To provide a novel and improved information processing device that can make more efficient an inspection performed by a flying body capable of performing imaging. Provided is an information processing device including an imaging position information acquisition unit configured to acquire imaging position information at a time when a structure is imaged which is acquired by an imaging device configured to fly over a periphery of die structure to image the structure on the basis of certain flight information, and a damage data generating unit configured to use a captured image of the structure imaged by the imaging device and the imaging position information and to generate data related to damage of the structure including position information of damage of the structure included in the captured image.

Embodiments include systems and methods for generating 2D and 3D layouts from a physical 3D space captured by a capturing device, the layouts having an identical scale to the physical 3D space, and estimating measurements of the physical 3D space from the layouts. The capturing device captures a point cloud or 3D mesh of the physical 3D space, from which one or more planes are identified. These one or more planes can then be used to create a virtual 3D reconstruction of the captured 3D space. In other embodiments, one plane may be identified as a floor plane, and features from the point cloud or 3D mesh that are above the floor plane may be projected onto the floor plane to create a top down view and 2D layout. Other embodiments are described.

Embodiments include systems and methods for generating 2D and 3D layouts from a physical 3D space captured by a capturing device, the layouts having an identical scale to the physical 3D space, and estimating measurements of the physical 3D space from the layouts. The capturing device captures a point cloud or 3D mesh of the physical 3D space, from which one or more planes are identified. These one or more planes can then be used to create a virtual 3D reconstruction of the captured 3D space. In other embodiments, one plane may be identified as a floor plane, and features from the point cloud or 3D mesh that are above the floor plane may be projected onto the floor plane to create a top down view and 2D layout. Other embodiments are described.

Methods, systems and apparatus, including computer programs encoded on computer storage media for determining a center location of a ground control point used in aerial surveys. Machine learning models are used to identify in digital images pixel coordinates of the ground control point identified in the digital images. These image pixel coordinates are used in photogrammetric processing and software.

According to the invention, the construction measuring device has a functionality for modifying the orientation of the sighting unit in a manually controllable manner, within the framework of which the orientation of the sighting unit is dynamically modified by the first or second rotary drive, according to a current direction and a current distance from a defined central anchor display point to a currently marked display point. The respective current direction defines an orientation modifying direction and the respective current distance defines an orientation modifying speed for changing the orientation of the sighting unit.

According to the invention, the construction measuring device has a functionality for modifying the orientation of the sighting unit in a manually controllable manner, within the framework of which the orientation of the sighting unit is dynamically modified by the first or second rotary drive, according to a current direction and a current distance from a defined central anchor display point to a currently marked display point. The respective current direction defines an orientation modifying direction and the respective current distance defines an orientation modifying speed for changing the orientation of the sighting unit.

A system of reconnaissance for the staging of a mission in a target area of a remote location in space is disclosed, including satellite surveillance means; a plurality of radio beacon/video camera transceiver means; communication means connecting the satellite surveillance means with the plurality of radio beacon/video camera transceiver means; communication means connecting the plurality of radio beacon/video camera transceiver means with at least one base station; and analysis means to analyze video, positional and other data from the target area.

A system of reconnaissance for the staging of a mission in a target area of a remote location in space is disclosed, including satellite surveillance means; a plurality of radio beacon/video camera transceiver means; communication means connecting the satellite surveillance means with the plurality of radio beacon/video camera transceiver means; communication means connecting the plurality of radio beacon/video camera transceiver means with at least one base station; and analysis means to analyze video, positional and other data from the target area.

A photoelectric conversion apparatus includes a photodiode, a counter, a control circuit. The photodiode is configured to cause avalanche multiplication. The counter is configured to generate a count signal as a result of counting a pulse generated by the avalanche multiplication during a predetermined period. The control circuit is configured to perform control to bring the photodiode into a waiting state in which the avalanche multiplication is possible and a stop state in which the avalanche multiplication is stopped, based on the count signal during a predetermined period.

A photoelectric conversion apparatus includes a photodiode, a counter, a control circuit. The photodiode is configured to cause avalanche multiplication. The counter is configured to generate a count signal as a result of counting a pulse generated by the avalanche multiplication during a predetermined period. The control circuit is configured to perform control to bring the photodiode into a waiting state in which the avalanche multiplication is possible and a stop state in which the avalanche multiplication is stopped, based on the count signal during a predetermined period.