Operation system of unmanned aircraft
An operation system includes: a connecting cable; a winder configured to cause a tensile force to act on the connecting cable; a delivered amount detecting section configured to detect the delivered amount of the connecting cable; a direction detecting section configured to detect a direction of a force acting on a to-be-detected part of the connecting cable; and a position determination section configured to determine a position of an unmanned aircraft. The position determination section determines a distance from a predetermined reference position to the unmanned aircraft based on a detection result from the delivered amount detecting section. The position determination section determines an orientation of the unmanned aircraft on the basis of the to-be-detected part based on a detection result from the direction detecting section.
1 . An operation system of an unmanned aircraft, comprising:
a connecting cable comprising a connected part connected to the unmanned aircraft;
a winder configured to wind a redundant part of the connecting cable to cause a tensile force to act on the connecting cable;
a delivered amount detecting section configured to detect a delivered amount of the connecting cable delivered by the winder;
a direction detecting sensor configured to detect a direction of a force acting on a to-be-detected part of the connecting cable between the connected part and the winder; and
a position determination section configured to determine a position of the unmanned aircraft, wherein:
the position determination section determines a distance from a predetermined reference position to the unmanned aircraft based on a detection result from the delivered amount detecting section;
the position determination section determines an orientation of the unmanned aircraft on the basis of the to-be-detected part based on a detection result from the direction detecting sensor,
the position determination section determines the position of the unmanned aircraft based on the distance from the predetermined reference position to the unmanned aircraft and the orientation of the unmanned aircraft on the basis of the to-be-detected part, and
the direction detecting sensor detects a direction of a force acting on the to-be-detected part from at least one of pressure and displacement caused in response to the direction detecting sensor coming into contact with the to-be-detected part.
2 . The operation system of the unmanned aircraft, according to claim 1 , further comprising:
a tensile force detecting section configured to detect a magnitude of a tensile force acting on the connecting cable; and
a state determination section configured to determine a state of the unmanned aircraft, wherein:
in a case where the tensile force detected by the tensile force detecting section is equal to or more than a predetermined crash determination reference value, the state determination section determines that the unmanned aircraft has crashed.
3 . The operation system of the unmanned aircraft, according to claim 2 , further comprising:
a winding control section configured to control the winder, wherein:
in a case where the state determination section determines that the unmanned aircraft has crashed, the winding control section executes a recovery process of winding the connecting cable.
4 . The operation system of the unmanned aircraft, according to claim 1 , further comprising:
a tensile force detecting section configured to detect a magnitude of a tensile force acting on the connecting cable;
a state determination section configured to determine a state of the unmanned aircraft; and
an aircraft control section configured to control the unmanned aircraft, wherein:
in a case where the tensile force detected by the tensile force detecting section is less than a predetermined flight determination reference value although a take-off command to fly while the connecting cable is attached is given to the unmanned aircraft from the aircraft control section, the state determination section determines that the unmanned aircraft does not take off.
5 . The operation system of the unmanned aircraft, according to claim 1 , further comprising:
a power supply; and
a power line provided integrally with the connecting cable, wherein:
the power supply is connected to a power receiving section of the unmanned aircraft via the power line.
6 . The operation system of the unmanned aircraft, according to claim 1 , further comprising:
a takeoff and landing port where the unmanned aircraft takes off and lands, wherein:
the takeoff and landing port is disposed to overlap with at least either of the winder and the direction detecting sensor in a top-bottom view, the at least either of the winder and the direction detecting sensor being positionally fixed relative to the takeoff and landing port.
7 . The operation system of the unmanned aircraft, according to claim 1 , further comprising:
a takeoff and landing port where the unmanned aircraft takes off and lands, wherein:
the unmanned aircraft is configured to fly in a passage space surrounded by a tubular wall extending in an up-down direction to transport an article; and
the takeoff and landing port is disposed at a position connected to the passage space.
8 . The operation system of the unmanned aircraft, according to claim 7 , wherein
the takeoff and landing port is disposed to overlap with the passage space in a horizontal view.
9 . An operation system of an unmanned aircraft, comprising:
a connecting cable comprising a connected part connected to the unmanned aircraft;
a winder configured to wind a redundant part of the connecting cable to cause a tensile force to act on the connecting cable;
a delivered amount detecting section configured to detect a delivered amount of the connecting cable delivered by the winder;
a direction detecting sensor configured to detect a direction of a force acting on a to-be-detected part of the connecting cable between the connected part and the winder;
a position determination section configured to determine a position of the unmanned aircraft;
a takeoff and landing port where the unmanned aircraft takes off and lands, wherein:
the unmanned aircraft is configured to fly in a passage space surrounded by a tubular wall extending in an up-down direction to transport an article; and
the takeoff and landing port is disposed at a position connected to the passage space, wherein:
the position determination section determines a distance from a predetermined reference position to the unmanned aircraft based on a detection result from the delivered amount detecting section;
the position determination section determines an orientation of the unmanned aircraft on the basis of the to-be-detected part based on a detection result from the direction detecting sensor,
the position determination section determines the position of the unmanned aircraft based on the distance from the predetermined reference position to the unmanned aircraft and the orientation of the unmanned aircraft on the basis of the to-be-detected part, and
at least a part of the passage space where the unmanned aircraft is allowed to fly is below at least either of the winder and the direction detecting sensor.
10 . An operation system of an unmanned aircraft, comprising:
a connecting cable comprising a connected part connected to the unmanned aircraft;
a winder configured to wind a redundant part of the connecting cable to cause a tensile force to act on the connecting cable;
a delivered amount detecting section configured to detect a delivered amount of the connecting cable delivered by the winder;
a direction detecting sensor configured to detect a direction of a force acting on a to-be-detected part of the connecting cable between the connected part and the winder; and
a position determination section configured to determine a position of the unmanned aircraft, and
a takeoff and landing port where the unmanned aircraft takes off and lands, wherein:
the position determination section determines a distance from a predetermined reference position to the unmanned aircraft based on a detection result from the delivered amount detecting section;
the position determination section determines an orientation of the unmanned aircraft on the basis of the to-be-detected part based on a detection result from the direction detecting sensor, and
the position determination section determines the position of the unmanned aircraft based on the distance from the predetermined reference position to the unmanned aircraft and the orientation of the unmanned aircraft on the basis of the to-be-detected part, and
the unmanned aircraft is configured to fly in a space below at least either of the winder and the direction detecting sensor positionally fixed relative to the takeoff and landing port.
11 . The operation system of the unmanned aircraft, according to claim 1 , wherein the unmanned aircraft is configured to fly with the connecting cable connected thereto.
12 . The operation system of the unmanned aircraft, according to claim 1 , further comprising:
a takeoff and landing port where the unmanned aircraft takes off and lands, wherein:
the winder is positionally fixed relative to the takeoff and landing port.
13 . The operation system of the unmanned aircraft, according to claim 1 , wherein
the direction detecting sensor detects the direction of a force acting on the to-be-detected part, which direction is orthogonal to a direction of a tensile force at the to-be-detected part.
14 . The operation system of the unmanned aircraft, according to claim 1 , wherein
the direction detecting sensor is on an unmanned aircraft-side relative to the winder.