The present technology relates to an information processing device, an information processing method, and a program that enable a mobile device to flexibly correspond to a designated action target. A movement target of the mobile device is calculated on the basis of action target information indicating an action target designating a movement destination of the mobile device and movable space information indicating a movable space which is a range of a real space in which the mobile device is movable.

A power station inspection system and a power station inspection method are disclosed. A power station inspection system includes an unmanned aerial vehicle, and an unmanned aerial vehicle flight controller, a central controller, and at least two types of data collection terminals that are disposed on the unmanned aerial vehicle. The central controller is configured to control the unmanned aerial vehicle flight controller, so that the unmanned aerial vehicle flight controller controls flight of the unmanned aerial vehicle. The central controller is further configured to control the at least two types of data collection terminals to collect at least two types of component image data of a power station component in a flight process of the unmanned aerial vehicle.

A power station inspection system and a power station inspection method are disclosed. A power station inspection system includes an unmanned aerial vehicle, and an unmanned aerial vehicle flight controller, a central controller, and at least two types of data collection terminals that are disposed on the unmanned aerial vehicle. The central controller is configured to control the unmanned aerial vehicle flight controller, so that the unmanned aerial vehicle flight controller controls flight of the unmanned aerial vehicle. The central controller is further configured to control the at least two types of data collection terminals to collect at least two types of component image data of a power station component in a flight process of the unmanned aerial vehicle.

An unmanned aerial vehicle (UAV) may have a positional sensor and an image sensor. The UAV may receive from an electronic structure a first wireless signal. The first wireless signal may include a first direction of illumination. In accordance with the first wireless signal, the UAV may identify a target object based, at least in part, on the first direction of illumination. The UAV may also determine positional coordinates of the target object.

An unmanned aerial vehicle (UAV) may have a positional sensor and an image sensor. The UAV may receive from an electronic structure a first wireless signal. The first wireless signal may include a first direction of illumination. In accordance with the first wireless signal, the UAV may identify a target object based, at least in part, on the first direction of illumination. The UAV may also determine positional coordinates of the target object.

A detector system for detecting at least one of dust, dirt, snow, and ice, comprising: one or more sensors configured to detect the at least one of dust, dirt, snow, and ice; and one or more processors configured to perform instructions, the instructions configured to cause the one or more processors to receive an indication from the one or more sensors relating to a detection of at least one of dust, dirt, snow, and ice, wherein the system comprises a light source, a dust panel, and a light detector.

A detector system for detecting at least one of dust, dirt, snow, and ice, comprising: one or more sensors configured to detect the at least one of dust, dirt, snow, and ice; and one or more processors configured to perform instructions, the instructions configured to cause the one or more processors to receive an indication from the one or more sensors relating to a detection of at least one of dust, dirt, snow, and ice, wherein the system comprises a light source, a dust panel, and a light detector.

An aircraft with a mission computer, a GNSS receiver with a first air interface and a first receiver and a data transmission unit with a second air interface and a second receiver. The data transmission unit can receive data via an encrypted, bidirectional communication path. The mission computer determines a position value for the aircraft based on satellite signals from the GNSS receiver to which a correction term has been applied, which is transmitted to the aircraft by the data transmission unit to determine corrected satellite signals. The corrected satellite signals are the basis for determining corrected position value. The mission computer uses a GNSS receiver and data transmission unit as part of the aircraft. A ground arrangement is provided with an associated ground station and optionally a test unit for checking correct determination of the corrected position value.

A method of discharging a battery assembly used to power at least part of an object includes detecting when power to the object is turned off, detecting, with aid of a timer, an amount of time elapsed since the power to the object is turned off, and initiating a controlled self-discharge of the battery assembly when the amount of time exceeds a threshold length of time. The controlled self-discharge of the battery assembly is performed by a self-discharging circuit electrically coupled to the battery assembly.

The invention is that of a flight data recorder with significant reduction in size, weight and power making it suitable for use with most unmanned aircraft systems (UAS). A flight data recorder of the present invention may be mounted to a UAS or stored in a payload bay or compartment therein. It is an object of the invention to enable programming aircraft flights and recording flight data when autopilot fails, dramatically improving data collection and the ability to determine flight limits and detect problems. An FDR according to the present invention comprises onboard hardware and software systems enabling the programmable collection, storage and processing of flight data along with a means of transferring data to other devices for use. It is an object of the invention to enable wireless data transmissions while maintaining the ability to disable wireless transceivers during flight to prevent interference with flight management signals.