTVs installed on each road is not constant, and the driver cannot arbitrarily access all CCTVs to check the image. That is, access and control of non-related persons are strictly restricted except for CCTVs provided for public use. In addition, since most CCTVs have a fixed installation direction, a user cannot arbitrarily select an image in a desired direction. For this reason, there is currently no way to acquire video information, etc. near one's vehicle while driving through CCTV.

While the vehicle is being driven, there are many cases where the situation ahead of the vehicle's travel path is intriguing. For example, if a road that could be driven smoothly at a relatively high speed suddenly becomes congested due to an increase in vehicles, there is a possibility that an accident may occur in front of the vehicle. There are situations where

In the above situation, it would be very convenient if the drone mounted on the vehicle could take off itself, photograph the situation ahead with the camera mounted on the drone, and then check it in the vehicle in real time.

In addition, taking off an unmanned aerial vehicle while driving in a wide grassland or desert to check the surrounding situation, photographing a desired animal or spot, and checking it in real time, or launching an unmanned aerial vehicle from a vehicle loaded with tourists Taking pictures from the sky and providing them to see their driving behavior in real time will provide new businesses and markets.

In addition, in the case of an ambulance, a fire engine, or a military vehicle, it will be possible to use the drone for various purposes, such as sending an unmanned aerial vehicle in advance to check the situation of the destination or to seek cooperation from the destination personnel.

The technology underlying the utilization of the unmanned aerial vehicle as described above is a technology capable of taking off the unmanned aerial vehicle from a running vehicle and a technology of allowing the take-off unmanned aerial vehicle to land again in a vehicle.

In particular, there is a need for a technology that allows the drone to land in a vehicle in a safe and stable state even in a situation where the vehicle cannot be stopped for the landing of the drone, that is, the vehicle is running.

Republic of Korea Patent No. 10-1617594

The present invention can safely land the drone even while the vehicle is driving by safely guiding the drone to the take-off and landing device by adjusting the strength of magnetic force according to the distance from the drone when landing the drone on the take-off and landing device mounted on the roof of the vehicle. An object of the present invention is to provide an apparatus for controlling take-off and landing of a vehicle that can be used and a method therefor.

The objects of the present invention are not limited to the above-mentioned objects, and other objects and advantages of the present invention not mentioned may be understood by the following description, and will be more clearly understood by the examples of the present invention. It will also be readily apparent that the objects and advantages of the present invention may be realized by the means and combinations thereof indicated in the appended claims.

An apparatus of the present invention for achieving the above object, in an apparatus for controlling take-off and landing of a vehicle, includes: a communication unit for transmitting vehicle location information as landing point information to a drone and receiving identification information of the drone; a distance measuring unit for measuring a separation distance from the drone; a magnetic force generating unit for generating a magnetic force; and a control unit that identifies whether the drone is a target drone, and controls the magnetic force generator to generate a magnetic force corresponding to a separation distance from the target drone if the drone is the target drone.

The apparatus of the present invention may further include a memory for storing a table in which the strength of the magnetic force corresponding to the separation distance is recorded.

Here, the control unit may control the communication unit to transmit a control signal for generating a magnetic force to the target drone. In this case, the polarity of the magnetic force generated by the target drone is different from the polarity of the magnetic force generated by the magnetic force generating unit.

Also, after the target drone is identified, the control unit may activate the distance measuring unit to measure a separation distance from the target drone.

In addition, the controller may control the communication unit to periodically transmit the location information of the vehicle to the target drone when the vehicle is driving.

The method of the present invention for achieving the above object is a method for controlling take-off and landing of a vehicle drone, comprising: transmitting location information of the vehicle as landing point information to the drone; measuring a separation distance from the drone; identifying whether the drone is a target drone as the drone approaches; and generating a magnetic force corresponding to a separation distance from the target drone when the drone is a target drone.

The method of the present invention may further include storing a table in which the strength of the magnetic force corresponding to the separation distance is recorded.

The method of the present invention may further include transmitting a control signal for generating a magnetic force to the target drone. In this case, the polarity of the magnetic force generated by the target drone is different from the polarity of the magnetic force generated by the magnetic force generating unit.

Here, the step of measuring the separation distance may measure the separation distance from the target drone after the target drone is identified.

In addition, the transmitting of the location information may include periodically transmitting the location information of the vehicle to the target drone when the vehicle is driving.

According to the present invention, when the drone is landed on the take-off and landing device located on the roof of the vehicle, the strength of the magnetic force is adjusted according to the distance to the drone to safely guide the drone to the take-off and landing device, so that the drone can be operated even while the vehicle is driving. It has the effect of landing safely.

1 is a view showing an example of use of a drone according to an embodiment of the present invention;
2 is a configuration diagram of a drone according to an embodiment of the present invention;
3 is a configuration diagram of an embodiment of an apparatus for controlling take-off and landing of a vehicle according to the present invention;
4 is an exemplary view of a take-off and landing device for a drone according to the present invention;
5 is a side view of an embodiment of the take-off and landing apparatus for a drone according to the present invention;
6 is an exemplary view of a take-off process of a drone according to the present invention;
7 is an exemplary view of a landing process of a drone according to the present invention;
8 is a flowchart illustrating a method for controlling landing of a drone in a vehicle according to an embodiment of the present invention.

Hereinafter, some embodiments of the present invention will be described in detail with reference to exemplary drawings. In adding reference numerals to the components of each drawing, it should be noted that the same components are given the same reference numerals as much as possible even though they are indicated on different drawings. In addition, in describing the embodiment of the present invention, if it is determined that a detailed description of a related known configuration or function interferes with the understanding of the embodiment of the present invention, the detailed description thereof will be omitted.

In describing the components of the embodiment of the present invention, terms such as first, second, A, B, (a), (b), etc. may be used. These terms are only for distinguishing the elements from other elements, and the essence, order, or order of the elements are not limited by the terms. In addition, unless otherwise defined, all terms used herein, including technical or scientific terms, have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. Terms such as those defined in commonly used dictionaries should be interpreted as having a meaning consistent with the meaning in the context of the related art, and should not be interpreted in an ideal or excessively formal meaning unless explicitly defined in the present application. does not

1 is a view showing an example of use of a drone according to an embodiment of the present invention.

As shown in FIG. 1 , the drone 100 may be paired with a take-off and landing control device (not shown) provided in the own vehicle 200, and may be paired with the own vehicle 200 according to a user's manipulation or a preset operation method. It is possible to perform monitoring of the front situation of the own vehicle 200 while hovering in the upper direction space of the vehicle.

1 , it is assumed that a traffic light 400 exists in front of the own vehicle 200 , and preceding vehicles 201 and 202 exist between the traffic light 400 and the own vehicle 200 .

In the situation shown in FIG. 1 , the driver of the own vehicle 200 has no way of obtaining information on the traffic situation in front of the preceding vehicle 201 because of the preceding vehicle 201 blocking the view. In particular, as in the case of FIG. 1 , when the preceding vehicle 201 in front belongs to a large vehicle such as a truck or a bus, it is not easy to cope with unexpected unexpected situations because the situation in front of the vehicle cannot be known.

In the current navigation system, only information such as speed, driving route or area name is provided to the user. information is not provided

However, as in the case of FIG. 1 , when the own vehicle 200 is paired with the drone 100 equipped with various detection means, the user receives various information detected by the corresponding drone 100 to monitor the situation around the own vehicle 200 . can be checked easily. According to a preferred embodiment of the present invention, the drone 100 may include a camera capable of capturing still images and moving images as a detection means, and may transmit image information captured by the camera to the own vehicle 200 in real time. .

1, the thin solid line is a leader line va for indicating the viewing angle θ of the camera of the drone 100, and the dotted arrow 101 shows the flow of information between the drone 100 and the host vehicle 200. will be. According to an embodiment of the present invention, the drone 100 may be provided with a camera equipped with a wide-angle lens as a detection means, and in this case, may perform shooting in a wide field of view.

In addition, the drone 100 may be equipped with a plurality of cameras, and may obtain real-time image information for a plurality of directions and provide it to the driver. According to a preferred embodiment of the present invention, the driver may check the real-time image provided by the drone 100 through an output means such as a navigation screen of the own vehicle 200 .

According to the embodiment of FIG. 1 , the driver can immediately check the driving conditions of the first preceding vehicle 201 and the second preceding vehicle 202 and the traffic conditions in front, and the traffic lights 400 , obstacles on the road, and the road It is also possible to easily cope with special events such as an accident on the floor. That is, the drone 100 of FIG. 1 may be utilized as a solution for solving a blind spot in the driver's field of vision. It can be said that the drone 100 is meaningful in that it provides information that cannot be provided by the existing communication infrastructure.

Meanwhile, in the embodiment of FIG. 1 , the drone 100 is illustrated as a quadcopter including four propellers, but is not limited thereto, and may be provided with various types of aircraft.

2 is a block diagram of a drone 100 according to an embodiment of the present invention.

As shown in FIG. 2 , the drone 100 may include a control unit 110 , a power unit 120 , a communication unit 130 , a sensing unit 140 , and a magnetic force generating unit 150 . Depending on the method of carrying out the present invention, each component may be combined with each other and provided as one, and some components may be omitted depending on the method of carrying out the invention.

The control unit 110 performs overall control so that each of the components can perform their functions normally. The control unit 110 may be implemented in the form of hardware or software, or may exist in a form in which hardware and software are combined. Preferably, the control unit 110 may be provided with a microprocessor, but is not limited thereto.

The power unit 120 may perform movement and posture control of the drone 100 under the control of the controller 110 . The power unit 120 may be provided in various ways. According to a method of carrying out the present invention, the power unit 120 may be a jet engine emitting a jet stream, or a turboprop engine in which a propeller and a turbo engine are combined. However, according to a preferred embodiment of the present invention, the drone 100 may be a multi-copter including a plurality of propellers. In the case of a multicopter, attitude control in the air is advantageous compared to other types of unmanned aerial vehicles, and hovering that can maintain a continuous air flight state at a specific location at a specific altitude is also possible. In this case, the power unit 120 may include at least one propeller and driving means such as a motor for driving the propeller.

The communication unit 130 may perform wireless communication with an external communication device under the control of the control unit 110 . Here, the external communication device may include a wireless terminal such as a smart phone and a wireless communication base station as well as a car paired with the drone 100 and other drones. The communication unit 130 may perform wireless communication using not only short-range wireless communication methods such as visible light communication, infrared communication WiFi, and Bluetooth, but also communication methods such as WCDMA, EV-DO, HSDPA, and LTE.

In addition, the communication unit 130 may periodically receive the GPS location coordinates from the landing control device provided in the own vehicle 200 . Such GPS location coordinates are information indicating the location of the own vehicle 200 , and may be used as a landing point (loop of the own vehicle) of the drone 100 .

The control unit 110 may transmit various types of information generated by the sensing unit 140 to be described later to the own vehicle 200 through the communication unit 130, and may transmit a user's control signal transmitted through a wireless terminal such as a car or a smart phone. can receive According to a preferred embodiment of the present invention, the drone 100 can interwork with a navigation device mounted on the own vehicle 200 , and destination information stored in the navigation device through the communication unit 130 , route information, location information identified through GPS, etc. may be received from the own vehicle 200 . According to another embodiment, the drone 100 may receive vehicle control information such as acceleration, stopping, and direction change of the own vehicle 200 through the communication unit 130 .

The sensing unit 140 may sense the external environment of the drone 100 under the control of the control unit 110 . According to a preferred embodiment of the present invention, the sensing unit 140 may include an image capturing unit such as a camera and a sound sensing unit such as a microphone.

Also, depending on the method of carrying out the invention, the sensing unit 140 may include a plurality of cameras or a plurality of microphones.

In addition, the detection unit 140 of the drone 100 may include an infrared detection sensor, and through this, it is possible to easily sense an obstacle or ice on the road in a night situation, the temperature of an external environment and an object, and the like. On the other hand, according to the method of carrying out the present invention, the drone 100 includes a barometer, an altimeter, a gyroscope, an acceleration sensor that detects the movement speed, altitude, and degree of inclination of the drone 100 under the control of the control unit 110, It may include a pressure sensor and the like, and through this, it is possible to detect the moving speed, altitude, and degree of inclination of the drone 100 .

The magnetic force generating unit 150 is activated under the control of the controller 110 to generate a magnetic force. The magnetic force generating unit 150 may be implemented as an electromagnet. In this case, the control unit 110 may activate the magnetic force generating unit 150 in response to receiving an activation signal from the landing control device through the communication unit 130 . In addition, the control unit 110 may deactivate the magnetic force generating unit 150 according to its own determination or a command from the landing control device when the drone 100 is taking off.

Although the magnetic force generated by the magnetic force generating unit 150 is not large compared to the magnetic force generated by the landing device provided in the own vehicle 200 , it can help the drone 100 to safely land. Of course, the drone 100 does not need to include the magnetic force generating unit 150 according to the implementation method.

Although not shown in FIG. 2 , the drone 100 may further include a positioning unit (not shown) capable of grasping GPS location coordinates. Through this, the control unit 110 of the drone 100 can determine the GPS position coordinates of the drone 100 by itself without the help of the own vehicle 200 .

According to an embodiment of the present invention, in a drone that is paired with a vehicle and provides information to the vehicle, a sensing unit sensing the surrounding environment of the drone, transmits and receives information with an external communication device, and receives vehicle control information from the vehicle a communication unit and each unit of the drone, select an operating mode of the drone based on the received vehicle control information, sense the surrounding environment according to the operating mode through the sensing unit, and A drone comprising a control unit that extracts core information as a criterion for determining the surrounding situation from the environmental sensing result and transmits the information about the surrounding situation of the vehicle determined based on the core information to the vehicle through the communication unit can be provided have. Here, the vehicle control information may include measurement result data of a sensing means mounted on the vehicle and a control signal generated when a driver of the vehicle controls the vehicle.

3 is a configuration diagram of an apparatus for controlling take-off and landing of a vehicle for a vehicle according to the present invention.

As shown in FIG. 3 , the apparatus for controlling takeoff and landing of a vehicle according to the present invention includes a memory 30 , a communication unit 31 , a distance measurement unit 32 , a magnetic force generating unit 33 , and a control unit 34 . may include

Looking at each of the above components, first, the memory 30 can store various control logic (algorithms) necessary for landing or taking off the drone 100 in the take-off and landing device provided on the roof of the vehicle, and has its own. Location information (GPS location coordinates, etc.) of the own vehicle 200 acquired through a GPS receiver (not shown) or a navigation system provided in the own vehicle 200 may be stored. In this case, the location information is information indicating a landing point (loop of the own vehicle 200), and may be periodically updated when the own vehicle 200 is running.

In addition, the memory 30 may include a table in which the strength of the magnetic force according to the separation distance from the drone 100 is recorded. For example, in the table, a maximum magnetic force may be recorded when the distance from the drone 100 is 3 m, and a minimum magnetic force may be recorded when the distance to the drone 100 is 1 m. In this case, the intermediate values may be calculated based on the maximum value and the minimum value.

The memory 30 is a flash memory type, a hard disk type, a solid state disk type (SSD), a silicon disk drive type (SDD), and a multimedia card micro type. type), card type memory (such as SD or XD memory), random access memory (RAM), static random access memory (SRAM), read-only memory (ROM), electrically erasable programmable (EEPROM) It may include a storage medium of at least one type of a read-only memory), a programmable read-only memory (PROM), a magnetic memory, a magnetic disk, and an optical disk.

Next, the communication unit 31 provides a communication interface with the drone 100 , transmits various control signals for controlling the drone 100 to the drone 100 , and various data collected by the drone 100 . and a response signal corresponding to the control signal.

Also, the communication unit 31 may periodically transmit location information (eg, GPS location coordinates) of the own vehicle 200 to the drone 100 . Such GPS location coordinates may be used as landing location information (loop of the own vehicle 200) of the drone 100.

In addition, the communication unit 31 may identify the ID by communicating with the drone 100 close to the own vehicle 200 through, for example, a Bluetooth communication method. This is to identify whether the drone 100 is owned by the driver of the own vehicle 200 or not.

Next, the distance measuring unit 32 may be implemented as a radar sensor, an ultrasonic sensor, or the like, and measures a separation distance from the drone 100 hovering in the air of the own vehicle 200 .

Next, the magnetic force generating unit 33 may be implemented as an electromagnet, and generates a magnetic force under the control of the controller 34 . At this time, the polarity of the generated magnetic force is opposite to the polarity of the magnetic force generated by the magnetic force generating unit provided in the drone 100 . In other words, mutual attraction is generated. Depending on the case (such as shock mitigation at the time of landing), it may be implemented to generate a repulsive force.

In addition, the magnetic force generating unit 33 may adjust the strength of the magnetic force generated under the control of the controller 34 . For reference, the electromagnet is a magnet that is magnetized when current flows and returns to its original non-magnetized state when current is cut off, and the strength of magnetic force can be adjusted by adjusting the strength of the current.

Next, the control unit 34 performs overall control so that each of the components can perform their functions normally. The control unit 34 may be implemented as a microprocessor, but is not limited thereto.

In particular, the control unit 34 transmits the GPS location information of the own vehicle 200, that is, the landing point information of the drone 100 (eg, the loop of the own vehicle 200) to the drone 100 periodically. can control It is not necessary to periodically transmit when the vehicle is running and the vehicle is stopped.

Also, the controller 34 may identify the ID through Bluetooth communication with the drone 100 close to the own vehicle 200 .

In addition, if it is determined that the drone is a normal drone (owned by the driver of the own vehicle), the controller 34 may activate the distance measuring unit 32 to measure the separation distance from the drone 100 . In this case, the control unit 34 may transmit a control signal to the drone 100 through the communication unit 31 so that the drone 100 also generates a magnetic force.

In addition, the control unit 34 is based on the table in which the strength of the magnetic force according to the separation distance stored in the memory 30 is recorded, the magnetic force corresponding to the separation distance from the drone 100 measured by the distance measuring unit 32 . It is possible to control the magnetic force generating unit 33 to generate the. At this time, the polarity of the generated magnetic force is opposite to the polarity (direction of the magnetic field) of the magnetic force generated by the drone 100 . That is, when the drone 100 is landed, an attractive force is generated between the takeoff and landing device and the drone 100 .

As a result, the control unit 34 controls the strength of magnetic force when the drone 100 is landed on the take-off and landing device provided on the roof of the own vehicle 200 to land the drone 100, so that the vehicle can be safely landed even while the vehicle is running.

4 is an exemplary view of the take-off and landing apparatus for a drone according to the present invention.

As shown in FIG. 4 , the take-off and landing device 410 for a drone according to the present invention is mounted on the roof of the own vehicle 200, and in particular, it can be implemented so that the landed drone 100 can be introduced into the interior of the vehicle. . That is, the take-off and landing device 410 has a structure capable of moving the drone 100 into the interior of the vehicle so that a driver located inside the vehicle can receive the landing drone.

For example, a member (plastic having bending) connected to the roof of the own vehicle 200 is located at each corner of the landing pad on which the drone 100 lands. It can be implemented so that the landing pad is drawn into the interior of the vehicle while being withdrawn from the inside. In this case, when operating by manual operation, a handle may be provided on the vehicle side surface of the landing pad, and when operating by automatic operation, a motor may be provided to push the member.

5 is a side view of an embodiment of the take-off and landing apparatus for a drone according to the present invention.

As shown in FIG. 5 , the take-off and landing device 410 of the drone according to the present invention normally serves as the roof 420 of the vehicle, and when the drone takes off or lands, it is shown in FIGS. 6 and 7 below. performs the same function as the bar.

Hereinafter, a take-off and landing process of the drone will be described with reference to FIGS. 6 and 7 .

6 is an exemplary diagram of a take-off process of a drone according to the present invention.

As shown in (a) of FIG. 6 , the driver mounts the drone on the take-off and landing device moved to the interior of the vehicle. When the mounting of the drone is completed, the take-off and landing device automatically moves the drone to the outside of the vehicle as shown in FIG. At this time, magnetic force may be generated to prevent the drone from flying by the wind. Thereafter, the drone may be taken off as shown in (c) of FIG. 6 .

7 is an exemplary diagram of a landing process of a drone according to the present invention.

As shown in (a) of FIG. 7 , when the drone 100 moves near the take-off and landing device based on the GPS location information of the own vehicle 200, the control unit 34 communicates with the drone 100 to identify the ID. do.

If it is a normal drone, magnetic force is generated as shown in (b) of FIG. 7 to guide the drone to the take-off and landing device. At this time, the control unit 34 controls the magnetic force generating unit 33 to adjust the strength of the magnetic force based on the table in which the strength of the magnetic force according to the separation distance from the drone 100 is recorded.

After that, when the drone 100 lands, the take-off and landing device can move the drone 100 into the interior of the vehicle automatically or by a driver's button input or a driver's pulling force, as shown in FIG. 7(c). have.

8 is a flowchart illustrating a method for controlling landing of a drone in a vehicle according to an embodiment of the present invention.

First, the communication unit 31 transmits the vehicle location information as landing point information to the drone under the control of the control unit 34 (801). In this case, the location information may be GPS location coordinates.

Thereafter, the distance measuring unit 32 measures the separation distance from the drone under the control of the controller 34 ( 802 ). In this case, the distance measuring unit 32 may measure the separation distance using radar, ultrasonic waves, or the like.

Thereafter, the control unit 34 identifies whether the drone is a target drone as the drone approaches ( 803 ). In this case, the process of identifying whether the drone is a target drone may be performed through Bluetooth communication, and ID information may be used.

Thereafter, the magnetic force generating unit 33 generates a magnetic force corresponding to the separation distance from the target drone when the drone is the target drone under the control of the controller 34 ( 804 ). In this case, the magnetic force may be generated by an electromagnet.

Through this process, the drone can safely land while the vehicle is driving.

The above description is merely illustrative of the technical spirit of the present invention, and various modifications and variations will be possible without departing from the essential characteristics of the present invention by those skilled in the art to which the present invention pertains.

Therefore, the embodiments disclosed in the present invention are not intended to limit the technical spirit of the present invention, but to illustrate, and the scope of the technical spirit of the present invention is not limited by these embodiments. The protection scope of the present invention should be interpreted by the following claims, and all technical ideas within the scope equivalent thereto should be construed as being included in the scope of the present invention.

30: memory
31: communication department
32: distance measuring unit
33: magnetic force generating unit
34: control unit

Claims (12)

a communication unit for transmitting vehicle location information to the drone as landing point information and receiving identification information of the drone;
a distance measuring unit for measuring a separation distance from the drone;
a magnetic force generating unit for generating a magnetic force; and
A control unit that identifies whether the drone is a target drone, and controls the magnetic force generator to generate a magnetic force corresponding to a separation distance from the target drone if the drone is a target drone
A drone takeoff and landing control device for a vehicle comprising a.
The method of claim 1,
A memory that stores a table in which the strength of magnetic force corresponding to the separation distance is recorded
Drone takeoff and landing control device of the vehicle further comprising a.
The method of claim 1,
The control unit is
The apparatus for controlling take-off and landing of a vehicle, characterized in that the communication unit is controlled to transmit a control signal for generating a magnetic force to the target drone.
4. The method of claim 3,
The polarity of the magnetic force generated by the target drone is,
A drone takeoff and landing control device for a vehicle, characterized in that the polarity of the magnetic force generated by the magnetic force generating unit is opposite to each other.
The method of claim 1,
The control unit is
After the target drone is identified, the device for controlling take-off and landing of a vehicle, characterized in that the distance measuring unit is activated to measure a separation distance from the target drone.
The method of claim 1,
The control unit is
When the vehicle is driving, the apparatus for controlling the take-off and landing of a vehicle, characterized in that the communication unit controls the communication unit to periodically transmit the location information of the vehicle to the target drone.
transmitting vehicle location information to the drone as landing point information;
measuring a separation distance from the drone;
identifying whether the drone is a target drone as the drone approaches; and
If the drone is a target drone, generating a magnetic force corresponding to a separation distance from the target drone
A drone landing control method of a vehicle comprising a.
8. The method of claim 7,
Storing a table in which the strength of magnetic force corresponding to the separation distance is recorded
Drone landing control method of a vehicle further comprising a.
8. The method of claim 7,
Transmitting a control signal for generating a magnetic force to the target drone
Drone landing control method of a vehicle further comprising a.
10. The method of claim 9,
The polarity of the magnetic force generated by the target drone is,
A drone landing control method of a vehicle, characterized in that the polarity of the magnetic force is opposite to each other.
8. The method of claim 7,
Measuring the separation distance comprises:
After the target drone is identified, the drone landing control method for a vehicle, characterized in that measuring a separation distance from the target drone.
8. The method of claim 7,
Transmitting the location information includes:
When the vehicle is driving, the vehicle's drone landing control method, characterized in that periodically transmitting the location information of the vehicle to the target drone.

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