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公开(公告)号:US11521504B2
公开(公告)日:2022-12-06
申请号:US16822999
申请日:2020-03-18
Applicant: Rosemount Aerospace Inc.
Inventor: Robert Rutkiewicz , Joseph T. Pesik
Abstract: Apparatus and associated methods relate to ranging object(s) nearby an aircraft using triangulation. A light projector mounted at a projector location on the aircraft projects pulses of polarized light onto the scene external to the aircraft. The projected pulses of polarized light are polarized in a first polarization state. A camera mounted at a camera location on the aircraft has a shutter synchronized to the projector output pulse and receives a portion of the projected pulses of polarized light reflected by the object(s) in the scene and polarized at a second polarization state orthogonal to the first polarization state. Location(s) and/or range(s) of the object(s) is calculated, based on the projector location, the camera location, and pixel location(s) upon which the portion of light is imaged.
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公开(公告)号:US20190310373A1
公开(公告)日:2019-10-10
申请号:US15949713
申请日:2018-04-10
Applicant: Rosemount Aerospace Inc.
Inventor: Robert Rutkiewicz , Todd Anthony Ell , Joseph T. Pesik
Abstract: Apparatus and associated methods relate to ranging an object in a scene external to an aircraft. A light projector and two cameras are mounted on the aircraft, the cameras at two locations distinct from one another. The light projector and the two cameras are coordinated so that the light projector projects a linear-patterned beam of light while the cameras simultaneously capture a row or column of image data corresponding to an active row or column of pixels upon which a linear-patterned beam of light projected by the light projector and reflected by the scene is focused. Range to the object is calculated using triangulation based on the captured rows or columns of image data and the distinct locations of the two cameras from which the image data are simultaneously captured.
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公开(公告)号:US20190066523A1
公开(公告)日:2019-02-28
申请号:US15683215
申请日:2017-08-22
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Robert Rutkiewicz , Todd Anthony Ell
Abstract: Apparatus and associated methods relate to controlling, based on a mode selector, the field of view of an external object detector during aircraft taxi operations. For example, during high-speed taxi operations, the field of view can be controlled to have a relatively-small solid-angle of detection capability. The relatively-small solid-angle field of view can be aligned so as to detect more distant objects within a narrow corridor extending forward of the aircraft's wingtips. During low-speed taxi operations, for example, the field of view can be controlled to have a relatively-large solid-angle of detection capability. The relatively-large solid-angle field of view can be aligned so as to detect close objects in the vicinity of the aircraft wings and engine nacelle. The object detector projects structured light within the controlled field of view, thereby illuminating the object(s) external to the aircraft that are within the illumination field of view.
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公开(公告)号:US12170029B2
公开(公告)日:2024-12-17
申请号:US17886147
申请日:2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Jonathan Boer
IPC: G08G5/06 , B64D45/00 , B64D47/08 , G06T7/13 , G06T7/246 , G06T7/70 , G06T7/73 , G06V10/22 , G06V10/75 , G06V10/82 , G06V20/10 , G06V20/17 , G06V20/52 , G06V20/56 , G06V20/64 , G06V40/10 , H04N7/18 , B64C1/14 , B64C25/36 , B64D25/14
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an evacuation slide deployment path is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to identify a region within the captured image data that corresponds to the evacuation slide deployment path, determine whether the evacuation slide deployment path will generate a failed deployment outcome, and produce a warning associated with the evacuation slide deployment path in response to determining that the evacuation slide deployment path will generate the failed deployment outcome.
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公开(公告)号:US20230050216A1
公开(公告)日:2023-02-16
申请号:US17886185
申请日:2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Jonathan Boer
IPC: G06V20/52 , H04N7/18 , G06V10/22 , G06V40/10 , G06V10/82 , G06T7/246 , G06T7/70 , G06V10/75 , B64D47/08 , B64D45/00
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an engine inlet of an engine of the aircraft is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to determine whether persons or foreign objects are present near the engine inlet, or detect damage or deformation of the engine inlet.
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公开(公告)号:US10559213B2
公开(公告)日:2020-02-11
申请号:US15450835
申请日:2017-03-06
Applicant: Rosemount Aerospace Inc.
Inventor: Todd Anthony Ell , Robert Rutkiewicz , Joseph T. Pesik
IPC: G08G5/04 , H04N7/18 , H04N5/33 , H04N5/225 , B64D47/08 , G08G5/06 , G06K9/20 , B64F1/00 , G06K9/00 , B64D47/02 , G06T7/55 , G06T7/521
Abstract: Apparatus and associated methods relate to ranging object(s) nearby an aircraft using triangulation of pulses of spatially-patterned light projected upon and reflected by the object(s). The projected pulses provide rapidly-changing illumination of a spatially patterned portion of the scene. A camera receives a reflected portion of the projected pulse and focuses the received portion onto a plurality of light-sensitive pixels, thereby forming a pulse image. The pulse image includes pixel data indicative of a rate of change of light intensity focused thereon exceeding a predetermined threshold. Pixel coordinates, corresponding to a subset of the plurality of light-sensitive pixels that are indicative of the rate of change of light intensity exceeding a predetermined threshold, are identified. Trajectory and/or range data of object(s) in the scene are calculated, based on a projector location, a camera location, and the identified pixel coordinates.
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公开(公告)号:US10371812B2
公开(公告)日:2019-08-06
申请号:US15440796
申请日:2017-02-23
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Todd Anthony Ell
IPC: G01S13/88 , G01S13/02 , G01S13/10 , G01S7/02 , G08G5/00 , H01Q1/28 , G01S7/03 , B64C39/02 , G01S13/93
Abstract: A system can include an unmanned aerial vehicle and an altimeter disposed on the unmanned aerial vehicle. The altimeter can include an ultra-wideband radar antenna disposed orthogonally to a plane of straight and level flight of the unmanned aerial vehicle and having an omnidirectional azimuthal beam pattern orthogonal to the plane of straight and level flight of the unmanned aerial vehicle. The altimeter can be configured to determine an altitude of the unmanned aerial vehicle above a target surface based on time of flight of radar pulses between the ultra-wideband radar antenna and the target surface.
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公开(公告)号:US20180301045A1
公开(公告)日:2018-10-18
申请号:US15489369
申请日:2017-04-17
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Todd Anthony Ell , Robert Rutkiewicz
CPC classification number: G08G5/065 , B64D47/08 , B64F1/002 , G06K9/00812 , G06K9/2018 , G06K9/2036 , G06K2009/3225 , G06T7/13 , G06T7/73 , G06T2207/10016 , G06T2207/10048 , G06T2207/30204 , G06T2207/30264 , G08G5/0021 , G08G5/045 , H04N5/33 , H04N7/183
Abstract: Apparatus and associated methods relate to using an image of a fiducial located indicating a parking location for the aircraft to provide docking guidance data to a pilot of an aircraft. The fiducial has vertically-separated indicia and laterally-separated indicia. A camera is configured to mount at a camera location so as to be able to capture two-dimensional images of a scene external to the aircraft. The two-dimensional image includes pixel data generated by the two-dimensional array of light-sensitive pixels. A digital processor identifies first and second sets of pixel coordinates corresponding to the two vertically-separated and the two laterally-separated indicia, respectively. The digital processor then calculates, based at least in part on the identified first pixel coordinates corresponding to the two vertically-separated indicia, a range to the parking location.
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公开(公告)号:US10043404B2
公开(公告)日:2018-08-07
申请号:US15385224
申请日:2016-12-20
Applicant: Rosemount Aerospace Inc.
Inventor: Todd Ell , Robert Rutkiewicz , Joseph T. Pesik
IPC: B64D47/02 , G08G5/04 , B64D43/00 , B64D47/08 , G01S17/89 , G06K9/00 , G08G5/06 , B64F1/00 , G06T7/50
Abstract: Apparatus and associated methods relate to ranging an object nearby an aircraft by triangulation of spatially-patterned light projected upon and reflected from the object. The spatially patterned light can have a wavelength corresponding to infrared light and/or to an atmospheric absorption band. In some embodiments, images of the object are captured both with and without illumination by the spatially-patterned light. A difference between these two images can be used to isolate the spatially-patterned light. The two images can also be used to identify pixel boundaries of the object and to calculate ranges of portions of the object corresponding to pixels imaging these portions. For pixels imaging reflections of the spatially-patterned light, triangulation can be used to calculate range. For pixels not imaging reflections of the spatially-patterned light, ranges can be calculated using one or more of the calculated ranges calculated using triangulation corresponding to nearby pixels.
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公开(公告)号:US12223850B2
公开(公告)日:2025-02-11
申请号:US17886147
申请日:2022-08-11
Applicant: Rosemount Aerospace Inc.
Inventor: Joseph T. Pesik , Jonathan Boer
IPC: G08G5/06 , B64D45/00 , B64D47/08 , G06T7/13 , G06T7/246 , G06T7/70 , G06T7/73 , G06V10/22 , G06V10/75 , G06V10/82 , G06V20/10 , G06V20/17 , G06V20/52 , G06V20/56 , G06V20/64 , G06V40/10 , H04N7/18 , B64C1/14 , B64C25/36 , B64D25/14
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an evacuation slide deployment path is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to identify a region within the captured image data that corresponds to the evacuation slide deployment path, determine whether the evacuation slide deployment path will generate a failed deployment outcome, and produce a warning associated with the evacuation slide deployment path in response to determining that the evacuation slide deployment path will generate the failed deployment outcome.
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