The present disclosure relates to an information processing device, an information processing method, and a program capable of avoiding a collision with an obstacle more reliably.

An avoidance trajectory setting unit sets an avoidance trajectory on which a flying object can avoid a collision with an obstacle on the basis of position information of the flying object and wind speed information of a flight position represented by the position information. The technology according to the present disclosure can be applied to air traffic control devices and drones.

An aircraft control apparatus (20) includes a display unit (210), a display (220), an input unit (230), a selection unit (240), and a command generation unit (250). The command generation unit (250) acquires an image that has been generated by an image capture unit (350) of an aircraft (30). The display unit (210) displays, on the display (220), the image acquired by the command generation unit (250). The image includes at least one electric wire or at least one pipe that could be an inspection target. The input unit (230) displays, according to an input from a user, a line within the image displayed on the display (220). The selection unit (240) selects an inspection target by use of the line displayed by the input unit (230). The command generation unit (250) generates command information for the aircraft to photograph the inspection target while moving along the inspection target, and transmitting the command information to the aircraft (30).

An unmanned aerial vehicle is caused to fly by avoiding a no-fly zone, which changes as a moving object moves. Provided is an unmanned aerial vehicle control system, including: moving object position acquisition means for acquiring moving object position information on a current position of a moving object moving above a surface of an earth; zone setting means for setting a no-fly zone in which a flight of an unmanned aerial vehicle is inhibited based on the moving object position information; and flight control means for controlling the flight of the unmanned aerial vehicle so that the unmanned aerial vehicle avoids the no-fly zone set based on the moving object position information.

An unmanned aerial vehicle is caused to fly by avoiding a no-fly zone, which changes as a moving object moves. Provided is an unmanned aerial vehicle control system, including: moving object position acquisition means for acquiring moving object position information on a current position of a moving object moving above a surface of an earth; zone setting means for setting a no-fly zone in which a flight of an unmanned aerial vehicle is inhibited based on the moving object position information; and flight control means for controlling the flight of the unmanned aerial vehicle so that the unmanned aerial vehicle avoids the no-fly zone set based on the moving object position information.

A configuration is achieved in which collision risk information is received from a mobile device such as a drone, a modified path with a low collision risk is generated, and movement according to the modified path is performed. Existence of a second mobile device or pedestrian exposed to a collision risk is checked on the basis of collision risk information received from the mobile device such as a drone, and in a case where the existence of the second mobile device or pedestrian exposed to the collision risk is confirmed, collision risk information received from a first mobile device or modified safe circuit information is transmitted to the second mobile device exposed to the collision risk, or transmitted to a user terminal held by the pedestrian exposed to the collision risk. The collision risk information received from the mobile device such as a drone is risk information with which a collision risk corresponding to a three-dimensional spatial position can be analyzed.

To provide an unmanned aerial vehicle remote control device, etc., capable of remotely controlling an unmanned aerial vehicle without using an operation wand and its guide mechanism. An unmanned aerial vehicle remote control device includes a gesture recognition means that recognizes a gesture of an operator's hand based on an image taken by a camera that includes the operator's hand, a control command specification means that specifies a control command to which the gesture of the operator's hand recognized by the gesture recognition means is associated, and a communication means that transmits the control command specified by the control command specification means to the unmanned aerial vehicle.

A distribution device (10) is provided with an acquisition unit (11) which acquires position information of an obstacle, and a distribution unit (12) which wirelessly distributes, from the obstacle to an aircraft, obstacle information including the acquired position information of the obstacle and identification information of the obstacle. The distribution device (10) distributes the identification information of the obstacle along with the position information of the obstacle to the aircraft, and the aircraft interprets the position, etc., of the specific obstacle.

A determination device according to one embodiment includes an acquiring unit (231) and a determination unit (233). The acquiring unit (231) acquires positional information that is related to a terminal device installed at an arbitrary location serving as a reference for a path of an air vehicle and that is calculated on the basis of correction information that includes information on coordinates of a reference station associated with an area in which the terminal device is positioned and information based on a satellite signal received by the reference station. The determination unit (233) determines a flight path of the air vehicle on the basis of the positional information acquired by the acquiring unit.

A system for automated flight correction in an electric aircraft includes an input control configured to generate a control datum, at least a sensor connected to the electric aircraft, wherein the at least a sensor is configured to detect a status datum, and a flight controller communicatively connected to the input control and the at least a sensor, wherein the flight controller is configured to determine a command datum as a function of the control datum and the status datum, wherein determining the command datum comprises comparing the control datum to a limitation set based on the status datum, and calculating a modified control datum based on a flight plan of the electric aircraft through a remote device.

A system for automated flight correction in an electric aircraft includes an input control configured to generate a control datum, at least a sensor connected to the electric aircraft, wherein the at least a sensor is configured to detect a status datum, and a flight controller communicatively connected to the input control and the at least a sensor, wherein the flight controller is configured to determine a command datum as a function of the control datum and the status datum, wherein determining the command datum comprises comparing the control datum to a limitation set based on the status datum, and calculating a modified control datum based on a flight plan of the electric aircraft through a remote device.