阅读说明：本技术 旋翼机着陆装置 (Landing device of gyroplane ) 是由 铃木阳一 于 2015-07-06 设计创作，主要内容包括：搭载有货物的无人机(1)从起飞装置(11)起飞,并将该货物的送货地即用户住宅(20)作为其目的地使用GPS系统进行飞行。而且,当无人机(1)接近目的地即用户住宅时,无人机(1)的飞行从使用GPS系统的自主导航切换至通过设置在该用户住宅(20)的着陆装置(21)以及住宅内控制装置(22)进行远程控制的方式。通过着陆装置(21)以及住宅内控制装置(22)的远程控制来使无人机(1)着陆在着陆装置(21)并将货物(50)分离开后,无人机(1)使用GPS系统返回至仓库(10)而着陆于起飞装置(11)。(An unmanned aerial vehicle (1) loaded with a cargo takes off from a take-off device (11), and flies with the delivery site of the cargo, namely a user house (20), as the destination thereof by using a GPS system. When the unmanned aerial vehicle (1) approaches a user house, which is the destination, the flight of the unmanned aerial vehicle (1) is switched from autonomous navigation using a GPS system to a mode of remote control by a landing device (21) and an in-house control device (22) provided in the user house (20). After the unmanned aerial vehicle (1) is landed on the landing device (21) and the goods (50) are separated by remote control of the landing device (21) and the in-house control device (22), the unmanned aerial vehicle (1) returns to the warehouse (10) by using a GPS system and lands on the take-off device (11).)

1. A gyroplane landing apparatus comprising:

a landing portion for gyroplane landing;

a position identification portion for identifying a position of the rotorcraft relative to the landing portion; and

a remote control section that remotely controls the gyroplane such that the gyroplane having no photographing function lands on the landing section based on a recognition result obtained by the position recognition section,

the landing part is provided at a position higher than the living space of the house.

2. The gyroplane landing gear according to claim 1, further comprising an opening/closing mechanism including said landing part,

the land portion is formed at a portion that becomes an inner side when the opening and closing mechanism is closed; when the opening/closing mechanism is opened, the landing part is in a horizontal posture at a position where the upper space is opened.

3. The gyroplane landing gear according to claim 1, comprising an opening and closing mechanism,

when the opening and closing mechanism is closed, the landing part is accommodated in the inner space; when the opening and closing mechanism is opened, the upper space of the land portion is opened.

4. A gyroplane landing gear according to claim 2 or 3, wherein the landing gear comprises a movable member,

the movable member is capable of assuming a first posture extending vertically upward from the periphery of the land portion and a second posture extending further outward and upward from the periphery of the land portion,

when the opening/closing mechanism is closed, the movable member takes the first posture;

when the opening/closing mechanism is opened and the rotorcraft lands on the landing portion, the movable member takes the second posture.

5. A rotorcraft landing gear according to claim 4,

the movable member is capable of moving a load, which is separated from the rotorcraft that has landed on the land portion, toward a position near the center of the land portion in a state of being in contact with the load.

6. A rotorcraft landing gear according to any one of claims 1 to 5, wherein,

the position recognition unit has imaging units provided at a plurality of positions of the landing unit, and recognizes a position of the rotorcraft relative to the landing unit based on an imaging result of the imaging units.

7. A rotorcraft landing gear according to any one of claims 1 to 6, wherein,

a distance measuring unit for measuring the distance from the landing unit to the gyroplane,

the remote control unit controls the lowering speed of the rotorcraft based on the measurement result measured by the distance measurement unit.

8. A rotorcraft landing gear according to any one of claims 1 to 7, wherein,

the remote control unit acquires identification information of the gyroplane from a gyroplane approaching the landing part, remotely controls the gyroplane to land the gyroplane on the landing part when the acquired identification information matches identification information of a gyroplane allowed to land on the landing part, and does not perform remote control when the acquired identification information does not match the identification information of the gyroplane allowed to land on the landing part.

9. A rotorcraft landing gear according to any one of claims 1 to 8, including a lifting mechanism,

the lifting mechanism can carry the goods received from the gyroplane landed on the landing part, descend to the living space of people, and can ascend to the position for receiving the goods again.

10. A gyroplane landing apparatus comprising:

a landing portion for gyroplane landing;

a position identification portion for identifying a position of the rotorcraft relative to the landing portion; and

a remote control section that remotely controls the gyroplane such that the gyroplane having no photographing function lands on the landing section based on a recognition result obtained by the position recognition section,

the land portion is a rectangular area,

the position recognition portions are disposed in the vicinity of the center of the land portion and in the vicinity of the edge of the land portion, respectively.

11. The gyroplane landing gear according to claim 11,

the position recognition unit is a plurality of infrared cameras which are arranged in the vicinity of the center of the land portion and the vicinity of the edge of the land portion, respectively, and which are on the diagonal line of the rectangle.

12. The gyroplane landing gear according to claim 11, further comprising an opening and closing mechanism including said landing part,

the land portion is formed at a portion that becomes an inner side when the opening and closing mechanism is closed; when the opening/closing mechanism is opened, the landing part is in a horizontal posture at a position where the upper space is opened.

13. The gyroplane landing gear according to claim 11, comprising an opening and closing mechanism,

when the opening and closing mechanism is closed, the landing part is accommodated in the inner space; when the opening and closing mechanism is opened, the upper space of the land portion is opened.

14. A rotorcraft landing gear according to claim 12 or claim 13, including a movable member,

the movable member is capable of assuming a first posture extending vertically upward from the periphery of the land portion and a second posture extending further outward and upward from the periphery of the land portion,

when the opening/closing mechanism is closed, the movable member takes the first posture;

when the opening/closing mechanism is opened and the rotorcraft lands on the landing portion, the movable member takes the second posture.

15. The gyroplane landing gear according to claim 14,

the movable member is capable of moving a load, which is separated from the rotorcraft that has landed on the land portion, toward a position near the center of the land portion in a state of being in contact with the load.

16. A rotorcraft landing gear according to any one of claims 10 to 15, wherein,

the position recognition unit has imaging units provided at a plurality of positions of the landing unit, and recognizes a position of the rotorcraft relative to the landing unit based on an imaging result of the imaging units.

17. A rotorcraft landing gear according to any one of claims 10 to 16, wherein,

a distance measuring unit for measuring the distance from the landing unit to the gyroplane,

the remote control unit controls the lowering speed of the rotorcraft based on the measurement result measured by the distance measurement unit.

18. A rotorcraft landing gear according to any one of claims 10 to 17, wherein,

the remote control unit acquires identification information of the gyroplane from a gyroplane approaching the landing part, remotely controls the gyroplane to land the gyroplane on the landing part when the acquired identification information matches identification information of a gyroplane allowed to land on the landing part, and does not perform remote control when the acquired identification information does not match the identification information of the gyroplane allowed to land on the landing part.

19. A rotorcraft landing gear according to any one of claims 10 to 18, including an elevator mechanism,

the lifting mechanism can carry the goods received from the gyroplane landed on the landing part, descend to the living space of people, and can ascend to the position for receiving the goods again.

20. A rotorcraft landing gear according to any one of claims 10 to 19, wherein,

the gyroplane landing gear is disposed at a position higher than the living space of the people.

Technical Field

The invention relates to a landing device for the landing of a rotorcraft.

Background

Small and lightweight gyroplanes called drones (drones) or multi-rotor helicopters (multicopters) are mainly used for aerial photography, but are also considered to be applied to, for example, distribution of goods in addition to such an application. Patent document 1 discloses a system for distributing cargo by a rotorcraft.

Documents of the prior art

Patent document

Patent document 1: U.S. patent application publication No. 2015/0120094 specification

Disclosure of Invention

(problems to be solved by the invention)

Here, in general, a camera (camera) is mounted on such a rotorcraft, and the rotorcraft can automatically land at a destination by recognizing a terrain or a building based on an image captured by the camera. However, if the surrounding environment can be freely photographed from the air, there is a problem that the portrait right and privacy right of a person included in a photographed image cannot be properly protected. Therefore, it is desirable to apply a rotorcraft that does not have a shooting function.

It is therefore an object of the present invention to provide a solution for landing a rotorcraft that does not have a camera function at a destination.

(means for solving the problems)

In order to solve the above problem, the present invention provides a rotorcraft including: a landing portion for gyroplane landing; a position identification portion for identifying a position of the rotorcraft relative to the landing portion; and a remote control unit that remotely controls the gyroplane so that the gyroplane having no imaging function lands on the landing unit, based on the recognition result obtained by the position recognition unit.

The landing device of the rotorcraft according to the present invention may include an opening/closing mechanism including the landing portion, the landing portion being formed in a portion that is inside when the opening/closing mechanism is closed; when the opening/closing mechanism is opened, the landing part is in a horizontal posture at a position where the upper space is opened.

The landing device of the rotorcraft according to the present invention may include an opening/closing mechanism that, when closed, houses the landing unit in an internal space; when the opening and closing mechanism is opened, the upper space of the land portion is opened.

The gyroplane landing apparatus according to the present invention may include a movable member capable of assuming a first posture extending vertically upward from the periphery of the land portion and a second posture extending further outward and upward from the periphery of the land portion, wherein the movable member assumes the first posture when the opening and closing mechanism is closed; when the opening/closing mechanism is opened and the rotorcraft lands on the landing portion, the movable member takes the second posture.

In the landing device for a rotorcraft according to the present invention, the movable member may be configured to be capable of moving a load, which is separated from the rotorcraft that has landed on the landing portion, toward a position near the center of the landing portion in a state of contact with the load.

In the gyroplane landing apparatus according to the present invention, the position recognition unit may include an imaging unit provided at a plurality of positions of the landing unit, and may recognize the position of the gyroplane with respect to the landing unit based on an imaging result of the imaging unit.

The landing apparatus for a rotorcraft according to the present invention may further include a distance measuring unit that measures a distance from the landing unit to the rotorcraft, and the remote control unit may control a descent speed of the rotorcraft based on a measurement result measured by the distance measuring unit.

In the gyroplane landing apparatus according to the present invention, the remote control unit may acquire identification information of the gyroplane from a gyroplane approaching the landing part, and when the acquired identification information matches identification information of a gyroplane allowed to land on the landing part acquired in advance, the remote control unit may remotely control the gyroplane to land the gyroplane on the landing part, and when the acquired identification information does not match the identification information, the remote control unit may not perform the remote control.

The gyroplane landing apparatus according to the present invention may further include a lifting mechanism which is capable of carrying the cargo received from the gyroplane landed on the landing part, lowering the cargo to a living space of people, and raising the cargo again to a position where the cargo is received

The landing gear of the rotorcraft according to the present invention may be installed at a position higher than the living space of people.

Drawings

Fig. 1 is a block diagram showing a configuration of a distribution system according to an embodiment of the present invention.

Fig. 2 is an exemplary diagram of the route DB according to the embodiment.

Fig. 3 is a diagram showing an example of the drone DB according to the embodiment.

Fig. 4 is a plan view of the land portion according to the embodiment.

Fig. 5 is a side view of the land portion according to the embodiment.

Fig. 6 is a side view of the landing gear according to this embodiment.

Fig. 7 is a sequence diagram of the entire system according to this embodiment.

Fig. 8 is a side view of a landing gear according to a modification.

Detailed Description

[ embodiment ]

Fig. 1 is a block diagram showing a configuration of a distribution system according to an embodiment of the present invention. In the present embodiment, a rotorcraft (hereinafter, referred to as an unmanned aerial vehicle) capable of carrying a load will be described as an example. The unmanned aerial vehicle 1 includes a rotor, a motor for rotating the rotor, a control device for controlling these, a battery for supplying electric power to these, a communication unit for performing wireless communication for remote control, a 6PS (global Positioning System) System as a position measurement mechanism, a level gauge for grasping the posture of the unmanned aerial vehicle, various sensors (none of which are shown), and the like, but does not need to have an imaging function. Although the GPS system is a position acquisition mechanism necessary for the unmanned aerial vehicle 1 to autonomously fly to a destination, for example, a system in which the unmanned aerial vehicle flies while grasping its position based on beacons (beacons) emitted from a plurality of base stations installed on the ground may be used instead of the GPS system.

The warehouse 10 houses therein a plurality of goods 50 to be delivered by the drone 1. A take-off device 11 is provided in the warehouse 10, and the take-off device 11 is used for taking off in a state where the unmanned aerial vehicle 1 carries the cargo 50 (specifically, in a state where the cargo 50 is suspended below the unmanned aerial vehicle 1).

The in-warehouse control device 12 provided in the warehouse 10, the in-house control device 22 provided in the user house 20, and the management system 30 provided in the facility of the administrator of the system are all computers (computers) having a cpu (central Processing unit), a memory, a mass storage device, a communication interface, and the like. The management system 30 performs management related to the distribution of the cargo 50 by the drone 1. The in-warehouse control device 12, the in-home control device 22, and the management system 30 are connected by a communication network 40 including a wired communication line or a wireless communication line, and can communicate with each other. The in-warehouse control device 12 and the in-home control device 22 are provided with a communication unit that performs wireless communication for remote control with the unmanned aerial vehicle 1.

The unmanned aerial vehicle 1 loaded with the cargo takes off from the takeoff device 11, and flies using the GPS system with the destination of the delivery site of the cargo, i.e., the user house 20. When the unmanned aerial vehicle 1 approaches the user house, which is the destination, the flight of the unmanned aerial vehicle 1 is switched from autonomous navigation using the GPS system to remote control by the landing device 21 and the in-house control device 22 provided in the user house 20. By remote control from the landing gear 21 and the in-house control device 22, the drone 1 lands on the landing gear 21 and separates the cargo 50, and then returns to the warehouse 10 using the GPS system and lands on the takeoff device 11.

An airline database (hereinafter, database is referred to as DB)3, a drone DB32, and a weather DB33 are stored in the mass storage device of the management system 30. As shown in fig. 2, in the air route DB31, the unmanned aerial vehicle 1D of the unmanned aerial vehicle 1 in flight or expected to fly corresponds to the air route data, wherein the unmanned aerial vehicle 1D is identification information assigned to each unmanned aerial vehicle 1; the route data is a route representing the unmanned aerial vehicle 1 from the origin to the destination. The flight path data includes position data representing each position on the flight path, and an expected time at which the drone passes the position. As shown in fig. 3, in the drone DB32, the drone lD of each drone 1 corresponds to the cargo 1D assigned to the cargo 50 to be delivered by the drone 1, and further corresponds to the attribute information of the battery mounted on the drone 1, the attribute information of the battery including the battery lD as the identification information of the battery, the amount of charge thereof, and the like. The cargo 1D corresponding to the drone lD of the drone 1 in flight or expected to be flying is blank (blank). The weather DB33 contains weather data for each location provided by, for example, a weather bureau.

The landing apparatus 21 includes: a landing part for landing of the unmanned aerial vehicle 1; and a lifting mechanism for transporting the cargo 50 separated from the unmanned aerial vehicle 1 landed on the landing part to the living space of the user. Of these landing portions and the lifting mechanism, fig. 4 is a plan view of the landing portion 210, particularly when viewed from vertically above. Fig. 4 is a diagram of the movable plates 215a, 215b, and 215c in the second posture.

The shape of the landing part 210 when viewed from vertically above is a rectangular area larger than the upper limit size of the cargo 50. A plurality of (here, three) infrared cameras 211 provided on the upper surface of the land portion 210 are imaging portions that respectively image vertically above the land portion 210. The in-house control device 22 recognizes the position of the unmanned aerial vehicle 1 with respect to the landing part 210 based on the captured image, and remotely controls the unmanned aerial vehicle 1 through the communication part based on the recognition result so that the unmanned aerial vehicle 1 lands on the landing part 210. When the unmanned aerial vehicle 1 is about to land (for example, the height from the land portion 210 is 50cm or less), since the infrared camera 211 near the center of the land portion 210 captures the cargo 50 (the entire field of view is the cargo 50) in full, the accuracy of identifying the position of the unmanned aerial vehicle 1 may be reduced. Then, the in-home control device 22 performs remote control of the unmanned aerial vehicle 1 based on the captured images of the plurality of (here, two) infrared cameras 211 arranged on the diagonal lines of the rectangle close to the edge of the land portion 210. That is, the infrared camera 211 and the in-house control device 22 function as a position recognition unit that recognizes the position of the unmanned aerial vehicle 1 with respect to the land portion 210 based on the result of imaging by the infrared camera 211. The in-home control device 22 and the communication unit function as a remote control unit that remotely controls the unmanned aerial vehicle 1 based on the recognition result of the position recognition unit so that the unmanned aerial vehicle 1 that does not have the imaging function lands on the landing unit 210.

In this way, in the vicinity of the user house 20, the unmanned aerial vehicle 1 does not autonomously land on the landing gear 21 but remotely controls the unmanned aerial vehicle 1 from the landing gear 21, and therefore the unmanned aerial vehicle 1 does not need to have an imaging function for flight control. Further, although it is sometimes difficult for an unmanned aerial vehicle that recognizes its own position using a GPS system and flies to a destination by itself to automatically land in an environment where GPS signals are difficult to reach, such as between buildings, in the present embodiment, automatic landing is easily performed even in such an environment by remotely controlling the unmanned aerial vehicle by the landing gear 21 during landing.

The distance measuring section 213 provided on the upper surface of the landing section 210 is used to measure the distance between the drone 1 and the landing section 210. The in-house control device 22 controls the descending speed of the unmanned aerial vehicle 1 based on the measurement result of the distance measurement unit 213. If the distance measuring unit 213 is provided on the unmanned plane side, the distance from the unmanned plane to an obstacle near the landing unit 210 may be erroneously detected, but if the landing unit 210 includes the distance measuring unit 213, the possibility of such erroneous detection is low. In addition, although the distance measuring unit 213 may measure the distance from the landing unit 210 to a nearby building such as an electric wire, for example, in this case, the distance measuring unit 213 may be set and registered to exclude the influence of the building when the landing device 21 is installed.

The image captured by the camera 214 is supplied to a display device (not shown) of the user house 20 via a communication line, or is supplied to a portable terminal (not shown) of a user living in the user house 20 and a display device (not shown) of the management system 30 via the in-house control device 22 and the communication network 40. Accordingly, the user and the operator of the management system 30 can visually confirm the landing of the unmanned aerial vehicle 1. At this time, since the camera 214 captures images vertically above the land device 21, that is, in the sky direction, there is little possibility that images having problems such as portrait right and privacy right are captured.

Movable plates 215a, 215b, and 215c as movable members are provided in the vicinity of the landing portion 210 in three directions (a direction of separating from the cylindrical body 230 described later and two directions orthogonal to the direction of separating). The vertically lower end portions of the movable plates 215a, 215b, and 215c are rotatably attached to the end portions of the three sides of the land portion 210. These movable plates 215a, 215b, and 215c are capable of assuming a first posture in which the movable plates 215a, 215b, and 215c extend vertically upward from the periphery of the land portion 210, and a second posture in which the movable plates 215a, 215b, and 215c extend further outward and upward from the periphery of the land portion 210, under the control of the in-house control device 22.

Fig. 5(a) is a side view of the movable plates 215a, 215b, and 215c in the first posture as viewed in the direction of the arrow a in fig. 4, and fig. 5(b) is a side view of the movable plates 215a, 215b, and 215c in the second posture as viewed in the direction of the arrow a in fig. 4. When the drone 1 lands, the movable plates 215a, 215b, and 215c assume the second posture (fig. 4 and 5 (b)). Accordingly, the entire landing part 210 has a funnel shape that is spread upward, and the cargo 50 loaded on the drone 1 is easily received.

On the other hand, in a state where the cargo 50 is separated from the unmanned aerial vehicle 1 toward the land portion 210, the movable plates 215a, 215b, and 215c take the first posture (fig. 5(c)), and function as a mechanism for preventing the cargo 50 from falling due to gusts of wind and the like. After the load 50 is separated, the movable plates 215a and 215c approach the middle of the land portion 210 along the groove 216 (see fig. 4) under the control of the in-house control device 22. Accordingly, the cargo 50 is pressed toward the center of the land portion 210 so as to be located at a substantially central portion of the land portion 210 (fig. 5 (d)).

As shown in fig. 1 and 6, the landing part 210 is provided in an opening/closing mechanism that opens and closes a tubular body 230 that protrudes vertically upward from the ceiling of the user house 20 in a chimney shape. More specifically, a land portion 210 is formed in a portion that becomes the inner side when the opening/closing mechanism is closed (fig. 6(a)), and when the opening/closing mechanism is opened, the land portion 210 assumes a horizontal posture at a position where the upper space is opened (fig. 6 (b)). Since the opening/closing mechanism is closed except when the unmanned aerial vehicle 1 lands, the members such as rubber constituting the land portion 210 are isolated from ultraviolet rays and the like to suppress the deterioration thereof. Further, if the air vent or the ventilation fan is provided in the cylinder 230, the temperature rise at the time of high temperature can be minimized, and the deterioration of each component constituting the landing gear 21 can be suppressed. Since the infrared camera 211, the illumination 212, the camera 214, the distance measuring unit 213, and the like are housed in the cylinder 230 except when the unmanned aerial vehicle 1 lands, they are not affected by rain, snow, and the like. Further, since the opening/closing mechanism is opened only when the unmanned aerial vehicle 1 lands, the landing gear 21 can be continuously used even in the case of light snowfall. In addition, the distribution service can be received even when the snow is blocked in the conventional distribution method.

In fig. 6, when the opening/closing mechanism constituting the land portion 210 is closed, the movable plates 215a, 215b, 215c take the first posture (fig. 6 (a)). When the unmanned aerial vehicle 1 lands, the opening/closing mechanism is switched from the closed state (fig. 6 a) to the open state (fig. 6 b). At this time, the movable plates 215a, 215b, 215c take the second posture. The unmanned aerial vehicle 1 lands on the landing part 210 with the cargo 50 suspended downward. If the cargo 50 is separated from the drone 1, the movable plates 215a, 215b, 215c assume the first attitude. Two fork members 221, which are provided inside the cylindrical body 230 and are extendable and retractable, extend in the direction of the two grooves 217 (fig. 4) provided in the landing part 210 and are inserted into the grooves 217 (fig. 6 c), respectively. Then, the two fork members 221 contract in a state where the load 50 is slightly lifted vertically upward, and draw the load 50 into the cylindrical body 230 (fig. 6 (d)). The fork 221 is lowered to the living space of the user U by the lifting mechanism 220 in a state where the load is loaded (fig. 6 d). The lifting mechanism 220 can be raised again to a height at which the cargo 50 is received from the drone 1.

When the landing part is installed in a yard of a user house, for example, contact between children or animals and the landing part, theft of goods, obstacles such as trees and wires during take-off and landing, and damage (mainly motor failure) of the unmanned aerial vehicle due to garbage raised during landing need to be considered. On the other hand, in the present embodiment, the landing part 210 is provided at a position higher than the living space of people, and therefore, these problems can be solved. Further, it is preferable that the land portion 210 is not provided on the roof of the first floor of the double-story house. This is because the user may enter the roof of the 1 st floor from the second floor window relatively easily and may approach the land portion 210 unnecessarily.

Fig. 7 is a sequence diagram of the entire system according to the present embodiment. First, the management system 30 receives a delivery request from, for example, a shopping site or the like used by the user (step S11). The delivery request includes the item 1D, the user lD, the position data of the warehouse where the item is located, the position data of the user house 20 serving as the delivery destination of the item, and the like.

The management system 30 determines the drone 1 to be used for distribution with reference to the drone DB32, the weather DB33, the map DB, and the like, which are not shown, calculates the route data, and updates the route DB31 and the drone DB32 based on the calculated route data. Then, the management system 30 transmits a distribution notification to the in-home control device 22 corresponding to the user lD (step S12). The delivery notification includes the product lD, the user lD, the unmanned aerial vehicle lD, and the expected date and time when the unmanned aerial vehicle 1 arrives at the user house 20.

The home control device 22 performs output processing such as displaying information included in the received delivery notification on a display device in the user home 20 or transmitting the information to a portable terminal of the user and displaying the information on the portable terminal (step S13). When the user operates the portable terminal to input an approval for the delivery notification, home control device 22 feeds back the response to management system 30 (step S14).

The management system 30 transmits delivery information including the commodity lD, the user lD, the unmanned aerial vehicle lD, and the route data to the in-warehouse control device 12 in which the delivery target cargo is located (step S15). When the in-warehouse control device 12 receives and stores the information (step S16), the response is fed back to the management system 30 (step S17).

When the predicted takeoff date and time indicated by the flight data comes, the unmanned aerial vehicle 1 loaded by the operator in the warehouse 10 takes off from the takeoff device 11 in a state where the cargo 50 is suspended. The unmanned aerial vehicle 1 autonomously flies near the destination using the GPS system, and if it enters an area within a threshold distance from the destination, the unmanned aerial vehicle 1D is wirelessly transmitted from the communication unit (step S18). If the communication unit receives the unmanned aerial vehicle 1D transmitted from the unmanned aerial vehicle 1 approaching the landing unit 210, the in-home control device 22 determines whether or not the received unmanned aerial vehicle 1D matches the unmanned aerial vehicle 1D of the unmanned aerial vehicle 1 that has been acquired in advance to be permitted to land on the landing unit 210 (the unmanned aerial vehicle 1D included in the delivery notification received in step S12). If they match, the in-home control device 22 transmits a signal for switching from autonomous travel of the unmanned aerial vehicle 1 to remote control by the in-home control device 22 to the unmanned aerial vehicle 1 so that the unmanned aerial vehicle 1 lands on the landing part 210 (step S19). On the other hand, if the received drone 1D does not match the drone 1D of the drone 1 permitted to land on the landing part 210 (the drone 1D included in the delivery notification received in step S12), the in-home control device 22 does not perform the remote control.

When the reception of the cargo is completed in the sequence described with reference to fig. 6 (step S20), the in-home control device 22 transmits a completion notification to the management system 30 (step S21). Upon receiving the end notification, the management system 30 transmits the end notification to the in-warehouse control device 12 (step S22).

According to the present embodiment as described above, it is possible to land an unmanned aerial vehicle having no photographing function at a destination.

[ modified examples ]

The above-described embodiment may be modified as follows.

[ modification 1] landing gear for non-snowfall areas

The landing gear 21 described in the embodiment is a mechanism that can withstand large-scale snowfall, but a landing gear having a structure as shown in fig. 8 may be used in non-snowfall areas. The landing part 240 is housed in a cylindrical body 250 that protrudes vertically upward in a chimney shape from the ceiling of the consumer house 20, and an opening/closing mechanism 260 is provided at the upper end of the cylindrical body 250. The opening and closing mechanism 260 is closed except when the unmanned aerial vehicle 1 lands, and the opening and closing mechanism 260 is opened only when the unmanned aerial vehicle 1 lands, so that the landing gear can be continuously used if the light snowfall occurs. The barrel 250 may also be equipped with vents, ventilators. In fig. 8, when the unmanned aerial vehicle 1 lands, the opening/closing mechanism 260 is in the open state (solid line in the figure) from the closed state (dotted line in the figure). The unmanned aerial vehicle 1 lands on the landing part 240 with the cargo suspended. If the cargo is separated from the drone 1, the landing part 240 is lowered to the living space of the user U by the elevating mechanism. The lifting mechanism can be raised again to a height at which the cargo is received from the drone 1.

As described above, the landing device according to the present invention may be provided with an opening/closing mechanism, and the landing part may be housed in the internal space when the opening/closing mechanism is closed, and the upper space of the landing part may be opened when the opening/closing mechanism is opened. In this way, the landing part 240 is configured to be directly accessible to the user, and therefore, the mechanism of the landing device is simplified, and the camera and the like can be cleaned from the room, and therefore, the maintainability is improved. The landing apparatus can be applied to an area (villa or the like) where a large number of fallen leaves or the like are present, by appropriately performing the sealing process of the opening/closing mechanism 260 and the countermeasure against snowfall.

Modification 2 Combined use with housing facility

The ventilation device and the smoke exhaust device may be mounted on the tubular body 230 of the landing device 21, and may be used in combination with a ventilation system that is usually provided in a house and a smoke exhaust system during a fire. Accordingly, the construction cost of the house can be suppressed. For example, the smoke evacuation system of the landing device 21 performs smoke evacuation in cooperation with a fire alarm in a house when a fire occurs. Further, the notification/disaster observation drone may be dispatched to the fire scene at the same time as the fire occurs. Since the landing device 21 is installed at a position higher than the living space, a higher smoke exhausting effect can be expected as compared with the case where it is installed in the living space.

[ modification 3] Meteorological Observation device

Each landing gear 21 may be provided with a meteorological observation device for observing meteorological data such as wind speed, wind direction, temperature, humidity, rainfall, visibility (field of vision), and air pressure. The in-house control device 22 transmits the weather data acquired by the weather-observing device to the management system 30. The management system 30 is expected to recognize, for example, a low pressure locally generated by storing and accumulating the weather data from the home control device 22 in the weather DB33, in addition to a normal weather observation system held by a weather bureau or the like. Further, the management system 30 may determine whether the unmanned aerial vehicle 1 can fly with reference to a failure database in which the causes of the unmanned aerial vehicle 1 falling are stored by being classified into, for example, a fuselage cause, a weather condition cause, a physical failure cause, a system cause, and the like.

The management system 30 can grasp the subtle weather conditions by the weather observation device installed in the landing device 21, and therefore, for example, it is expected that the occurrence of clouds causing local precipitation of sudden heavy rain (gurerilla rainstorm) can be predicted in urban areas, or that such a situation can be grasped at a level one minute before rain. The user may set an emergency forecast level in advance at a level required by the user in the management system 30, and when the weather in the area where the user is located or the area where the landing gear 21 is located suddenly changes, the management system 30 may issue a warning to the user's mobile terminal or the like.

[ modification 4] temporary application to Emergency landing

In the embodiment, the landing gear 21 is used for delivery service of goods, but it is also possible to provide the landing gear 21 as an emergency landing place for a surrounding flying drone. In the case where the unmanned aerial vehicle 1 needs an emergency landing, for example, a relatively safe place for evasion such as a river, a forest, or a roof of a large-scale factory can be found in a suburb, but it is difficult to secure such a place in an urban area. When the vehicle is landed on a road or the like, an electric wire or a pedestrian becomes an obstacle, and when the vehicle is landed on a roof of a building, it is necessary to take into consideration the entrance and exit of a lightning rod or a person. Then, when the unmanned aerial vehicle 1 detects a voltage drop of the battery, or detects an abnormality of the motor, or the like, and cannot reach the landing facility where maintenance is possible, the wireless emergency signal is transmitted from the communication unit. Among the landing apparatuses 21 that have received the emergency signal, the landing apparatus 21 that has no arrival plan of another drone transmits an acceptable signal. When the unmanned aerial vehicle 1 receives the receivable signal and responds, the landing gear 21 remotely controls the unmanned aerial vehicle 1 in the same manner as in the embodiment, and the unmanned aerial vehicle 1 lands on the landing part 210.

[ modification 5] Portable landing device

The use of an industrial unmanned aerial vehicle that is considered to be a main task in a disaster situation immediately after an earthquake or the like occurs is conceivable. In the case of such a disaster, the landing device corresponding to the landing part 210 according to the present embodiment may be transported to a place where material support is required as a portable (portable) landing device for disaster. Accordingly, the unmanned aerial vehicle can be used for supporting the transportation of the material. The landing unit 210 is mounted with a battery, a camera, an infrared camera, a distance measuring unit, a GPS, and a communication unit. The communication unit has a repeater function and can communicate with the communication units of the other landing units 210 within the communication range. Therefore, even in a large-scale disaster in which the communication function is lost, each landing part functions as a relay station on which an unmanned aerial vehicle supporting materials is mounted, or transmits information.

The landing device 21 is basically intended for a house of a single family or the like, but is not limited to this, and may be applied to a public facility, a temporarily installed event place, or the like.

[ modification 6] countermeasure against falling

There is a possibility that all the drones 1 fall together, for example, due to the occurrence of a solar storm. In this case, although a parachute (parachute) provided in the unmanned aerial vehicle 1 is opened to perform soft landing, it is also possible to notify people on the ground that the unmanned aerial vehicle 1 is landing from the air. Specifically, a whistle may be installed to the parachute, which makes a sound due to air resistance when the unmanned aerial vehicle 1 descends.

[ modification 7] Warning of approach of unmanned aerial vehicle having camera

Since the unmanned aerial vehicle 1 described in the embodiment is not equipped with a shooting function, the problem of infringing the privacy right does not occur during normal flight. On the other hand, in real life, since a certain number of unmanned aerial vehicles having an imaging function are flying, it is also possible to issue an alarm to the user when such an unmanned aerial vehicle having a camera approaches the landing device 21. The following table is an example of drone classification.

[ Table 1]

The meanings of the terms in the above table are as follows.

Comprehensive control: whether or not to have a function of flying in accordance with instructions from the integrated control system such as take-off, route, avoidance (very good:, many cases, no:, the same shall apply hereinafter)

A camera: whether or not to mount a camera

Carrying goods: whether or not to have the function of carrying goods

Manual control: whether the function of changing air route according to the user's desire is provided

Autonomous flight: whether or not to have the function of flying according to the air route reflecting the intention of the user in an autonomous flying manner

Approach measurement: whether to obtain the position of the wire and the tree in real time and automatically avoid the contact function

Emergency landing: whether or not to have a function of using the landing device as a landing place in an emergency

Approach alarm: whether the unmanned aerial vehicle is the object giving an alarm when approaching the landing device (X: unmanned aerial vehicle giving alarm, O: unmanned aerial vehicle giving alarm, more times: unmanned aerial vehicle not giving alarm)

The industrial unmanned aerial vehicle of class 1 refers to an unmanned aerial vehicle having advanced technology, specialized in a specific business, for use in, for example, surveying/bridge inspection/pesticide spraying/disaster support/movie shooting. In addition to autonomous flight using an integrated control system, manual flight is also possible according to the operator's will, but it is generally not possible to enter a flight prohibited area or an area other than that prescribed by regulations.

The air-shot drone classified in category 2 is a drone for shooting a photo or a video, for example, and generally requires an air route plan to be applied before flight. The route plan can be confirmed in advance by a simulator. Even with an aerial photography drone, photography is not required in a photography prohibited area, or image processing such as mosaic processing is required.

The distribution drone of category 3 is a drone for air transportation, which performs air transportation of light goods at a short distance. Particularly heavy goods are the applicable scope of industrial unmanned aerial vehicles. The user can set a departure place/destination/loading weight/arrival time and the like. The unmanned aerial vehicle is not provided with the camera, so that the possibility of infringing the privacy right can be eliminated. The control right is given to the landing apparatus by communicating with the landing apparatus in the vicinity directly above the landing apparatus from the vicinity of the landing apparatus where the main aircraft flies to the destination, such as a GPS or a beacon. After goods are delivered, the control right of the landing device is removed after the goods enter a stage with a certain height.

The unmanned aerial vehicle of interest (Hobby tree) of category 4 is an unmanned aerial vehicle for the purpose of interest use and simple aerial photography. Although the GPS system is mounted, autonomous flight is not allowed. An Automatic go home (auto home) is allowed according to the user's intention and when the control wave is interrupted. Although the fpv (first Person view), i.e., the image in the aerial shot, can be confirmed in real time by a monitor on the ground, its overlook distance is limited to about 100 m. The presence of the interested drone can be perceived from the landing gear by being assigned to a dedicated frequency.

[ modification 8] storage battery

The management system 30 may be configured to acquire various kinds of attribute information on the battery of the unmanned aerial vehicle 1 from the in-warehouse control device 12 and the like and store the attribute information. Specifically, the charger connected to the in-warehouse control device 12 transmits the storage battery 1D, the storage battery charge amount, the current voltage, the expected time of completion of charging, and other storage battery identification information to the management system 30 via the communication network 40. The management system 30 stores the battery 1D, the voltage change of the battery of the unmanned aerial vehicle 1 in flight, and the state of charge of the battery, and determines the state of aging of each battery based on these.

(modification 9) Black Box

Except for the interested drone, it is obligated to carry a black box. This is for investigation of the cause of the accident and for preventing criminal acts when the person is out of control or falls. The black box stores therein the following information for a certain period of time.

Position data of unmanned plane (longitude/latitude/altitude. level of flight can be reproduced after accident)

Image data of camera carried by unmanned aerial vehicle (including 360 degrees right above and below)

History record carried by storage battery in unmanned aerial vehicle

Voltage variation of battery carried by unmanned aerial vehicle

Motor revolution number change in unmanned aerial vehicle flight

Although the distribution drone is not equipped with a camera in principle, a camera for a black box may be equipped as an exception. The camera image is not leaked to the outside except in the case of an accident.

Before the flight, the camera mounted on the black box is initially inspected (initial check) in the following order.

1. A flight permit is issued from the management system 30.

2. The unmanned aerial vehicle carries the goods and is arranged on the take-off device.

3. Final confirmation before takeoff (communication check between drone and takeoff device) is completed.

4. Random letters and numerals (for example, A8u6lV684s) are displayed on the display screen on the takeoff device side.

5. And the camera of the black box shoots the display picture and sends random English letters and numbers as character data to the take-off device.

6. And when the random English letters and the random numbers of the two at the take-off device side are consistent, the take-off permission is sent to the unmanned aerial vehicle.

The distribution drone has the potential to be used for crimes by field personnel. For example, the system steals goods halfway, takes a surreptitious photograph of a delivery site with another camera, and uses a bomb for terrorist attack. In order to suppress such crimes and catch a criminal, a camera is mounted on the black box. The initial check is made before takeoff to confirm that the camera is functioning properly.

Modification 10 take-off device

The sequence from takeoff to takeoff is as follows. The cargo 50 is loaded into the cargo receiving portion of the take-off device. In the take-off device, the external dimension is obtained according to the bar code of the outer box of the goods. The minimum required drone specification is selected according to the actual weight measured. Whether the cargo is inclined during flight is estimated through an inclination test. Confirm the presence of hazardous materials (explosives/nebulizers) in the cargo, etc. In the case of dedicated distribution of meals and the like, the tilt test is omitted. Instead, special boxes are designed to prevent inadvertent cargo bias in the air.

[ modification 11] Lane

The distribution unmanned aerial vehicle flies according to the following routes.

Directly above the road and river: due to the overhead usage rights, the drone flies directly over the road and river with the same rules as cars (left-hand traffic and priority road relationship). At the intersection, the flight altitude is maintained at the value shown in the flight chart to prevent collision. When merging the priority roads, the unmanned aerial vehicles approaching the management system 30 side are confirmed in cooperation, and merging is performed without collision by the sensors mounted on the unmanned aerial vehicles.

And (3) specifying a route: the airline can fly even directly over the private land of the third party. Mainly, if it is unreasonable right above the road, the setting is performed in advance. The land owner is allowed to proceed to the course.

Private of delivery destination: the airline can fly even directly over the private land of the third party.

Modification 12 Beacon (base station)

In order to indicate a correct route and safe navigation for the unmanned aerial vehicle, base stations carrying beacons are arranged at intervals. The base station is a place where a landing device, a signal, a street lamp, a portable base station, a power line, and the like are installed. The functions installed in the base station are as follows.

Storage unit for position information (longitude/latitude/altitude/installation height/foundation height)

Anemometer, barometer, rain gauge, visibility meter

Communication part with unmanned aerial vehicle

Video camera

The drone 1 is connected to the management system 30 through a base station. The cameras photograph the drones flying around and monitor in real time the drones that are not permitted to fly.

Modification example 13 countermeasure against terrorist attack on unmanned aerial vehicle

It is also possible to prevent the case of terrorist attacks from low altitudes by illegal drones that are not managed by the system. The positions and the flight purposes are managed by the system except for the interested drones, and even in the case of the interested drones, the number and the positions of the unmanned planes can be grasped roughly by grasping the wireless frequency band used by the unmanned planes by the system.

The beacons arranged at various places observe the operation conditions of various unmanned aerial vehicles. In this beacon network, when a drone satisfying a specific condition (speed/altitude/moving range/1D) is present, a warning is issued to the management system 30. The management system 30 instructs the system of the following defense guidelines depending on the scale of the terrorist attack that can be predicted.

Warning: in the warning phase, a possible terrorist attack by the drone is prompted and directed to enter the building and close the window. In addition to the fixed landing gear, the portable terminal can be warned so that terrorist attacks can be dealt with during travel.

And (3) limiting the flight: new flight behavior of the drone is prohibited in certain areas. If necessary, the landing is performed on the nearest landing gear by emergency landing. A drone obtained by restricting flight can be temporarily borrowed as an anti-terrorist drone.

And (3) observation and reinforcement: the camera of the landing apparatus is operated to transmit the captured image directly above to the management system 30. And releases the black box mounted on the drone 1. Hereby, images from the delivery drones can also be sent to the management system 30, enabling blocking/greeking using visual information.

Blocking: various kinds of unmanned aerial vehicles are installed in places such as rivers where the unmanned aerial vehicles do not cause a disaster even if they fall, and the unmanned aerial vehicles are suspended in the traveling direction of the terrorist attack unmanned aerial vehicles to hinder (block) their flight. With regard to a terrorist attack drone, a few of them have a high possibility of breaking through the blocking net, and therefore, a plurality of drones are provided for important blocking. Even if the terrorist attack side performs saturation attack, a good defense effect can be expected due to the sufficient number of the operated distribution unmanned aerial vehicles.

Attack-meeting: for important areas, unmanned aerial vehicles aiming at attack on terrorist attack unmanned aerial vehicles are equipped. In an area set to allow attack in advance, the terrorist attack unmanned aerial vehicle is brought close to the area to perform electromagnetic interference, and the terrorist attack unmanned aerial vehicle is hit down. The unmanned plane is attacked, and then the parachute is opened to land.

Description of the symbols

1 unmanned aerial vehicle (rotorcraft);

10 a warehouse;

11 a takeoff device;

12 in-warehouse control means;

20 user residences;

21 landing gear (rotorcraft landing gear);

22 in-home control devices;

30 a management system;

31 a lane DB;

32, unmanned aerial vehicle DB;

33 weather DB;

211 an infrared camera;

212, illumination;

213 distance measuring part;

214 camera;

215 movable plate.