KR20170120475A - Apparatus and method for supporting flight of unmanned aerial vehicle - Google Patents

Abstract

A navigation support apparatus and method for an unmanned aerial vehicle are disclosed. A navigation support apparatus for an unmanned airplane according to the present invention includes a navigation target input unit for inputting a navigation target in the form of at least one of a target point coordinate and a waypoint of an unmanned airplane, A policy information input unit for inputting policy information for each domain, a domain setting unit for setting a domain that can be operated on the basis of the policy information for each domain, And an unmanned airplane control unit for controlling the operation of the unmanned airplane so that the unmanned airplane operates the unmanned airplane.

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to an apparatus and a method for operating an unmanned airplane,

TECHNICAL FIELD The present invention relates to a technology for supporting the operation of an unmanned airplane, and more particularly, to a technique for controlling the operation of an unmanned airplane based on various constraints on a three-dimensional space operated by an unmanned airplane.

The development of unmanned aircraft technology and the increase in demand are expected to increase the number of unmanned aerial vehicles, and various types of high performance unmanned aerial vehicles are being developed and released. Today, the development of more than 150kg military mid- to large-sized unmanned aerial vehicles has already been widely used in surveillance / reconnaissance beyond the prototype stage.

In the case of civilian small unmanned aerial vehicles, IT companies and logistics companies such as Google, Amazon, and Alibaba are starting various initiatives such as DJI in China and Parrot in France. As a result, legal and institutional discussions on unmanned aerial vehicles are in full swing.

In the future, if these civilian unmanned aerial vehicles enter the airspace of the airplane or enter the low - altitude area of the urban area to perform various missions, it is expected that restrictions on how the unmanned airplane should move in the three - dimensional space will be needed.

As with self-propelled vehicles, it is necessary to develop a technology for establishing a flight plan for unmanned aerial vehicles. The autonomous vehicle maps the precise map of the road and the GNSS / sensor information to identify the location of the vehicle and establish various travel plans according to the location of the vehicle. Thus, in the case of unmanned aerial vehicles, it is necessary to develop a technique for establishing a flight plan based on the constraints of the inflow route and the inflow route depending on the characteristics of each unmanned aerial vehicle.

In the existing aeronautical field, information on the way that a person must travel by himself is determined and operated through information such as communication with the base station on the ground and the altitude of the aircraft. Commercial unmanned aerial vehicles are also being developed for geofencing, which controls the operation area of the unmanned airplane through a communication base station on the ground or controls the inputted altitude and position in advance.

However, the technology for geofencing is based on GPS and it is aimed to suppress access based on the position of UAV, and it limits the speed, altitude and mission in specific area, . Therefore, in the environment where the speed, altitude and mission of the UAV must be restricted according to the characteristic of the downtown area or the main area, there are problems such as the security problem and the violation of the personal privacy protection law.

Therefore, it is necessary to develop technologies that can limit the speed, altitude and mission of unmanned aerial vehicles, depending on the characteristics of the area where the UAV is flying.

Korean Patent Laid-Open No. 10-2010-0016915, February 16, 2010 (name: flight control device of unmanned airplane and control method thereof)

SUMMARY OF THE INVENTION An object of the present invention is to enable safe operation of an unmanned airplane by controlling a navigation route of an unmanned airplane and a navigation system of an unmanned airplane.

Another object of the present invention is to control the navigation of an unmanned airplane by areas, thereby preventing an unspecified number of privacy infringements caused by the unmanned airplane and protecting personal information.

It is also an object of the present invention to enable smooth traffic flow with other aircraft by controlling the operation of the UAV.

According to another aspect of the present invention, there is provided an operation support device for an unmanned airplane, including: a navigation target input unit for inputting a navigation target in the form of at least one of a target point coordinate and a waypoint of an unmanned airplane; A policy information input unit for inputting policy information for each domain corresponding to the current location and the navigation target; a domain setting unit for setting a domain that can be operated on the basis of the policy information for each domain; And a control unit for controlling the operation of the unmanned airplane so that the unmanned airplane operates the unmanned airplane.

At this time, the zone setting unit may set the zone that can be operated based on at least one of the permitted zone information, the weight, the speed, the mission, and the charge information of the zone.

At this time, the navigation path generation unit may generate at least one of altitude, coordinates, speed and function of the unmanned aerial vehicle in the operable region based on at least one of three-dimensional path information, altitude information and surface information corresponding to the operable region And the constraint condition may be generated.

At this time, the policy information for the zone may include at least one of an altitude policy, a speed policy, and a function restriction policy of the UAV that is set for each type of the UAV in the region.

At this time, the altitude policy of the unmanned aerial vehicle may be set based on at least one of the weight of the unmanned air vehicle, the speed of the unmanned air vehicle, and the region.

At this time, the altitude policy set by the weight of the UAV may be set so that the altitude of the UAV is proportional to the weight of the UAV.

At this time, the altitude policy set by the speed of the UAV may be set so that the altitude of the UAV is proportional to the speed of the UAV.

At this time, the altitude policy set for each zone of the UAV may be set so that the altitude of the UAV is corresponding to at least one of a maximum speed limit and a minimum speed limit set for each zone.

At this time, the function restriction policy of the UAV may be to stop the operation of at least one of the photographing function and the recording function of the UAV when the region is a residence.

At this time, the speed policy of the unmanned airplane may allow the unmanned airplane to operate at a high speed if the unmanned airplane's mission is an emergency mission or the zone is a paid area.

Further, a method for supporting operation of an unmanned airplane performed by an operation supporting device of an unmanned airplane according to an embodiment of the present invention includes the steps of: (a) inputting at least one of a target point coordinate and a waypoint of the unmanned airplane; Inputting policy information for each zone corresponding to the current location of the UAV and the navigation target, setting a zone that can be operated based on the policy information for each zone, Generating a navigation route corresponding to the navigation target, based on the navigable area, and controlling navigation of the unmanned airplane so that the unmanned airplane operates the navigation route.

At this time, the step of setting the operable region may set the operable region based on at least any one of permitted region information, weight, speed, mission and charge information of the region.

At this time, the step of generating the navigation route corresponding to the navigation target may include: generating, based on at least any one of three-dimensional route information, altitude information and surface information corresponding to the navigable area, The altitude, the coordinates, the speed, and the function restriction conditions of the navigation path.

At this time, the policy information for the zone may include at least one of an altitude policy, a speed policy, and a function restriction policy of the UAV that is set for each type of the UAV in the region.

At this time, the altitude policy of the unmanned aerial vehicle may be set based on at least one of the weight of the unmanned air vehicle, the speed of the unmanned air vehicle, and the region.

At this time, the altitude policy set by the weight of the UAV may be set so that the altitude of the UAV is proportional to the weight of the UAV.

At this time, the altitude policy set by the speed of the UAV may be set so that the altitude of the UAV is proportional to the speed of the UAV.

At this time, the altitude policy set for each zone of the UAV may be set so that the altitude of the UAV is corresponding to at least one of a maximum speed limit and a minimum speed limit set for each zone.

At this time, the function restriction policy of the UAV may be to stop the operation of at least one of the photographing function and the recording function of the UAV when the region is a residence.

At this time, the speed policy of the unmanned airplane may allow the unmanned airplane to operate at a high speed if the unmanned airplane's mission is an emergency mission or the zone is a paid area.

According to the present invention, it is possible to support safe operation of an unmanned airplane by controlling the operation route of the unmanned airplane and the operation manner of the unmanned airplane.

Further, according to the present invention, by controlling the operation of the UAV by each zone, it is possible to prevent an unspecified number of privacy invasion due to the UAV, and protect personal information.

Further, according to the present invention, smooth traffic flow with other aircraft can be maintained by controlling the operation of the UAV.

FIG. 1 is a schematic view of an environment to which an operation supporting apparatus for an unmanned airplane according to an embodiment of the present invention is applied.
2 is a block diagram illustrating a configuration of an operation support device for an unmanned aerial vehicle according to an embodiment of the present invention.
3 is a flowchart illustrating a method for supporting navigation of an unmanned aerial vehicle according to an embodiment of the present invention.
4 is a diagram illustrating policy information stored in an air context DB according to an embodiment of the present invention.
5 is a diagram illustrating policy information for each domain according to an exemplary embodiment of the present invention.
6 is a block diagram illustrating a computer system in accordance with an embodiment of the present invention.

The present invention will now be described in detail with reference to the accompanying drawings. Hereinafter, a repeated description, a known function that may obscure the gist of the present invention, and a detailed description of the configuration will be omitted. Embodiments of the present invention are provided to more fully describe the present invention to those skilled in the art. Accordingly, the shapes and sizes of the elements in the drawings and the like can be exaggerated for clarity.

Hereinafter, preferred embodiments according to the present invention will be described in detail with reference to the accompanying drawings.

FIG. 1 is a schematic view of an environment to which an operation supporting apparatus for an unmanned airplane according to an embodiment of the present invention is applied.

As shown in FIG. 1, an operation support apparatus 200 of an unmanned airplane for supporting the operation of the UAV 100 may include at least one of a 3D air map 400 and an air context DB 500 One can communicate with the other.

First, the UAV 100 refers to a flight body manufactured to perform a designated mission without carrying an arbitrator such as an unmanned aerial vehicle (UAV) and a drone.

At this time, the unmanned airplane 100 may be a military purpose unmanned airplane equipped with various devices such as optical, infrared, and radar sensors, and performing tasks such as monitoring / reconnaissance, precision attack weapon induction, communication / information relay .

In addition, the UAV 100 may be a civilian UAV that is used for commercial, public, hobby, and the like. The UAV 100 may perform the task of delivering goods or perform emergency rescue missions, such as delivering relief items in a disaster area. The UAV 100 can be utilized for the purpose of building a wireless Internet network, an air map production business, or the like in the field of image shooting.

The public purpose UAV 100 may perform missions such as observing the fire, monitoring the criminals, border and coast guard, and watching illegal fishing boats. Also, the unmanned airplane 100 can be used for photographing or recording pictures for the purpose of personal hobbies.

Next, the navigation support device 200 of the unmanned airplane can receive the navigation goal in the form of at least one of a target point coordinate and a waypoint of the unmanned airplane. At this time, the operation support device 200 of the UAV can set the operation target of the UAV 100 from the control system 300.

The operation support device 200 of the unmanned airplane receives the policy information for each zone corresponding to the current location and operation target of the UAV 100. At this time, the operation support device 200 of the UAV can receive policy information from the air context DB 500. [

For example, when the navigation target for the current location A to B is set, the navigation support device 200 of the unmanned airplane can receive policy information on one or more regions corresponding to the route from A to B. [

The operation support apparatus 200 of the UAV, which receives the policy information, sets the region that can be operated using the policy information for each zone. Then, the navigation support device 200 of the UAV creates a navigation route corresponding to the navigation target based on the set operational areas.

The operation support device 200 of the UAV controls the operation of the UAV 100 so that the UAV 100 can operate the generated operation route. At this time, the operation support device 200 of the UAV can control the operation of the UAV 100 by transmitting a flight control signal to the flight control module mounted on the UAV 100. Here, the flight control module may refer to a module used for attitude control and flight control of the UAV 100.

The control system 300 can be implemented in the form of a general remote controller or a monitoring system, and sets the operation target of the UAV 100. At this time, the control system 300 can set the operation target in the form of at least one of the target point coordinate and the way point.

Next, the 3D Air Map (400) is used to provide navigation route information corresponding to the route that can be operated by the UAV 100, information supporting the operation of the UAV 100, To the device 200. At this time, the navigation route information may include at least one of three-dimensional path information, altitude information, and surface information.

Finally, the air context database (DB) 500 provides policy information on the region requested by the navigation support device 200 of the unmanned aerial vehicle.

The air context DB 500 includes at least one of an altitude policy by weight, an altitude policy by speed, an altitude policy by region, a speed policy by region, a speed and altitude policy by mission characteristic, a mission restriction policy by region, The above policy information can be stored. The policy information of the air context DB 500 will be described in more detail with reference to FIG. 4, which will be described later.

2 is a block diagram illustrating a configuration of an operation support device for an unmanned aerial vehicle according to an embodiment of the present invention.

2, the navigation support apparatus 200 of the UAV includes a navigation target input unit 210, a policy information input unit 220, a region setting unit 230, a navigation path generating unit 240, (250).

First, the navigation target input unit 210 receives a navigation target in the form of at least one of a target point coordinate and a waypoint of the UAV 100. At this time, the navigation target input unit 210 can receive the navigation target directly from the user who controls the UAV 100, or receive the navigation target from the control system.

The policy information input unit 220 receives policy information for each zone corresponding to the current position of the UAV 100 and the navigation target. At this time, the policy information input unit 220 can receive the respective policy information for one or more regions, and can receive the policy information from the air context DB.

Next, the domain setting unit 230 sets the domain that can be operated based on the policy information for each domain. At this time, the zone setting unit 230 can set a zone that can be operated based on at least one of permitted zone information, gas weight, speed, mission of the UAV 100, and charge information of the zone.

The navigation path generating unit 240 may generate a navigation path corresponding to the navigation target, based on the settable regions. At this time, the navigation route generating unit 240 can receive, from the 3D air map, the navigation route information corresponding to the region that can be operated. The navigation path information may include at least one of three-dimensional path information, altitude information, and surface information of the corresponding region. In addition, the navigation route generating unit 240 generates a navigation route including at least one of altitude, coordinates, speed, and function restriction conditions of the UAV 100 based on the navigation route information corresponding to the operational region .

Finally, the unmanned airplane control unit 250 controls the operation of the unmanned airplane 100 so that the unmanned airplane 100 operates the navigation path.

The unmanned airplane control unit 250 transmits a navigation route including at least one of altitude, coordinates, speed, and function restriction conditions of the unmanned airplane 100 to the unmanned airplane 100 to control the operation of the unmanned airplane 100 do.

Hereinafter, a method for supporting operation of an unmanned airplane performed by an operation supporting device of an unmanned airplane according to an embodiment of the present invention will be described in detail with reference to FIG. 3 through FIG.

3 is a flowchart illustrating a method for supporting navigation of an unmanned aerial vehicle according to an embodiment of the present invention.

First, the navigation support device 200 of the UAV receives input of a navigation target of the UAV 100 (S310).

The operation support device 200 of the UAV 100 receives the operation target in the form of at least one of a target point coordinate and a way point of the UAV 100. At this time, the navigation support device 200 of the UAV can receive the navigation target directly from the user or receive the navigation target from the control system.

In operation S320, the operation support device 200 of the UAV receives the current location of the UAV 100 and the policy information of each zone corresponding to the operation target.

At this time, the current position of the UAV 100 may be received from the UAV 100 or received from the control system. The operation support device 200 of the unmanned airplane receives policy information on one or more regions corresponding to the current position and the operation target of the unmanned airplane. Here, the navigation support device 200 of the UAV can receive policy information from the air context DB.

4 is a diagram illustrating policy information stored in an air context DB according to an embodiment of the present invention.

As shown in FIG. 4, the air context DB may store one or more policy information. Here, the policy information may mean that the altitude, speed, and restriction task of the gas are recorded by the type of the UAV in a specific region based on the GPS coordinates.

In particular, the air context DB may include at least one of an altitude policy by weight, an altitude policy by speed, an altitude policy by region, a speed policy by region, a speed and altitude policy by mission type, a mission restriction policy by region, Policy information can be stored.

For example, the altitude policy by weight may be set to fly at high altitude if the weight of the unmanned aerial vehicle is heavy, and to fly at low altitude if the weight of the aircraft is light. And the altitude policy according to the speed may be set to fly at high altitude if the speed of the UAV is fast and to fly at low altitude if the speed is low.

In addition, the altitude policy for each zone can set at least one of the maximum limit height and the minimum limit height of a specific zone so that the UAV 100 can fly in compliance with the limit height in the corresponding zone. And the regional speed policy may be set to at least one of a maximum speed and a minimum speed in a specific area.

The speed and altitude policy according to the mission characteristics allows at least one of the high speed flight and the low flight flight of the UAV 100 when the mission of the UAV 100 is an emergency mission such as rescue and relief delivering, ) May be configured to limit at least one of the high-speed flight and the low-altitude flight of the UAV 100 when the flight mission of the UAV 100 is for commercial use or is not an emergency mission.

Next, when the zone is restricted to a private residential area or a private place, the operation restriction of the cameras and microphones of the UAV 100 is stopped so that the UAV 100 can not perform shooting or recording in flight Can be set. In addition, the rate and altitude policy for each rate may be set to allow at least one of high-speed flight and low-altitude flight if the zone is a pay zone.

The AirContext DB may also include policies that restrict entry and entry into zones, and may limit the speed of unmanned aircraft when entering or advancing into that zone.

Next, the operation support apparatus 200 of the UAV sets up a domain that can be operated based on the policy information for each domain (S330).

The operation support device 200 of the unmanned airplane is operated based on at least any one of policy information on a zone, a navigation target, permitted zone information, the weight of the unmanned airplane 100, the weight, speed, Set the available regions.

At this time, the operation support apparatus 200 of the UAV can set a plurality of operational regions, and can select and set an optimal operational region among the plurality of operational regions.

5 is a diagram illustrating policy information for each domain according to an exemplary embodiment of the present invention.

As shown in FIG. 5, policy information may be set in each of a plurality of regions. For example, the policy information may not be set in the area A and the area B, and the area C may have the policy information related to the fee as the fee area.

Region D may have an altitude of 200 m or more, a maximum speed of 200 km / h, and image collection prohibition may be set as policy information, and Zone E may be set as a non-flying zone. In addition, Zone F may prohibit flights during emergency missions, prohibit flights during normal missions, Zone G may prohibit flights below 100 m altitude, and may limit the maximum speed to 20 km / h. Zone H allows the operation of an unmanned airplane (100) having a weight of 12 kg or more and less than 23 kg, an altitude of 100 m, and a minimum speed of 40 km / h of the unmanned airplane (100).

5, when the current position 510 and the target point coordinate (waypoint) 520 of the UAV 100 are set, the navigation support apparatus 200 of the UAV 100 determines whether or not the UAV 100 is a region A, region D, and region F to reach the target point coordinate 520. In this case,

In addition, the operation support device 200 of the UAV may set a region that can be operated so that the UAV 100 reaches the target point coordinates 520 through the zones B, C, H, and G.

In this manner, the operation support apparatus 200 of the UAV can set a plurality of operational regions based on the policy information set in each of the regions.

For example, when the unmanned airplane 100 performs an urgent task of delivering relief items, the operation support apparatus 200 of the unmanned airplane sets the region A, the region D, and the region F as the first operable region, The region B, the region C, the region H, and the region G as the second operable region.

Then, the navigation support apparatus 200 of the UAV can select a region that is optimal for at least one of the shortest time, the shortest distance, and the minimum cost among the first and the second operable regions.

On the other hand, when the UAV 100 performs the task of delivering the courier for commercial purposes, the operation support apparatus 200 of the UAV can set the region B, region C, region H, .

Referring back to FIG. 3, the navigation support apparatus 200 of the UAV 100 generates a navigation route corresponding to the navigation target of the UAV 100 (S340), based on the settable regions.

At this time, the navigation support apparatus 200 of the UAV can receive flight path information including at least one of three-dimensional path information, altitude information, and surface information from the 3D air map. And, the navigation support device 200 of the UAV can generate the navigation route of the UAV 100 based on the navigation route information corresponding to the area in which the navigation device can operate.

In addition, the navigation support apparatus 200 of the UAV can generate a navigation route including a waypoint in which at least one of altitude, coordinates, speed, and restriction conditions is defined.

For example, in step S330, when the navigation support device 200 of the unmanned airplane selects the area B, the area C, the area H, and the area G, The corresponding coordinates can be set as waypoints, and the altitude and speed of each UAV 100 can be set.

In addition, when a restriction condition such as prohibition of image collection is set in a specific area, the operation support device 200 of the unmanned airplane can not restrict the operation of the unmanned airplane 100 in the corresponding area You can set a defined waypoint.

The navigation support apparatus 200 of the unmanned aerial vehicle can generate a navigation route based on the operational areas corresponding to at least one of the unmanned airplane 100 and the navigation target among the plurality of the operational areas.

Finally, the operation support device 200 of the UAV controls the operation of the UAV 100 so that the UAV 100 operates the operation route (S350).

At this time, the operation support device 200 of the UAV can transmit the operation control signal for controlling the operation of the UAV 100 to the flight control module of the UAV 100 to control the operation of the UAV 100 have.

Here, the navigation control signal includes at least one of altitude, direction, coordinates, speed, and function restriction conditions of the UAV 100 corresponding to the navigation route, waypoint information, and navigation route corresponding to the UAV 100 .

The function limiting condition may include an operation control signal of a sensor (a camera, a microphone, etc.) of the UAV 100. The operation support device 200 of the UAV may use an operation control signal of the sensor to control the operation of the UAV 100) to perform the operation corresponding to the function restriction condition.

As described above, the navigation support apparatus 200 for an unmanned airplane according to an embodiment of the present invention includes a navigation chip including the precision map for the navigation target and the policy information for the area, and the navigation chip for the unmanned airplane 100 100) can be provided.

Thus, the navigation support apparatus 200 of the unmanned airplane supports the operation of the unmanned airplane 100 so as to operate in accordance with the information of the unmanned airplane 100 and the policy information of the unmanned airplane 100 in the space where the unmanned airplane 100 is flying Or control. In addition, the navigation support apparatus 200 of the UAV can systematically manage the UAVs 100.

6 is a block diagram illustrating a computer system in accordance with an embodiment of the present invention.

Referring to FIG. 6, embodiments of the present invention may be implemented in a computer system 600, such as a computer readable recording medium. 6, the computer system 600 includes one or more processors 610, a memory 630, a user input device 640, a user output device 650, and a storage 630, which communicate with one another via a bus 620. [ 660 < / RTI > In addition, the computer system 600 may further include a network interface 670 connected to the network 680. The processor 610 may be a central processing unit or a semiconductor device that executes the processing instructions stored in the memory 630 or the storage 660. [ Memory 630 and storage 660 may be various types of volatile or non-volatile storage media. For example, the memory may include a ROM 631 or a RAM 632. [

Thus, embodiments of the invention may be embodied in a computer-implemented method or in a non-volatile computer readable medium having recorded thereon instructions executable by the computer. When computer readable instructions are executed by a processor, the instructions readable by the computer are capable of performing the method according to at least one aspect of the present invention.

As described above, the apparatus and method for supporting the operation of the UAV according to the present invention are not limited to the configuration and method of the embodiments described above, but the embodiments can be applied to various implementations All or some of the examples may be selectively combined.

100: Unmanned aircraft
200: Operation support device of unmanned airplane
210: Navigation target input unit
220: Policy information input unit
230:
240: Navigation path generating unit
250: Unmanned aerial vehicle control unit
300: Control system
400: 3D Air Map
500: Air Context DB
600: Computer system
610: Processor
620: bus
630: Memory
631: Rom
632: RAM
640: User input device
650: User output device
660: Storage
670: Network interface
680: Network

Claims (20)

A navigation target input unit for inputting a navigation target in the form of at least one of a target point coordinate and a waypoint of the UAV,
A policy information input unit for inputting policy information for each zone corresponding to the current position of the UAV and the navigation target,
A domain setting unit for setting a domain that can be operated on the basis of the policy information for each domain,
A navigation route generating unit for generating a navigation route corresponding to the navigation target based on the set operational area,
The unmanned airplane control unit controls the operation of the unmanned airplane so that the unmanned airplane operates the navigation path
Wherein the navigation device is a navigation device. The method according to claim 1,
The region setting unit,
And sets the operable region based on at least any one of the permitted zone information, the weight, the speed, the mission of the unmanned airplane, and the charge information of the zone. The method according to claim 1,
Wherein the navigation path generating unit comprises:
Coordinates, speed, and function limitation conditions of the unmanned aerial vehicle in the operable region based on at least any one of three-dimensional path information, altitude information, and surface information corresponding to the operable region The navigation system comprising: The method according to claim 1,
The policy information for the domain includes,
And an altitude policy, a speed policy, and a function restriction policy of the unmanned airplane set for each type of the unmanned airplane in the region. 5. The method of claim 4,
The altitude policy of the unmanned aerial vehicle is,
The speed of the unmanned airplane, the speed of the unmanned airplane, and the region. 6. The method of claim 5,
The altitude policy set for each weight of the unmanned aerial vehicle,
Wherein the height of the unmanned airplane is set to be proportional to the weight of the unmanned airplane. 6. The method of claim 5,
The altitude policy set for each speed of the UAV is,
Wherein the altitude of the unmanned airplane is set to be proportional to the speed of the unmanned airplane. 6. The method of claim 5,
The altitude policy set for each zone of the unmanned aerial vehicle is,
Wherein the altitude of the unmanned aerial vehicle is set to correspond to at least one of a maximum speed limit and a minimum speed limit set for each of the zones. 5. The method of claim 4,
The functional restriction policy of the unmanned aerial vehicle,
Wherein the controller controls to stop the operation of at least one of the photographing function and the recording function of the unmanned airplane when the area is a residence. 5. The method of claim 4,
The speed policy of the UAV,
Wherein the unmanned airplane allows the unmanned airplane to operate at a high speed when the mission of the unmanned airplane is an emergency mission or when the area is a toll area. A method for supporting operation of an unmanned airplane performed by an operation support device of an unmanned airplane,
Receiving a navigation target in the form of at least one of a target point coordinate and a waypoint of the UAV;
Receiving policy information for each zone corresponding to the current location of the UAV and the navigation target;
Setting a domain that can be operated based on the policy information for each domain,
Generating a navigation route corresponding to the navigation target, based on the set navigable area, and
Controlling the operation of the unmanned airplane so that the unmanned airplane operates the navigation path
Wherein said method comprises the steps of: 12. The method of claim 11,
Wherein the setting of the operable region comprises:
And setting the operable region based on at least any one of authorized zone information, weight, speed, mission of the unmanned airplane, and charge information of the zone. 12. The method of claim 11,
Wherein the step of generating a navigation route corresponding to the navigation target comprises:
Coordinates, speed, and function limitation conditions of the unmanned aerial vehicle in the operable region based on at least any one of three-dimensional path information, altitude information, and surface information corresponding to the operable region Wherein the navigation system is operable to generate the navigation route. 12. The method of claim 11,
The policy information for the domain includes,
A speed policy, and a function restriction policy of the unmanned airplane set for each type of the unmanned airplane in the region. 15. The method of claim 14,
The altitude policy of the unmanned aerial vehicle is,
The speed of the unmanned airplane, the speed of the unmanned airplane, and the region. 16. The method of claim 15,
The altitude policy set for each weight of the unmanned aerial vehicle,
Wherein the altitude of the unmanned airplane is set to be proportional to the weight of the unmanned airplane. 16. The method of claim 15,
The altitude policy set for each speed of the UAV is,
Wherein the elevation of the unmanned airplane is set to be proportional to the speed of the unmanned airplane. 16. The method of claim 15,
The altitude policy set for each zone of the unmanned aerial vehicle is,
Wherein the altitude of the unmanned aerial vehicle is set to correspond to at least one of a maximum speed limit and a minimum speed limit set for each of the areas. 15. The method of claim 14,
The functional restriction policy of the unmanned aerial vehicle,
Wherein the controller controls to stop the operation of at least one of the photographing function and the recording function of the unmanned airplane when the area is a residence. 15. The method of claim 14,
The speed policy of the UAV,
Wherein the unmanned airplane permits high speed operation of the unmanned airplane when the mission of the unmanned airplane is an emergency mission or when the region is a charged area.

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