JP2017027355A - Monitoring device - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a monitoring device using unmanned flight bodies, capable of collecting the unmanned flight bodies even when control of the unmanned flight bodies becomes impossible.SOLUTION: A monitoring device comprises: a base substrate 2; unmanned flight bodies 3; string-like members 4 connected to the base substrate 2 and the unmanned flight bodies 3; monitoring cameras 7 mounted on the unmanned flight bodies 3; flight body control parts 8 mounted on the unmanned flight bodies 3 and control the unmanned flight bodies 3; and a monitor control part 5 disposed on a position different from positions of the unmanned flight bodies 3, and controls the unmanned flight bodies 3. The base substrate 2 is a movable body.SELECTED DRAWING: Figure 1

Description

  The present invention relates to a monitoring device for monitoring using an unmanned air vehicle.

  Patent Document 1 describes a monitoring device that monitors the surroundings of a heavy machine such as a crane at a civil engineering site or a building site. In this monitoring apparatus, a plurality of monitoring cameras are fixed to heavy equipment, and images taken by the respective monitoring cameras are switched and displayed, thereby ensuring safety around the heavy equipment. However, if the surveillance camera is fixed to a heavy machine, there is a problem that an area that cannot be monitored is generated due to a blind spot because the range that can be imaged is limited.

  Therefore, Patent Document 2 proposes a monitoring device that monitors farmland and the like using an unmanned air vehicle. An unmanned air vehicle can fly at any position. For this reason, the above problem can be solved by using an unmanned aerial vehicle as in Patent Document 2.

JP 2004-137035 A JP-A-11-291991

  However, if the unmanned aerial vehicle becomes uncontrollable due to a failure, crosstalk, or the like, there is a risk of dropping or missing.

  Therefore, an object of the present invention is to provide a monitoring apparatus that uses an unmanned aerial vehicle and can collect the unmanned aerial vehicle even when the unmanned aerial vehicle becomes uncontrollable.

  A monitoring device according to the present invention includes a base, an unmanned air vehicle, a string-like member connected to the base and the unmanned air vehicle, a monitoring camera mounted on the unmanned air vehicle, and a control unit that controls the unmanned air vehicle. And the base body is a movable body capable of moving.

  In the monitoring apparatus according to the present invention, since the monitoring camera is mounted on the unmanned air vehicle, the surroundings of the base can be imaged from an arbitrary position. On the other hand, since the unmanned aerial vehicle is connected to the base body by a string-like member, even if it becomes uncontrollable due to a failure, a crossing or the like, the unmanned flying object does not go beyond the range constrained by the string-like member. Thereby, even if the unmanned air vehicle becomes uncontrollable, the unmanned air vehicle can be recovered. Further, in this monitoring apparatus, since the base body is a movable body, it is possible to perform monitoring from an unmanned flying body at various places. Thereby, the utilization range of a monitoring apparatus can be expanded.

  Another monitoring device according to the present invention controls a base, an unmanned air vehicle, a string-like member connected to the base and the unmanned air vehicle, a monitoring camera mounted on the unmanned air vehicle, and the unmanned air vehicle. A control unit, and a disconnection detection unit that detects disconnection of the string-like member.

  In the monitoring apparatus according to the present invention, since the monitoring camera is mounted on the unmanned air vehicle, the surroundings of the base can be imaged from an arbitrary position. On the other hand, since the unmanned aerial vehicle is connected to the base body by a string-like member, even if it becomes uncontrollable due to a failure, a mixed line or the like, the unmanned flying object does not move away from the base body beyond the length of the string-like member. Thereby, even if the unmanned air vehicle becomes uncontrollable, the unmanned air vehicle can be recovered. Furthermore, in this monitoring apparatus, the disconnection detection part detects the disconnection of a string-like member. For this reason, when the disconnection of the string-like member is detected, it is possible to suppress the unmanned air vehicle from being lost by performing the flight control of the unmanned air vehicle.

  In this case, the signal line provided along the string-like member, the transmission unit connected to one side of the base body of the signal line and the unmanned air vehicle, and the other side of the base body of the signal line and the unmanned air vehicle And a receiving unit to be connected, the transmitting unit transmits a signal to the receiving unit through a signal line, and the disconnection detecting unit determines that the string-like member is disconnected when the receiving unit cannot receive the signal. Also good. In this monitoring apparatus, when the string-like member is not disconnected, the transmission unit and the reception unit are electrically connected by the signal line, so that the signal can be received by the reception unit. On the other hand, when the string-like member is disconnected, since the transmission unit and the reception unit are not electrically connected by the signal line, the reception unit cannot receive a signal. For this reason, the disconnection detection part can detect easily the presence or absence of the disconnection of a string-like member by determining the reception presence or absence of the signal in a reception part.

  Further, the control unit may cause the unmanned air vehicle to fly to the set position when the disconnection detection unit detects the disconnection of the string-like member. In this monitoring device, when the string-like member is disconnected, the control unit causes the unmanned flying object to fly to the set position. Therefore, the unmanned flying object can be prevented from being lost due to the disconnection of the string-like member.

  Moreover, it is preferable that a control part stops the imaging by a surveillance camera, when the disconnection of a string-like member is detected by the disconnection detection part. In this monitoring apparatus, when the string-like member is disconnected, the control unit stops the imaging by the monitoring camera, so when the unmanned flying object is separated from the base body due to the disconnection of the string-like member, Imaging can be suppressed.

  Moreover, you may further provide the load detection part which detects the tensile load which is acting on the string-like member. In this monitoring apparatus, if an excessive tensile load acts on the string-like member, the string-like member may be disconnected. Therefore, it is possible to determine whether or not the string-like member is likely to be broken before the string-like member is broken by detecting the tensile load acting on the string member. .

  Further, the control unit may cause the unmanned air vehicle to fly in the direction in which the string-like member is loosened when the tensile load detected by the load detection unit exceeds a threshold value. In this monitoring apparatus, when the tensile load detected by the load detection unit exceeds the threshold value, the control unit causes the unmanned flying object to fly in the direction in which the string-like member is slackened, so that an excessive tensile load acts on the string-like member. This can prevent the string-like member from breaking.

  The control unit may be a flying object control unit mounted on an unmanned flying object. In this monitoring device, since the control unit for controlling the unmanned aerial vehicle is mounted on the unmanned aerial vehicle, when the disconnection of the string-like member is detected, a process corresponding to the disconnection is performed by the autonomous control of the unmanned aerial vehicle. be able to.

  Another monitoring apparatus according to the present invention includes a base, a plurality of unmanned air vehicles, a string member connected to the base and the unmanned air vehicles, a surveillance camera mounted on the unmanned air vehicles, and an unmanned air vehicle. A control unit that controls, and the control unit adjusts the flight position of the unmanned air vehicle based on the image captured by the monitoring camera.

  In the monitoring apparatus according to the present invention, since the monitoring camera is mounted on the unmanned air vehicle, the surroundings of the base can be imaged from an arbitrary position. On the other hand, since the unmanned aerial vehicle is connected to the base body by a string-like member, even if it becomes uncontrollable due to a failure, a mixed line or the like, the unmanned flying object does not move away from the base body beyond the length of the string-like member. Thereby, even if the unmanned air vehicle becomes uncontrollable, the unmanned air vehicle can be recovered. Furthermore, in this monitoring apparatus, since the imaging area by the monitoring camera changes depending on the flight position of the unmanned air vehicle, the control unit adjusts the flight position of the unmanned air vehicle based on the image captured by the monitoring camera, thereby monitoring The desired area can be appropriately imaged.

  In this case, the control unit includes a region that is not captured between the images captured by the monitoring cameras mounted on the adjacent first unmanned flight vehicle and the second unmanned flight vehicle among the plurality of unmanned flight vehicles. In this case, at least one of the first unmanned air vehicle and the second unmanned air vehicle may be caused to fly in a direction approaching each other. If adjacent unmanned aerial vehicles are too far apart, an area that is not captured by the surveillance camera is generated, but the area captured by the captured image varies depending on the horizontal position and the vertical position of the unmanned aerial vehicle. Therefore, in this monitoring device, if there is an area that is not captured between images captured by a monitoring camera mounted on an adjacent unmanned aerial vehicle, the control unit brings these unmanned aerial vehicles closer to each other. Can be suppressed.

  The control unit may cause the unmanned air vehicle to fly to a position above the current position when the monitoring target protrudes from the image captured by the monitoring camera. When the unmanned aerial vehicle flies at a low position with respect to the monitoring target, the monitoring target may protrude from the image captured by the monitoring camera. Therefore, in this monitoring apparatus, when the monitoring target protrudes from the image captured by the monitoring camera, the control unit causes the unmanned air vehicle to fly to a position above the current position, so that the entire monitoring target is captured by the monitoring camera. be able to.

  Further, the control unit may be a monitoring control unit provided in a place different from the unmanned air vehicle. In this monitoring apparatus, since the control unit for controlling the unmanned aerial vehicle is provided at a location different from that of the unmanned aerial vehicle, an operator or the like can position the unmanned aerial vehicle at an optimum position based on an image captured by the surveillance camera. Can be made to fly.

  In any one of the monitoring control devices described above, the string-like member may include a power supply line that supplies power to the unmanned air vehicle from the base side. In this monitoring device, since electric power is supplied from the base side to the unmanned aerial vehicle via the power supply line of the string-like member, it is not necessary to mount a battery on the unmanned aerial vehicle. As a result, the unmanned air vehicle can be reduced in weight, and the unmanned air vehicle can be allowed to fly for a long time.

  Moreover, you may further provide the elastic elastic member connected between a base | substrate and a string-like member. In this monitoring device, even if the unmanned air vehicle moves away from the base body vigorously, the elastic expansion / contraction member elastically expands / contracts, whereby the tensile load acting on the string-like member can be gradually increased. Thereby, it can suppress that a string-like member breaks.

  Moreover, you may further provide the elastic expansion-contraction member connected to a base | substrate and the intermediate part of a string-like member in the state which the string-like member slackened. In this monitoring device, even if the unmanned air vehicle moves away from the base body vigorously, the elastic expansion / contraction member elastically expands / contracts, whereby the tensile load acting on the string-like member can be gradually increased. Thereby, it can suppress that a string-like member breaks. In addition, since the elastic stretchable member is connected to the base and the middle portion of the string-like member in a state where the string-like member is slackened, the string-like member is restrained from inhibiting the elastic stretchable member from being stretched. The shaped member can be connected to the substrate.

  According to the present invention, in a monitoring device using an unmanned air vehicle, the unmanned air vehicle can be recovered even if the unmanned air vehicle becomes uncontrollable.

It is a schematic block diagram of the monitoring apparatus which concerns on 1st embodiment. It is a functional block diagram of a flying object control part. It is the schematic of the tower crane to which the monitoring apparatus of this embodiment is applied. It is the schematic which shows the joining operation | work of the suspended load by the tower crane shown in FIG. It is the schematic of the tower crane of the comparative example 1. It is the schematic of the tower crane of the comparative example 2. It is a schematic block diagram of the monitoring apparatus which concerns on 2nd embodiment. It is a functional block diagram of a flying object control part. It is a flowchart which shows the disconnection detection and tensile load detection process of a string-like member. It is a schematic block diagram of the monitoring apparatus which concerns on 3rd embodiment. It is a schematic block diagram of the monitoring apparatus which concerns on 4th embodiment. It is a figure for demonstrating the image imaged by the adjacent unmanned air vehicle. It is a figure for demonstrating the image imaged by the adjacent unmanned air vehicle. It is a figure for demonstrating the image imaged by the adjacent unmanned air vehicle. It is a flowchart which shows an image display process. It is a flowchart which shows a flight position adjustment process.

  DESCRIPTION OF EMBODIMENTS Hereinafter, a preferred embodiment of a monitoring device according to the present invention will be described in detail with reference to the drawings. In all drawings, the same or corresponding parts are denoted by the same reference numerals.

(First embodiment)
FIG. 1 is a schematic configuration diagram of a monitoring device according to the first embodiment. As shown in FIG. 1, the monitoring device 1 according to the first embodiment includes a base body 2, one or a plurality of unmanned flying bodies 3, a string-like member 4 connected to the base body 2 and the unmanned flying bodies 3, A monitoring control unit 5.

  The base body 2 is connected to the unmanned aerial vehicle 3 by a string-like member 4. The base body 2 is provided with a power supply source 6 for supplying power to the unmanned air vehicle 3. As the power supply source 6, a capacitor (battery), a generator, or the like can be used.

  The substrate 2 may be a stationary object, but is preferably a movable body that can move. The place where the movable body moves may be any place such as land, water, and air. The movable body may be moved in any manner such as moving, flying, turning, rotating, swinging, and bending. Specific examples of movable bodies include cranes, tower cranes, excavator and other construction machines, automobiles, trucks, buses, motorcycles and other traveling vehicles, railways, monorails and other rail devices, airplanes, helicopters, Airships such as airships, balloons, ships, ships such as boats, power lifts, unloaders, winch and other lifting devices, humanoid robots, animal robots, industrial robots and other mechanical devices, humans, dogs and other animals, Etc. When the base body 2 is an animal such as a person or a dog, the string-like member 4 may be directly connected to these animals, but via a rucksack, a belt or other attachment device attached to these animals. Alternatively, it may be indirectly connected to the string-like member 4.

  The unmanned air vehicle 3 is an unmanned air vehicle that can fly. The unmanned air vehicle 3 can acquire the current position of the unmanned air vehicle 3 by GPS or the like. The current position can be represented by, for example, a horizontal position (horizontal coordinate) and a vertical position (altitude). The unmanned air vehicle 3 can fly at a position commanded from the monitoring control unit 5 by autonomous control or the like. As the unmanned aerial vehicle 3, various known unmanned aerial vehicles can be used with the unmanned aerial vehicle described in Patent Document 2 as an example.

  The unmanned air vehicle 3 includes a monitoring camera 7 and an air vehicle control unit 8. As will be described later, since the unmanned air vehicle 3 flies by receiving power supply from the power supply source 6 of the base body 2, it is not necessary to include a battery for flying the unmanned air vehicle 3.

  The monitoring camera 7 images the outside of the unmanned air vehicle 3 in order to monitor the surrounding situation of the base body 2. The surveillance camera 7 may capture a still image, but preferably captures a moving image. In any case, the surveillance camera 7 acquires a captured image. Although the imaging direction of the monitoring camera 7 is not particularly limited, in this embodiment, the monitoring camera 7 will be described as imaging the lower part of the unmanned air vehicle 3. The unmanned aerial vehicle 3 may include a wind sensor (not shown) that measures a wind direction and a wind speed in addition to the monitoring camera in order to monitor the surroundings of the base body 2.

  The flying object control unit 8 controls the unmanned flying object 3 using a CPU, a memory, and the like as main components.

  FIG. 2 is a functional block diagram of the flying object control unit. As shown in FIGS. 1 and 2, the flying object control unit 8 includes a flight control unit 81 and a transmission control unit 82.

  The flight control unit 81 performs flight control of the unmanned air vehicle 3. The flight control of the unmanned air vehicle 3 by the flight control unit 81 includes flight control based on a command from the monitoring control unit 5 and flight control not based on the command from the monitoring control unit 5.

  The flight control unit 81 causes the unmanned air vehicle 3 to fly, for example, at a position commanded by the monitoring control unit 5 as flight control based on the command from the monitoring control unit 5. As the flight position of the unmanned air vehicle 3 instructed by the monitoring control unit 5, for example, a position where a plurality of unmanned air vehicles 3 are equally spaced from each other, a position where a specific position around the base body 2 can be imaged from the monitoring camera 7, etc. Is mentioned. As described above, since the unmanned air vehicle 3 can acquire the current position of the unmanned air vehicle 3, the current position of the base body 2 is registered in the flight control unit 81 or the monitoring control unit 5. Thus, the relative position of the unmanned air vehicle 3 with respect to the base body 2 can be calculated.

  The flight control unit 81 causes the unmanned air vehicle 3 to fly to a set position when a failure occurs, for example, as flight control not based on a command from the monitoring control unit 5. The set position is a position set in advance in the unmanned air vehicle 3. The set position may be a specific position of the base 2 or a position different from the base 2. Examples of the failure include a case where a command from the monitoring control unit 5 does not reach due to a failure or a crossing line, or a case where power supply from the power supply source 6 is interrupted.

  The transmission control unit 82 transmits the image captured by the monitoring camera 7 to the monitoring control unit 5. The transmission of the image from the transmission control unit 82 to the monitoring control unit 5 can be performed by wire or wireless. When performing by wire, the string-like member 4 can be used. When a wind sensor or the like is mounted on the unmanned air vehicle 3, the transmission control unit 82 also transmits a value measured by this sensor to the monitoring control unit 5.

  The string-like member 4 is connected to the base body 2 and the unmanned air vehicle 3. That is, the unmanned air vehicle 3 is connected to the base body 2 by the string-like member 4. For this reason, the unmanned aerial vehicle 3 can fly only within the range restrained by the string-like member 4. The connection between the string-like member 4 and the base body 2 and the unmanned air vehicle 3 may be directly connected or indirectly connected via another member. When there are a plurality of unmanned air vehicles 3, the string-like member 4 may connect each unmanned air vehicle 3 to the base body 2 individually, or connect the plurality of unmanned air vehicles 3 together to the base body 2. Good.

  The string-like member 4 includes a power supply line (not shown) for supplying power (power supply) to the unmanned air vehicle 3 from the power supply source 6. For this reason, the power supply source 6 and the unmanned aerial vehicle 3 are electrically connected via the feeder line of the string-like member 4.

  The monitoring control unit 5 is provided at a location different from the unmanned air vehicle 3. The monitoring control unit 5 controls the unmanned aerial vehicle 3 using a CPU, a memory, and the like as main components. More specifically, the supervisory control unit 5 controls the flight of the unmanned air vehicle 3 by instructing the flight position to the flight control unit 81 of the unmanned air vehicle 3. Moreover, the monitoring control part 5 acquires the image imaged with the monitoring camera by receiving the image which the transmission control part 82 of the unmanned air vehicle 3 transmitted. Then, the monitoring control unit 5 displays the acquired image on a display device such as a monitor and commands the flight position of the unmanned air vehicle 3. At this time, the monitoring control unit 5 may display the images transmitted from the plurality of unmanned air vehicles 3 on the display device as they are, or may combine them into one and display them on the display device.

  The monitoring control unit 5 may be provided at any location as long as it is provided at a location different from the unmanned air vehicle 3. For example, it may be provided on the base 2 or may be provided at a location different from the base 2.

  Next, the example which applied the monitoring apparatus 1 of this embodiment to the tower crane of a construction site is demonstrated.

  FIG. 3 is a schematic view of a tower crane to which the monitoring device of the present embodiment is applied. FIG. 4 is a schematic diagram showing the joining work of the suspended load by the tower crane shown in FIG. As shown in FIGS. 3 and 4, in this application example, a battery 6 a that functions as the power supply source 6 is attached to the tower crane 2 a that functions as the base body 2. A plurality of unmanned aerial vehicles 3 are connected to the battery 6 a by the string-like member 4, and each unmanned aerial vehicle 3 is supplied with power from the battery 6 a by the string-like member 4. A monitoring controller (not shown in FIGS. 3 and 4) is provided in the operation room (not shown) of the tower crane 2a. When the suspended load A suspended from the tower crane 2a is joined to the members to be joined B1 and B2, the suspended load A is lowered from above the members to be joined B1 and B2.

  However, from the operation room, the joining position of the suspended load A and the joined members B1 and B2 may not be visible due to a blind spot. In such a case, the operator first causes the unmanned air vehicle 3 to fly to a position where the surveillance camera 7 can image the joining position of the suspended load A and the members to be joined B1 and B2, and displays it on the display device provided in the operation room. Then, an image captured by the monitoring camera 7 is displayed. Then, the operator lowers the suspended load A from above the joined members B1 and B2 while looking at the display device on which the joining position between the suspended load A and the joined members B1 and B2 is displayed. Thereby, the operator can join the suspended load A to the to-be-joined members B1 and B2 easily.

  Next, the tower crane of the comparative example in which an unmanned air vehicle is not provided will be described.

  FIG. 5 is a schematic view of a tower crane of Comparative Example 1. As shown in FIG. 5, in the comparative example 1, the monitoring camera 7b is attached to the tip of the jib of the tower crane 2a. For this reason, from the display device provided in the operation room, the suspended load A can be seen from directly above, but the joining position of the suspended load A and the joined members B1 and B2 cannot be seen.

  FIG. 6 is a schematic view of a tower crane of Comparative Example 2. As shown in FIG. 6, in Comparative Example 2, surveillance cameras 7 c are attached to both ends of the suspended load A. For this reason, the joining position of the suspended load A and the joined members B1 and B2 can be seen from the display device provided in the operation chamber. However, since the surveillance camera 7c is attached to the suspended load A, it is necessary to replace the surveillance camera 7c with another suspended load (not shown) after joining the suspended load A to the members B1 and B2.

  Thus, in the monitoring apparatus 1 of this embodiment, since the monitoring camera 7 is mounted on the unmanned air vehicle 3, the surroundings of the base body 2 can be imaged from an arbitrary position. On the other hand, since the unmanned aerial vehicle 3 is connected to the base body 2 by the string-like member 4, even if it becomes uncontrollable due to a failure, a mixed line or the like, the unmanned air vehicle 3 moves away from the base body 2 beyond the range constrained by the string-like member 4. There is nothing. Thereby, even if the unmanned air vehicle 3 becomes uncontrollable, the unmanned air vehicle 3 can be recovered.

  Furthermore, in this monitoring apparatus 1, since the base | substrate 2 is a movable body, it can monitor from the unmanned air vehicle 3 in various places. Thereby, the utilization range of the monitoring apparatus 1 can be expanded.

  In the monitoring device 1, since electric power is supplied from the base body 2 to the unmanned aerial vehicle 3 through the power supply line of the string-like member 4, it is not necessary to mount a battery on the unmanned aerial vehicle 3. Thereby, the unmanned aerial vehicle 3 can be reduced in weight, and the unmanned aerial vehicle 3 can be allowed to fly for a long time.

(Second embodiment)
Next, a second embodiment will be described. The second embodiment is basically the same as the first embodiment, but differs from the first embodiment only in that the disconnection detection / tensile load detection of the string-like member is performed. For this reason, below, only the matter which is different from 1st embodiment is demonstrated, and description of the matter similar to 1st embodiment is abbreviate | omitted.

  FIG. 7 is a schematic configuration diagram of a monitoring device according to the second embodiment. As shown in FIG. 7, the monitoring device 1 </ b> A according to the second embodiment includes a base 2, one or more unmanned air vehicles 3, a string-like member 4 connected to the base 2 and the unmanned air vehicles 3, A monitoring control unit 5, a load sensor 11, and a receiving unit 12 are provided. In FIG. 7, only one unmanned air vehicle 3 is shown for easy understanding.

  The string-like member 4 includes a signal line (not shown) provided along the string-like member 4 separately from the power supply line. The load sensor 11 and the receiving unit 12 are electrically connected by a signal line of the string-like member 4.

  The load sensor 11 is a sensor that detects a tensile load acting on the string-like member 4. For this reason, the load sensor 11 functions as a load detection unit that detects a tensile load acting on the string-like member 4. As the load sensor 11, various known sensors can be used. The load sensor 11 is connected to the string-like member 4 and the signal line base 2 side end. Then, the load sensor 11 converts the detected tensile load into an electric signal and transmits it to the receiving unit 12 through a signal line. For this reason, the load sensor 11 also functions as a transmission unit that transmits a signal to the reception unit through the signal line. The transmission of the tensile load can be performed regularly or continuously.

  The receiving unit 12 is mounted on the unmanned aerial vehicle 3 and connected to the end of the signal line on the unmanned aerial vehicle 3 side. The receiving unit receives the electrical signal of the tensile load transmitted from the load sensor 11. Then, the receiving unit 12 transmits the received tensile load to the flying object control unit 8.

  FIG. 8 is a functional block diagram of the flying object control unit. As shown in FIGS. 7 and 8, the flying object control unit 8 includes a flight control unit 81, a transmission control unit 82, an imaging control unit 83, a disconnection detection unit 84, and a load determination unit 85.

  The imaging control unit 83 controls imaging by the monitoring camera 7. Examples of the control of the monitoring camera 7 by the imaging control unit 83 include start of imaging by the monitoring camera 7, stop of imaging by the monitoring camera 7, and the like.

  The disconnection detection unit 84 detects disconnection of the string-like member 4. Specifically, when the string-like member 4 is not disconnected, the load sensor 11 and the receiving unit 12 are electrically connected by the signal line of the string-like member 4, and thus transmitted from the load sensor 11. The receiving unit 12 can receive the electrical signal of the tensile load. On the other hand, when the string-like member 4 is disconnected, the load sensor 11 and the receiving unit 12 are not electrically connected by the signal line of the string-like member 4. The electric signal cannot be received by the receiving unit 12. Therefore, the disconnection detection unit 84 determines that the string-like member 4 is disconnected when the reception unit 12 cannot receive the electrical signal of the tensile load, and thereby detects the disconnection of the string-like member 4.

  And when the disconnection of the string-like member 4 is detected by the disconnection detection unit 84, the flight control unit 81 causes the unmanned air vehicle 3 to fly to the set position as the disconnection process, and the imaging control unit 83 performs the disconnection process. Imaging by the monitoring camera 7 is stopped.

  The load determination unit 85 determines whether the tensile load detected by the load sensor 11 exceeds a threshold value. That is, the load determination unit 85 receives the tensile load transmitted from the reception unit 12 to the flying object control unit 8, and determines whether or not the received tensile load exceeds a threshold value. The threshold value is a value of a tensile load that does not cause the string-like member 4 to be disconnected, and is preferably a value with a certain margin.

  And when it determines with the tensile load exceeding a threshold value by the load determination part 85, the flight control part 81 is made to fly the unmanned air vehicle 3 in the direction in which the string-like member 4 loosens as a disconnection avoidance process. That is, if the tensile load acting on the string-like member 4 becomes excessive, the string-like member 4 may be disconnected. In such a case, the unmanned air vehicle 3 is caused to fly in the direction in which the string-like member 4 is loosened. . The direction in which the string-like member 4 is slackened is a direction approaching the base body 2 and can be easily calculated from the current positions of the base body 2 and the unmanned air vehicle 3.

  Next, with reference to FIG. 9, the disconnection detection / tensile load detection processing of the string-like member in the monitoring device 1A will be described.

  FIG. 9 is a flowchart showing the disconnection detection / tensile load detection processing of the string-like member. As shown in FIG. 8, first, the load sensor 11 detects a tensile load acting on the string-like member 4 (S1). And the load sensor 11 transmits the electrical signal of the detected tensile load to the receiving part 12 (S2).

  Next, the disconnection detection unit 84 determines whether or not the string-like member 4 is disconnected based on whether or not the tensile load is received by the reception unit 12 (S3).

  When it is determined that the string-like member 4 is disconnected (S3: YES), the flight control unit 81 and the imaging control unit 83 perform a disconnection process (S4). The flight control unit 81 causes the unmanned air vehicle 3 to fly to the set position as the disconnection process. The imaging control unit 83 stops imaging by the monitoring camera 7 as the disconnection process.

  On the other hand, when it determines with the string-like member 4 not being disconnected (S3: NO), the load determination part 85 determines whether the tensile load detected by the load sensor 11 exceeds a threshold value (S5).

  When it determines with a tensile load not exceeding a threshold value (S5: NO), 1 A of monitoring apparatuses complete | finish a disconnection detection and tensile load detection process of a string-like member.

  On the other hand, when it determines with a tensile load exceeding a threshold value (S5: YES), the flight control part 81 is made to fly the unmanned air vehicle 3 in the direction in which the string-like member 4 loosens as a disconnection avoidance process (S6). And 1A of monitoring apparatuses complete | finish a disconnection detection and tensile load detection process of a string-like member.

  Thus, in the monitoring apparatus 1A of the present embodiment, the disconnection detection unit 84 detects disconnection of the string-like member 4. For this reason, when the disconnection of the string-like member 4 is detected, it is possible to suppress the unmanned air vehicle from being lost by performing the flight control of the unmanned air vehicle 3. In this case, it is possible to easily detect whether or not the string-like member 4 is disconnected by determining whether or not the receiving unit 12 has received the electrical signal of the tensile load.

  Moreover, in this monitoring apparatus 1A, when the string-like member 4 is disconnected, the flight control unit 81 causes the unmanned aircraft 3 to fly to the set position, and therefore the unmanned aircraft 3 is lost due to the disconnection of the string-like member 4. Can be suppressed. Similarly, when the string-like member 4 is disconnected, the imaging control unit 83 stops the imaging by the monitoring camera 7, so that when the unmanned flying vehicle 3 is separated from the base body due to the disconnection of the string-like member 4, the monitoring camera Imaging other than the monitoring target can be suppressed.

  Further, in this monitoring apparatus 1A, the load sensor 11 detects the tensile load acting on the string member, so that the string-like member 4 is likely to be disconnected by the disconnection detecting unit 84 before the string-like member 4 is disconnected. It is possible to determine whether or not this is a state.

  Moreover, in this monitoring apparatus 1A, when the tensile load detected by the load sensor 11 exceeds the threshold value, the flight control unit 81 causes the unmanned air vehicle 3 to fly in the direction in which the string-like member 4 is loosened. It is possible to prevent the string-like member 4 from being disconnected due to an excessive tensile load acting on it.

  Moreover, in this monitoring apparatus 1A, since the flying body control unit 8 that controls the unmanned flying body 3 is mounted on the unmanned flying body, the autonomous control of the unmanned flying body 3 when the disconnection of the string-like member 4 is detected. Thus, processing corresponding to the disconnection can be performed.

(Third embodiment)
Next, a third embodiment will be described. The third embodiment is basically the same as the second embodiment, but differs from the second embodiment only in that an elastic elastic member is connected to the string-like member. For this reason, below, only the matter which is different from 2nd embodiment is demonstrated, and description of the matter similar to 2nd embodiment is abbreviate | omitted.

  FIG. 10 is a schematic configuration diagram of a monitoring device according to the third embodiment. As shown in FIG. 10, the monitoring device 1B according to the third embodiment includes a base body 2, one or a plurality of unmanned flying bodies 3, a string-like member 4 connected to the base body 2 and the unmanned flying bodies 3, A monitoring control unit 5, a load sensor 11, a receiving unit 12, and an elastic elastic member 13 are provided. In FIG. 10, only one unmanned air vehicle 3 is shown for easy understanding.

  The elastic expansion / contraction member 13 is a member capable of elastic expansion / contraction. A coil spring or the like can be used as the elastic elastic member 13. The elastic elastic member 13 is connected between the base 2 and the string-like member 4. That is, the string-like member 4 is indirectly connected to the base 2 via the elastic elastic member 13 and the load sensor 11. In this case, the power supply line of the string-like member 4 and the power supply source 6 of the base body 2 are electrically connected by passing the power supply line through the elastic expansion / contraction member 13 or arranging the power supply line in parallel with the elastic expansion / contraction member 13. Connect to. The elastic elastic member 13 may be connected between the base body 2 and the load sensor 11, or may be connected between the load sensor 11 and the string-like member 4. FIG. 10 shows a form in which the elastic elastic member 13 is connected between the load sensor 11 and the string-like member 4.

  As described above, in the monitoring apparatus 1B of the present embodiment, the elastic member 13 can expand and contract the maximum separation distance between the base body 2 and the unmanned flying vehicle 3, so that an excessive tensile load acts on the string member 4. Thus, the string-like member 4 can be prevented from being disconnected.

(Fourth embodiment)
Next, a fourth embodiment will be described. The fourth embodiment is basically the same as the second embodiment, but differs from the second embodiment only in that an elastic elastic member is connected to the string-like member. For this reason, below, only the matter which is different from 2nd embodiment is demonstrated, and description of the matter similar to 2nd embodiment is abbreviate | omitted.

  FIG. 11 is a schematic configuration diagram of a monitoring device according to the fourth embodiment. As shown in FIG. 11, the monitoring device 1C according to the fourth embodiment includes a base body 2, one or more unmanned air vehicles 3, a string-like member 4 connected to the base body 2 and the unmanned air vehicles 3, A monitoring control unit 5, a load sensor 11, a receiving unit 12, and an elastic elastic member 13 are provided. In FIG. 11, only one unmanned aerial vehicle 3 is shown for easy understanding.

  The elastic expansion / contraction member 13 is a member capable of elastic expansion / contraction. A coil spring or the like can be used as the elastic elastic member 13. The elastic elastic member 13 is connected to the base body 2 and the intermediate portion of the string-like member 4 in a state where the string-like member 4 is slack. The connection position of the string-like member 4 to which the elastic stretchable member 13 is connected is not particularly limited. If the string-like member 4 is slack in the natural state of the elastic stretchable member 13, the string-like member 4 The elastic elastic member 13 may be connected at any position. The load sensor 11 may be connected between the elastic member 13 and the base 2 or may be connected between the string-like member 4 and the base 2. FIG. 11 shows a form in which the load sensor 11 is connected between the elastic elastic member 13 and the base 2.

  As described above, in the monitoring device 1C of the present embodiment, even if the unmanned air vehicle 3 moves away from the base body 2 vigorously, the elastic elastic member 13 elastically expands and contracts, so that the tensile load acting on the string member 4 Can be raised slowly. Thereby, it can suppress that the string-like member 4 is disconnected. In addition, since the elastic stretch member 13 is connected to the base 2 and the middle portion of the string member 4 in a state where the string member 4 is slack, the stretch of the elastic stretch member 13 is inhibited by the string member 4. The string-like member 4 can be connected to the base 2 while suppressing the above.

(Fifth embodiment)
Next, a fifth embodiment will be described. The fifth embodiment is basically the same as the first embodiment, but only the flight control of the unmanned air vehicle is different from the first embodiment. For this reason, below, only the matter which is different from 1st embodiment is demonstrated, and description of the matter similar to 1st embodiment is abbreviate | omitted.

  As shown in FIGS. 1 and 2, the monitoring control unit 5 adjusts the flight position of the unmanned air vehicle 3 based on the image captured by the monitoring camera 7. If it demonstrates concretely, the monitoring control part 5 synthesize | combines the several image transmitted from the transmission control part 82 of each unmanned air vehicle 3 to one plane image. An image synthesized with one planar image is referred to as a synthesized image. And the monitoring control part 5 adjusts the flight position of each unmanned air vehicle 3 so that a synthesized image becomes favorable. Here, that the composite image is good means that the monitoring target is appropriately included in the composite image. The monitoring target appropriately included in the composite image means that the monitoring target is included in the composite image in a monitorable manner. Whether the composite image is good or not may be determined by human judgment or may be performed by image processing or the like in the monitoring control unit 5.

  Here, among the plurality of unmanned air vehicles 3, adjacent unmanned air vehicles 3 are defined as a first unmanned air vehicle 3a and a second unmanned air vehicle 3b, and are mounted on the first unmanned air vehicle 3a and the second unmanned air vehicle 3b. Consider a case in which the building D surrounded by the temporary enclosure C at the building site is imaged by the monitoring camera 7. However, the flight control of the unmanned air vehicle in the present embodiment is applied not only to the flight control of the first unmanned air vehicle 3a and the second unmanned air vehicle 3b but also to the flight control of one or more unmanned air vehicles 3. Can do.

  12-14 is a figure for demonstrating the image imaged by the adjacent unmanned air vehicle, (a) of FIGS. 12-14 is a 1st unmanned air vehicle, a 2nd unmanned air vehicle, temporary. The figure which shows the positional relationship of an enclosure and a building, (b) of FIGS. 12-14 shows the synthesized image of the image imaged with the 1st unmanned air vehicle 3a and the 2nd unmanned air vehicle 3b.

  As shown in FIG. 12, when the first unmanned air vehicle 3a and the second unmanned air vehicle 3b are flying at good positions, the first unmanned air vehicle 3a is imaged by the surveillance camera 7 mounted on the first unmanned air vehicle 3a. A part of the image overlaps with a part of the image captured by the monitoring camera 7 mounted on the second unmanned air vehicle 3b. For this reason, the synthesized image obtained by synthesizing these images is a continuous image as a whole. A plurality of images can be combined as follows, for example. As a first method, first, a plurality of points serving as landmarks are arranged in the imaging region. Then, this point is extracted from the captured image, and the positional relationship between the images is calculated. Then, based on the calculated positional relationship, a plurality of images are synthesized. As a second method, first, the shape of the temporary enclosure C is registered. Then, the temporary enclosure C is extracted from the captured image, and the positional relationship between the images is calculated by comparing the extracted shape of the temporary enclosure C with the registered shape of the temporary enclosure C. Then, based on the calculated positional relationship, a plurality of images are synthesized. However, synthesis of a plurality of images is not limited to these methods, and can be performed by various methods.

  On the other hand, as shown in FIG. 13, when the first unmanned air vehicle 3a and the second unmanned air vehicle 3b are flying too far, the surveillance camera 7 mounted on the first unmanned air vehicle 3a. There is a region that has not been captured between the image captured by the above and the image captured by the surveillance camera 7 mounted on the second unmanned air vehicle 3b. Therefore, a composite image obtained by combining these images is a discontinuous image with a gap. In this case, the monitoring control unit 5 causes at least one of the first unmanned air vehicle 3a and the second unmanned air vehicle 3b to fly in a direction approaching each other.

  As shown in FIG. 12, when the first unmanned air vehicle 3a and the second unmanned air vehicle 3b are flying at a good height with respect to the temporary enclosure C and the building D, the first unmanned air vehicle 3a And the whole of the temporary enclosure C and the building D fits in an appropriate size in the composite image of the images captured by the second unmanned air vehicle 3b.

  On the other hand, as shown in FIG. 14, when the first unmanned air vehicle 3a and the second unmanned air vehicle 3b are flying at a position that is too low (too close) to the temporary enclosure C and the building D, The building D or both the building D and the temporary enclosure C protrude from the composite image of the images taken by the first unmanned air vehicle 3a and the second unmanned air vehicle 3b. In this case, the supervisory control unit 5 causes the first unmanned air vehicle 3a and the second unmanned air vehicle 3b to fly to positions above the present.

  In addition, as a case where a synthesized image is not favorable, it is not limited to these examples. For example, there is a case where an image captured by the monitoring camera 7 mounted on the first unmanned air vehicle 3a and an image captured by the monitoring camera 7 mounted on the second unmanned air vehicle 3b are shifted in a predetermined direction. is there. In this case, the monitoring controller 5 causes the first unmanned air vehicle 3a and the second unmanned air vehicle 3b to fly to positions that approach each other in a predetermined direction.

  Next, the flight position adjustment process of the unmanned air vehicle 3 will be described with reference to FIGS. 15 and 16. FIG. 15 is a flowchart showing image display processing. FIG. 16 is a flowchart showing the flight position adjustment process.

  As shown in FIGS. 1, 2, and 15, first, imaging by the monitoring camera 7 is started in a plurality of unmanned air vehicles 3 (S <b> 21). Then, the transmission control unit 82 transmits the image captured by the monitoring camera 7 to the monitoring control unit 5 (S22).

  When the monitoring control unit 5 receives the images transmitted from the transmission control unit 82 of each unmanned air vehicle 3, the monitoring control unit 5 combines these images to create one combined image (S23). Then, the monitoring control unit 5 displays the created composite image on the display device (S24).

  Next, as shown in FIGS. 1, 2, and 16, image determination of the composite image displayed on the display device in step S24 is performed (S31). In the image determination, it is determined whether or not the composite image is good. The case where the composite image is good means, for example, the case where the entire monitoring target is included and the image is a continuous image without a gap, as shown in FIG. On the other hand, the case where the composite image is not good is, for example, a case where the image is a non-continuous image with a gap as shown in FIG. 13 or a case where the monitoring target protrudes from the composite image as shown in FIG. (See FIG. 14). Note that the image determination in step S31 may be performed by human judgment, or may be performed by image processing or the like in the monitoring control unit 5.

  And when it determines with a synthesized image being favorable (S31: YES), the flight position adjustment process of the unmanned air vehicle 3 is complete | finished.

  On the other hand, when it determines with a synthesized image being unsatisfactory (S31: NO), the monitoring control part 5 acquires the position data which show the present position of the unmanned air vehicle 3 (S32).

  Next, the flight position of the unmanned air vehicle 3 where the composite image is good is calculated as the change position (S33). For example, in the case of the composite image shown in FIG. 13, the flight position of the unmanned air vehicle 3 where the composite image is good is the position in the direction in which the adjacent unmanned air vehicles 3 approach each other, and in the case of the composite image shown in FIG. 14. Is a position above the current position.

  Next, the monitoring control unit 5 instructs the flight control unit 81 of the unmanned air vehicle 3 to fly at the calculated changed position (S35). Then, the flight control unit 81 moves the unmanned air vehicle 3 to the change position commanded from the monitoring control unit 5 and causes the unmanned air vehicle 3 to fly at the change position. And the flight position adjustment process of the unmanned air vehicle 3 is complete | finished.

  As described above, in the monitoring device 1 according to the present embodiment, since the imaging region of the monitoring camera 7 changes depending on the flight position of the unmanned air vehicle 3, the monitoring control unit 5 performs the unmanned flight based on the image captured by the monitoring camera 7. By adjusting the flight position of the body 3, the area to be monitored can be appropriately imaged.

  Further, in this monitoring device 1, if there is a region that is not captured between images captured by the monitoring camera 7 mounted on the adjacent unmanned air vehicle 3, the monitoring control unit 5 causes these unmanned air vehicles 3 to be detected. Since they are close to each other, it is possible to suppress the occurrence of a region that is not imaged.

  Moreover, in this monitoring apparatus 1, when the monitoring target protrudes from the image captured by the monitoring camera 7, the monitoring control unit 5 causes the unmanned air vehicle 3 to fly to a position above the current position. Images can be taken by the monitoring camera 7.

  Further, in this monitoring device 1, since the monitoring control unit 5 that controls the unmanned air vehicle 3 is provided at a place different from the unmanned air vehicle 3, an operator or the like is based on the image captured by the monitoring camera 7. The unmanned air vehicle 3 can be caused to fly at an optimal position.

  The preferred embodiment of the present invention has been described above, but the present invention is not limited to the above embodiment.

  For example, in the above-described embodiment, the control unit has been described as being divided into a flying object control unit mounted on an unmanned air vehicle and a monitoring control unit provided at a location different from the unmanned air vehicle. Part or all of the processing performed by the body control unit may be performed by the monitoring control unit, and part or all of the processing performed by the monitoring control unit may be performed by the flying object control unit.

  In the above embodiment, the unmanned aerial vehicle is described as being supplied with power from the base side by the string-like member. However, the battery is mounted on the unmanned aerial vehicle and the string-like member does not supply power to the unmanned aerial vehicle. It is good.

  Moreover, although 2nd embodiment demonstrated as what detects the disconnection of a string-like member based on the detection presence or absence of the signal transmitted to the signal line of a string-like member, the disconnection detection of a string-like member is based on this method. It is not limited and any method may be adopted.

  Moreover, although 2nd embodiment demonstrated as what transmits a tensile load to an unmanned air vehicle by the signal wire | line of a string-like member, it is good also as what transmits a tensile load to an unmanned air vehicle wirelessly.

  In the second embodiment, the load sensor, which is a transmission unit, is connected to the base side of the signal line, and the reception unit is connected to the unmanned air vehicle side of the signal line, but the transmission unit and the reception unit are It may be connected reversely. That is, the transmission unit may be connected to either the signal line base or the unmanned air vehicle, and the reception unit may be connected to either the signal line base or the unmanned air vehicle.

  Moreover, although 2nd embodiment demonstrated as what performs both disconnection detection and tensile load detection, you may perform only disconnection detection, without performing tensile load detection.

  In the fifth embodiment, when there is only one unmanned air vehicle 3, the image transmitted from the unmanned air vehicle 3 may be used in place of the composite image without performing step S23. . Similarly, when there are a plurality of unmanned aerial vehicles 3, an image transmitted from the unmanned aerial vehicle 3 may be used in the subsequent processes without performing step S <b> 23.

  In addition, each said embodiment can be combined suitably.

1, 1A, 1B, 1C ... monitoring device, 2 ... base, 2a ... tower crane, 3 ... unmanned flying vehicle, 3a ... first unmanned flying vehicle, 3b ... second unmanned flying vehicle, 4 ... string-like member, 5 ... Monitoring control unit (control unit), 6 ... Power supply source, 6a ... Battery, 7, 7b, 7c ... Monitoring camera, 8 ... Aircraft control unit (control unit), 11 ... Load sensor, 12 ... Receiving unit, 13 ... Elastic expansion / contraction member, 81 ... flight control unit, 82 ... transmission control unit, 83 ... imaging control unit, 84 ... disconnection detection unit, 85 ... load determination unit, A ... suspended load, B1, B2 ... joined member, C ... temporary Enclosure, D ... A building.

Claims (15)

A substrate;
An unmanned air vehicle,
A string-like member connected to the base body and the unmanned air vehicle,
A surveillance camera mounted on the unmanned air vehicle,
A control unit for controlling the unmanned aerial vehicle,
The base is a movable body capable of moving,
Monitoring device. A substrate;
An unmanned air vehicle,
A string-like member connected to the base body and the unmanned air vehicle,
A surveillance camera mounted on the unmanned air vehicle,
A control unit for controlling the unmanned air vehicle;
A disconnection detection unit that detects disconnection of the string-like member,
Monitoring device. A signal line provided along the string-like member;
A transmitter connected to either one of the base of the signal line and the unmanned air vehicle,
A receiver connected to the other side of the base of the signal line and the unmanned air vehicle, and
The transmitter transmits a signal to the receiver through the signal line,
The disconnection detection unit determines that the string-like member is disconnected when the reception unit cannot receive the signal,
The monitoring device according to claim 2. The controller is configured to cause the unmanned air vehicle to fly to a set position when the disconnection of the string-like member is detected by the disconnection detector.
The monitoring device according to claim 2 or 3. The control unit stops imaging by the monitoring camera when a disconnection of the string-like member is detected by the disconnection detection unit,
The monitoring apparatus as described in any one of Claims 2-4. It further comprises a load detection unit that detects a tensile load acting on the string-like member,
The monitoring apparatus as described in any one of Claims 2-5. When the tensile load detected by the load detection unit exceeds a threshold, the control unit causes the unmanned air vehicle to fly in a direction in which the string-like member is loosened.
The monitoring device according to claim 6. The control unit is a flying object control unit mounted on the unmanned flying object,
The monitoring apparatus as described in any one of Claims 2-7. A substrate;
Multiple unmanned air vehicles,
A string-like member connected to the base body and the unmanned air vehicle,
A surveillance camera mounted on the unmanned air vehicle,
A control unit for controlling the unmanned aerial vehicle,
The control unit adjusts a flight position of the unmanned air vehicle based on an image captured by the monitoring camera.
Monitoring device. The control unit includes a region that is not captured between the images captured by the monitoring cameras mounted on the adjacent first unmanned air vehicle and the second unmanned air vehicle among the plurality of unmanned air vehicles. In this case, it is characterized in that at least one of the first unmanned air vehicle and the second unmanned air vehicle is caused to fly in a direction approaching each other,
The monitoring device according to claim 9. When the monitoring target protrudes from the image captured by the monitoring camera, the control unit causes the unmanned air vehicle to fly to a position above the current position.
The monitoring device according to claim 9 or 10. The control unit is a monitoring control unit provided in a place different from the unmanned air vehicle,
The monitoring apparatus as described in any one of Claims 9-11. The string-like member has a power supply line that supplies electric power to the unmanned air vehicle from the base side.
The monitoring apparatus as described in any one of Claims 1-12. It further comprises an elastic elastic member connected between the base and the string-like member,
The monitoring device according to any one of claims 1 to 13. It further comprises an elastic stretchable member connected to the base and an intermediate portion of the string-like member in a state where the string-like member is loosened,
The monitoring apparatus as described in any one of Claims 1-14.

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