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公开(公告)号:US20170186330A1
公开(公告)日:2017-06-29
申请号:US15390436
申请日:2016-12-23
Applicant: THALES
Inventor: Emmanuel MONVOISIN , Thierry GANILLE , Johanna LUX , Pierre MARIANI
CPC classification number: G08G5/025 , B64D45/00 , G01C23/005 , G06T17/05 , G06T2200/04 , G06T2207/30241 , G08G5/0021
Abstract: The general field of the invention is that of methods of three-dimensional graphical representation of a landing runway on a viewing screen of an onboard viewing system for aircraft, the said graphical representation being displayed in a synthetic view of an exterior landscape. The graphical representation according to the invention comprises a line disposed along the axis of the runway, the said line being a straight stripe inclined by an angle of between one and a few degrees with respect to the horizontal, the said line beginning at the runway threshold.
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公开(公告)号:US20180010922A1
公开(公告)日:2018-01-11
申请号:US15638218
申请日:2017-06-29
Applicant: THALES
Inventor: Emmanuel MONVOISIN , Xavier SERVANTIE , Pierre MARIANI
CPC classification number: G01C23/005 , G06T17/05 , G08G5/0086
Abstract: A method for three-dimensional graphic representation of the outside landscape in an on-board display system for aircraft comprises a graphical computer and a display screen. The graphic representation is computed to a visibility distance. In the method the zero pitch line of the aircraft forms, with the real horizon line, a first angle, the line representing the limit of the visibility distance forming, with the real horizon line, a second angle, in a first step, the graphical computer determines the maximum visibility distance such that the difference between the first angle and the second angle remains less than a determined value; in a second step, the graphical computer determines the visibility distance as a function of the maximum visibility distance, of the maximum altitude of the relief of the local environment and of the flight phase.
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公开(公告)号:US20170186406A1
公开(公告)日:2017-06-29
申请号:US15394778
申请日:2016-12-29
Applicant: THALES
Inventor: Norbert FRESTEL , Emmanuel MONVOISIN , Pierre MARIANI , Johanna LUX
CPC classification number: G09G5/38 , G01C23/00 , G02B27/01 , G02B2027/014 , G02B2027/0183 , G06T15/20 , G06T17/05 , G06T19/006 , G06T19/20 , G06T2215/16 , G06T2219/2016 , G09G2340/0464 , G09G2380/12
Abstract: The general field of the invention is that of the graphical representation of a synthetic three dimensional view of the exterior landscape in an onboard visualisation system for aircraft, said graphical representation being displayed on a visualisation screen comprising the piloting and navigation information of said aircraft superposed onto said three-dimensional synthetic representation of the exterior landscape, said synthetic representation being computed up to a first determined distance, characterised in that said three-dimensional synthetic representation is tilted at a tilt angle about an axiom positioned at the level of the terrain in a substantially horizontal plane, and substantially perpendicularly to an axis between the flight direction and the heading of the aircraft, said axis moving with the aircraft.
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公开(公告)号:US20240210918A1
公开(公告)日:2024-06-27
申请号:US18542743
申请日:2023-12-17
Applicant: THALES
Inventor: Sébastien RAZE , François COULMEAU , Bruno CAPELLE , Yannick LE ROUX , Pierre MARIANI
IPC: G05B19/4155
CPC classification number: G05B19/4155 , G05B2219/31112
Abstract: A supervision device configured for communicating with a computation device onboard an aircraft, wherein the onboard edge device is configured for executing software applications related with one or a plurality of onboard electronic devices with certified operation, the supervision device comprising a human-machine interface and being configured for receiving, from the edge computation device, observability signals comprising data relating to local computing resources of the onboard edge computation device and information relating to the execution of at least one of the software applications, the supervision device including at least one computing processor configured for computing a state of operation of the edge computation device and a state of execution of the at least one software application from the received observability signals and for displaying the state of operation and the state of execution on the human-machine interface.
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公开(公告)号:US20230377328A1
公开(公告)日:2023-11-23
申请号:US18319431
申请日:2023-05-17
Applicant: THALES
Inventor: Guillaume PABIA , Bruno CAPELLE , Pierre MARIANI , Nicolas COUDER , Ali KARKI , Siegfried ROUZES
Abstract: A method of generating a peripheral image of an aircraft having pixels obtained from a plurality of cameras equipping the aircraft. The method is implemented by an electronic generation device. The method comprises a step of receiving a position of a peripheral point of view from which the peripheral image is to be generated. The method comprises steps of obtaining an orientation of the aircraft and of acquisition of a respective image from each camera. The method comprises a step of calculating a respective transfer function for each camera, each transfer function being intended for being applied to a pixel of the peripheral image so as to identify a possible corresponding pixel of the acquired image associated with the transfer function. The method comprises a step of generating the peripheral image from the images acquired from each camera and from each calculated transfer function.
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6.
公开(公告)号:US20240211313A1
公开(公告)日:2024-06-27
申请号:US18542715
申请日:2023-12-17
Applicant: THALES
Inventor: Sébastien RAZE , François COULMEAU , Bruno CAPELLE , Yannick LE ROUX , Pierre MARIANI
IPC: G06F9/50
CPC classification number: G06F9/5027
Abstract: An edge computation device on board an aircraft is configured for communicating with one or a plurality of onboard electronic devices having certified operation, and with at least one remote computation system. Same includes local computational resources, and is configured for implementing a management module for a plurality of software applications suitable for providing at least one control parameter and/or receiving at least one datum from at least one onboard electronic device, a module for activating the execution of at least one of the stored software applications, a management module for an execution stack, configured for determining, for each software application to be executed, an allocation of local computation resources and, where appropriate, for executing locally a first part of the application, and for requesting remote execution, by means of the remote computation system, of a second part of the application to be executed.
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7.
公开(公告)号:US20170183103A1
公开(公告)日:2017-06-29
申请号:US15394777
申请日:2016-12-29
Applicant: THALES
Inventor: Emmanuel MONVOISIN , Pierre MARIANI , Norbert FRESTEL , Johanna LUX
CPC classification number: B64D43/00 , G01C21/00 , G01C23/00 , G06T17/05 , G06T19/006 , G06T2200/04 , G06T2215/16
Abstract: The general field of the invention is that of the methods for graphic representation of the relative position of the sky and of the earth in an onboard display system for aircraft, said graphic representation being displayed on a display screen comprising piloting and navigation information superimposed on a three-dimensional synthetic representation of the outside landscape. Said graphic representation is displayed only when the attitude of the aircraft is unusual, an unusual attitude corresponding to a roll value or to a pitch value located outside of a first range of nominal values. It comprises two disc segments of identical form, that are opaque and of different colour, situated symmetrically on a circle concentric to that bearing the roll scale, the straight-line segments of the two disc segments being parallel to the line representing the zero longitudinal trim indicator, the rotation of the two disc segments being slaved to the rotation of said zero longitudinal trim indicator.
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