Control device, system, and method
A control device ( 200 ) includes a ground vehicle controller ( 230 ) that causes a ground vehicle to travel at a target area, an acquirer ( 210 ) that acquires state information expressing a state of a surface of the target area while the ground vehicle travels the target area, and a determiner ( 240 ) that determines, based on the acquired state information, whether or not an aircraft is landable at the target area.
1. A control device, comprising:
at least one memory storing computer program code; and
at least one processor operable to read the computer program code and operate as instructed by the computer program code, wherein
the computer program code includes:
aircraft control code configured to cause the at least one processor to perform control to cause a transport aircraft to lower a ground vehicle to a target area while the transport aircraft is flying above the target area, the transport aircraft being configured to be physically connected to the ground vehicle and being configured to transport the ground vehicle;
ground vehicle control code configured to cause the at least one processor to perform, after the ground vehicle is lowered to the target area, control to cause the ground vehicle to travel the target area while the transport aircraft is flying; and
acquiring code configured to cause the at least one processor to acquire state information expressing a state of a surface of the target area, the state being a state of the surface when the ground vehicle travels the target area,
wherein the aircraft control code is configured to cause the at least one processor to further perform, after the ground vehicle travels the target area, control to cause the transport aircraft to lift the ground vehicle from the target area while the transport aircraft is flying, and
wherein the computer program code further includes determination code configured to cause the at least one processor to determine, based on the acquired state information, whether or not an aircraft is landable at the target area, the aircraft being identical to the transport aircraft or being different from the transport aircraft.
2. The control device according to claim 1 , wherein
the surface of the target area is covered by a covering,
the acquiring code is configured to cause the at least one processor to acquire, as the state information, information expressing an image obtained by imaging, by an imaging device configured to image the covering covering the surface, while the ground vehicle travels on the covering, and
the determination code is configured to cause the at least one processor to determine, based on a change of the covering identified based on the acquired state information, whether or not the aircraft is landable at the target area covered by the covering.
3. The control device according to claim 2 , wherein
the covering includes a predetermined pattern, and
the determination code is configured to cause the at least one processor to determine, based on a change of the pattern of the covering identified based on the acquired state information, whether or not the aircraft is landable at the target area covered by the covering.
4. The control device according to claim 3 , wherein
the ground vehicle includes a detector that is configured to detect an attitude of the ground vehicle while the ground vehicle travels the target area,
the acquiring code is configured to cause the at least one processor to acquire, as the state information, information expressing the detected attitude of the ground vehicle, and
the determination code is configured to cause the at least one processor to determine, based on the attitude of the ground vehicle expressed in the acquired state information, whether or not the aircraft is landable at the target area.
5. The control device according to claim 3 , wherein
the determination code is configured to cause the at least one processor to
identify, based on the change of the pattern of the covering, a characteristic of the surface of the target area covered by the covering, and
determine, based on the identified characteristic of the surface, whether or not the aircraft is landable at the target area.
6. The control device according to claim 5 , wherein
the ground vehicle includes a detector that is configured to detect an attitude of the ground vehicle while the ground vehicle travels the target area,
the acquiring code is configured to cause the at least one processor to acquire, as the state information, information expressing the detected attitude of the ground vehicle, and
the determination code is configured to cause the at least one processor to determine, based on the attitude of the ground vehicle expressed in the acquired state information, whether or not the aircraft is landable at the target area.
7. The control device according to claim 5 , wherein the characteristic of the surface includes any one or more of a size of an unevenness of the surface, a size of an incline of the surface, and a softness of the surface.
8. The control device according to claim 7 , wherein
the ground vehicle includes a detector that is configured to detect an attitude of the ground vehicle while the ground vehicle travels the target area,
the acquiring code is configured to cause the at least one processor to acquire, as the state information, information expressing the detected attitude of the ground vehicle, and
the determination code is configured to cause the at least one processor to determine, based on the attitude of the ground vehicle expressed in the acquired state information, whether or not the aircraft is landable at the target area.
9. The control device according to claim 2 , wherein
the transport aircraft includes the imaging device configured to image the covering, and
the acquiring code is configured to cause the at least one processor to acquire, from the transport aircraft that is configured to transport the ground vehicle, the information expressing the image obtained by imaging while the ground vehicle travels on the covering, as the state information.
10. The control device according to claim 2 , wherein
the ground vehicle includes a detector that is configured to detect an attitude of the ground vehicle while the ground vehicle travels the target area,
the acquiring code is configured to cause the at least one processor to acquire, as the state information, information expressing the detected attitude of the ground vehicle, and
the determination code is configured to cause the at least one processor to determine, based on the attitude of the ground vehicle expressed in the acquired state information, whether or not the aircraft is landable at the target area.
11. The control device according to claim 1 , wherein
the ground vehicle includes a detector that is configured to detect an attitude of the ground vehicle while the ground vehicle travels the target area,
the acquiring code is configured to cause the at least one processor to acquire, as the state information, information expressing the detected attitude of the ground vehicle, and
the determination code is configured to cause the at least one processor to determine, based on the attitude of the ground vehicle expressed in the acquired state information, whether or not the aircraft is landable at the target area.
12. The control device according to claim 1 , wherein the determination code is configured to cause the at least one processor to determine, based on the acquired state information, whether or not the aircraft is capable of taking off from the target area.
13. A system, comprising:
a ground vehicle configured to travel a target area; and
a control device that includes
at least one memory storing computer program code, and
at least one processor operable to read the computer program code and operate as instructed by the computer program code, wherein
the computer program code includes:
aircraft control code configured to cause the at least one processor to perform control to cause a transport aircraft to lower the ground vehicle to the target area while the transport aircraft is flying above the target area, the transport aircraft being configured to be physically connected to the ground vehicle and being configured to transport the ground vehicle;
ground vehicle control code configured to cause the at least one processor to perform, after the ground vehicle is lowered to the target area, control to cause the ground vehicle to travel the target area while the transport aircraft is flying; and
acquiring code configured to cause the at least one processor to acquire state information expressing a state of a surface of the target area, the state being a state of the surface when the ground vehicle travels the target area,
wherein the aircraft control code is configured to cause the at least one processor to further perform, after the ground vehicle travels the target area, control to cause the transport aircraft to lift the ground vehicle from the target area while the transport aircraft is flying, and
wherein the computer program code further includes determination code configured to cause the at least one processor to determine, based on the acquired state information, whether or not an aircraft is landable at the target area, the aircraft being identical to the transport aircraft or being different from the transport aircraft.