Abstract: An operation management apparatus includes a surrounding environment estimating unit, an energy calculator, and a time changer. The surrounding environment estimating unit is configured to estimate a surrounding environment at a returning start time of a movable body. The energy calculator is configured to search, based on the surrounding environment, a returning route along which the movable body performs the returning, to a first position from a second position, that is started at the returning start time, and calculate an energy amount necessary for the returning. The time changer is configured to advance the returning start time by a predetermined time period until the energy amount reaches or falls below a predetermined value. The surrounding environment estimating unit and the energy calculator are configured to respectively perform the estimation of the surrounding environment and the calculation of the energy amount, each time the time changer changes the returning start time.

Abstract: A stereo distance measuring apparatus includes a first optical camera and a second optical camera, a position-posture calculator, an image corrector, and a stereo distance measuring unit. The first and second optical cameras are provided in an elastic structure part of an aircraft and separated from each other. The first and second optical cameras constitute a stereo camera. The position-posture calculator calculates, on the basis of a displacement amount of the elastic structure part, first and second position-posture information regarding positions and postures of the first and second optical cameras, respectively. The image corrector generates first and second corrected images by correcting, on the basis of the first and second position-posture information, positions and orientations of images taken by the first and second optical cameras, respectively. The stereo distance measuring unit calculates a distance to a photographing target, on the basis of the first and second corrected images.

Abstract: Provided are a stereoscopic distance measuring apparatus and method, and a computer readable program. The apparatus includes first and second optical cameras, first and second position-posture meters, an image corrector, and a stereoscopic distance measuring unit. The first and second position-posture meters acquire first and second position-posture information regarding the first and second optical cameras. The image corrector corrects, on the basis of the first and second position-posture information, positions and orientations of a plurality of first and second images taken by the first and second optical cameras, to generate a plurality of first and second corrected images. The stereoscopic distance measuring unit calculates a distance to a photographing target, on the basis of a pair of the corrected images including one of the plurality of the first corrected images and one of the plurality of the second corrected images.

Abstract: A method of detecting abnormality in an unmanned aircraft control system that allows an unmanned aircraft including a first transceiver and a first directional antenna, and a ground facility including a second transceiver and a second directional antenna, to transmit and receive a signal to and from each other, the method including: calculating an inter-antenna distance from the first directional antenna to the second directional antenna; calculating respective transmission performances of the first directional antenna and the second directional antenna; calculating respective reception performances of the first directional antenna and the second directional antenna; estimating a reception level of a radio wave at each of the first transceiver and the second transceiver; and determining occurrence of abnormality in each of the first transceiver and the second transceiver when a difference between the estimated reception level and an actual reception level is equal to or greater than a predetermined value.

Abstract: A target searching apparatus includes a display, an object region extractor, a feature amount calculator, a second feature amount calculator, and an object present region extractor. The object region extractor extracts, from a display image, an object region including an identification object. The feature amount calculator calculates in-region and out-region representative values of the image feature amount that respectively are representative values inside and outside the object region in the display image. The second feature amount calculator calculates a representative value of the image feature amount in each of a plurality of small regions into which the object region is divided. The object present region extractor extracts, from the plurality of small regions, one or more small region having the representative value that is closer to the in-region representative value than the out-region representative value, as an object present region in which the identification object is present.

Abstract: A flight hindrance display apparatus includes circuitry. The circuitry is configured to acquire surrounding information of an aircraft. The surrounding information is related to a hindrance factor which is a possible flight hindrance to the aircraft. The circuitry is configured to determine a spatial range of the flight hindrance factor on a basis of the acquired surrounding information. The circuitry is configured to determine a flight hindrance cross-section that intersects a plane including a vector of a flight direction of the aircraft and is included in the determined spatial range of the flight hindrance factor. The circuitry is configured to cause a display unit to stereoscopically display an own position of the aircraft, the spatial range of the flight hindrance factor, and the flight hindrance cross-section.

Abstract: A search assisting apparatus includes a line-of-sight trajectory detector, a gaze region extractor, and a target presence determiner. The line-of-sight trajectory detector that detects a line-of-sight trajectory of the operator on an image displayed on a display. The gaze region extractor that extracts, on a basis of the line-of-sight trajectory detected by the line-of-sight trajectory detector, a gaze region gazed by the operator in the image displayed on the display.

Abstract: A flight hindrance display apparatus includes circuitry. The circuitry is configured to acquire surrounding information of an aircraft. The surrounding information is related to the a hindrance factor which is a possible flight hindrance to the aircraft. The circuitry is configured to determine a spatial range of the flight hindrance factor on a basis of the acquired surrounding information. The circuitry is configured to determine a flight hindrance cross-section that intersects a plane including a vector of a flight direction of the aircraft and is included in the determined spatial range of the flight hindrance factor. The circuitry is configured to cause a display unit to stereoscopically display an own position of the aircraft, the spatial range of the flight hindrance factor, and the flight hindrance cross-section.