Subaru Corporation

Yoichi Onomura

Akihiro Yamane

Akitoshi Sakaguchi

Yutaka Sasaki

Kumiko Kindaichi

Toshiyuki Narahashi

Shinei Takahashi

Yu Itabashi

Iwao Murata

Yukinobu Tomonaga

Takeshi Fukurose

Yu Takahashi

Takashi Nagayama

Takeshi Kibayashi

A deceiving signal detection system includes a first antenna, a second antenna, and a signal processor. The first antenna is configured to receive at least four radio wave signals. The signal processor determines that the radio wave signals are the deceiving signals by determining that a relative positional relation between the first antenna and the second antenna calculated on a basis of the radio wave signals deviates from an actual relative positional relation between the first antenna and the second antenna by more than a predetermined amount, and also determines whether an orientation of the aircraft determined based on positions of the first antenna and the second antenna matches an orientation of the aircraft calculated based on an inertial navigation system.

Deceiving signal detection system and deceiving signal detection method

A navigation system includes a receiver and a signal processor. The receiver is mounted on a second aircraft. The second aircraft is an acquisition target of location information. The receiver is configured to receive a navigation signal from each of three or more first aircrafts. The navigation signal includes the location information on a location of the corresponding first aircraft. The navigation signal is transmitted as a radio signal from a navigation apparatus mounted on each of the three or more first aircrafts. The signal processor is mounted on the second aircraft. The signal processor is configured to calculate a location of the second aircraft on the basis of the navigation signal.

Navigation system, navigation method, and aircraft

A position measurement system includes a movable body and at least one indicator including identification information. The movable body includes an optical sensor configured to acquire an image of the indicator, an information acquisition unit configured to acquire the identification information of the indicator and a bearing of the indicator as seen from the movable body based on the image of the indicator acquired by the optical sensor, a coordinate acquisition unit configured to acquire coordinates of the indicator based on the acquired identification information of the indicator, and a position calculation unit configured to calculate a position of the movable body based on the acquired bearing of the indicator and the acquired coordinates of the indicator. The indicator includes, as the identification information, at least one of a unique reflection spectrum, a spectrum change pattern, a hue change pattern, a brightness change pattern, or a temperature change pattern.

Position measurement system for movable body

A flying object position measuring apparatus includes an optical sensor, a storage, an orientation calculator, and a position calculator. The optical sensor obtains an image of a flying object. The flying object performs flight along a ballistic trajectory. The storage stores, in advance, basic trajectory information regarding a basic trajectory of the flying object. The basic trajectory information includes position information of a start point at which the flying object starts the flight. The orientation calculator calculates an orientation of the flying object as viewed from the optical sensor on the basis of the image obtained by the optical sensor. The position calculator calculates, as a position of the flying object, an intersection of a plane of rotation with the orientation of the flying object. The plane of rotation is a plane based on a rotation of the basic trajectory around a vertical axis that travels through the start point.

Flying object position measuring apparatus, flying object position measuring method, and non-transitory storage medium

There is provided a navigation system, comprising: a buoy on a water surface movably anchored to a bottom; a plurality of at least three transmitters fixed to the bottom or at different positions in the water for transmitting signals to specify the positions; a receiver, being disposed with the buoy, configured to receive signals transmitted by the plurality of transmitters; a signal processor, being disposed with the buoy, configured to specify the position of the buoy, based on the signals received by the receiver, and generate a navigation signal indicating the position of the buoy, and a radio, being disposed with the buoy, configured to transmit the navigation signal generated in the signal processor wirelessly, the navigation signal being receivable by a radio in a mobile body.

Navigation system and navigation method

A position measuring apparatus includes an imaging device and a controller, and is mounted on one or more mobile objects and configured to measure a position of a target. The imaging device is configured to acquire images of the target from a plurality of locations that are different from each other. The controller is configured to measure, on the basis of the images of the target, one or both of orientations of the target as viewed from the respective locations and distances to the target from the respective locations, correct one of the measured orientations of the target and the measured distances to the target to thereby reduce a difference between times at which the respective images are acquired at the respective locations, and calculate an estimated position of the target, on a basis of one of the corrected orientations of the target and the corrected distances to the target.

Position measuring method, position measuring apparatus, and position measuring system

A self-position measuring device includes an information generator, a position extractor, and a navigation method selector. The information generator generates estimated information that is expected to be obtained when at least one of the ground information and the celestial information is obtained, at each of multiple reference points generated on the basis of measured inertial navigation position. The position extractor checks at least the one of the ground information and the celestial information against the estimated information at each of the multiple reference points and extracts a position of a specific reference point corresponding to specific estimated information with a highest matching degree. The navigation method selector selects, on the basis of the specific reference point, a navigation method with less navigational error as a navigation method for measuring the self-position.

Self-position measuring device, self-position measuring method, and non-transitory storage medium

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.

Operation management apparatus, operation management method, and non-transitory recording medium

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.

Method of detecting abnormality in unmanned aircraft control system and abnormality detector

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.

Target searching apparatus, target searching method, and computer readable medium

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.

Stereo distance measuring apparatus, stereo distance measuring method, and computer readable medium

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.

Stereoscopic distance measuring apparatus, stereoscopic distance measuring method, and computer readable medium

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. The target presence determiner that determines, on a basis of a distance from a predetermined position, presence of a predetermined detection target in the gaze region.

Search assisting apparatus, search assisting method, and computer readable medium

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.

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Tokyo, Japan

Yoichi Onomura