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公开(公告)号：AU2016245380B2
公开(公告)日：2020-03-05
申请号：AU2016245380
申请日：2016-04-07
Applicant: BAE SYSTEMS PLC
Abstract: A counter measure apparatus and method for modifying a path of an electromagnetic detector signal (204) so as to prevent incidence thereof on a platform (200), the apparatus comprising an electromagnetic radiation source, communicably coupled to a control system. The control system is configured to create an atmospheric element (202) operative to simulate a physical electromagnetic radiation path modifying device within an atmospheric volume located in said electromagnetic detector signal path (204) by causing electromagnetic radiation from the source to be applied to a selected plurality of three-dimensional portions of said atmospheric volume so as to heat and/or ionise the air within said portions, wherein said selected portions are spatially located together in a substantially unbroken, three-dimensional configuration.
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公开(公告)号：AU2016344526A1
公开(公告)日：2018-05-10
申请号：AU2016344526
申请日：2016-10-28
Applicant: BAE SYSTEMS PLC
Inventor： WRIGHT JULIAN DAVID , COLOSIMO NICHOLAS GIACOMO ROBERT , WARSOP CLYDE
Abstract: An air vehicle (10) comprising a main body (12) and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body(12) having a principal axis orthogonal to the longitudinal axis(20) of said wing members, at least a first propulsion device (16a) associated with a first of said wing members arranged and configured to generate a linear thrust relative to the main body in a first direction, and a second propulsion device (16b) associated with a second of said wing members arranged and configured to generate linear thrust relative to said main body in a second, substantially opposite, direction such that said wing members and said main body are caused to rotate about said principal axis, in use, the air vehicle further comprising an imaging system (100) configured to cover a substantially 360o imaging area about said principal axis and comprising at least one electro-optic sensor (102) mounted on a support member (104) and having a field of view (102a) covering a portion of said imaging area, said support member being mounted on said air vehicle, said imaging system (100) further comprising a control module (400) configured to define an object or region of interest in relation to said air vehicle, determine a nominal sensor field of view incorporating said object or region of interest, and obtain sequential image data from a sensor having a field of view matching said nominal field of view as said air vehicle completes a rotary cycle.
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公开(公告)号：AU2016246105A1
公开(公告)日：2017-10-26
申请号：AU2016246105
申请日：2016-04-11
Applicant: BAE SYSTEMS PLC
Inventor： COLOSIMO NICHOLAS GIACOMO ROBERT
Abstract: A holographic projector apparatus comprising an electromagnetic radiation source (204) communicably coupled to a control system and a three dimensional (3D) image projector (202) for outputting a plurality of image signals (200) representative of a subject, the control system being configured to cause electromagnetic radiation to be applied to a plurality of sets of selected three-dimensional portions of a gaseous volume so as to heat and/or ionise the gas within said selected portions, wherein each set of selected three-dimensional portions of said gaseous volume intersects a path of a respective one of said image signals (200), and wherein said selected portions of each of said set are spatially located together in a substantially unbroken three-dimensional configuration and selectable orientated and configured to simulate an electromagnetic radiation path modifying element (208) for directing a respective image signals incident thereon to a selected location within a viewing region (210).
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公开(公告)号：AU2016245380A1
公开(公告)日：2017-10-26
申请号：AU2016245380
申请日：2016-04-07
Applicant: BAE SYSTEMS PLC
Abstract: A counter measure apparatus and method for modifying a path of an electromagnetic detector signal (204) so as to prevent incidence thereof on a platform (200), the apparatus comprising an electromagnetic radiation source, communicably coupled to a control system. The control system is configured to create an atmospheric element (202) operative to simulate a physical electromagnetic radiation path modifying device within an atmospheric volume located in said electromagnetic detector signal path (204) by causing electromagnetic radiation from the source to be applied to a selected plurality of three-dimensional portions of said atmospheric volume so as to heat and/or ionise the air within said portions, wherein said selected portions are spatially located together in a substantially unbroken, three-dimensional configuration.
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公开(公告)号：AU2016245369A1
公开(公告)日：2017-10-26
申请号：AU2016245369
申请日：2016-04-07
Applicant: BAE SYSTEMS PLC
Inventor： COLOSIMO NICHOLAS GIACOMO ROBERT
Abstract: A long range electromagnetic radiation sensor apparatus comprising a sensing system for receiving electromagnetic radiation signals from an object or area of interest and at least one electromagnetic radiation sensor, the apparatus further comprising an electromagnetic radiation source and a control system configured to cause electromagnetic radiation from said source to be applied to a selected plurality of three- dimensional portions of an atmospheric volume between said optical system and said object or area of interest (204) so as to heat and/or ionise the air within said portions, wherein said selected portions are spatially located together in a three-dimensional configuration so as to simulate an electromagnetic radiation path modifying device (202) for capturing said electromagnetic signals from said object or area of interest and directing and/or converging said captured signals toward said electromagnetic radiation sensor of said sensing system.
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Patent Agency Ranking
公开(公告)号：ES2980472T3
公开(公告)日：2024-10-01
申请号：ES19762196
申请日：2019-08-28
Applicant: BAE SYSTEMS PLC
Inventor： COLOSIMO NICHOLAS GIACOMO ROBERT
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公开(公告)号：AU2016246105B2
公开(公告)日：2021-03-04
申请号：AU2016246105
申请日：2016-04-11
Applicant: BAE SYSTEMS PLC
Inventor： COLOSIMO NICHOLAS GIACOMO ROBERT
Abstract: A holographic projector apparatus comprising an electromagnetic radiation source (204) communicably coupled to a control system and a three dimensional (3D) image projector (202) for outputting a plurality of image signals (200) representative of a subject, the control system being configured to cause electromagnetic radiation to be applied to a plurality of sets of selected three-dimensional portions of a gaseous volume so as to heat and/or ionise the gas within said selected portions, wherein each set of selected three-dimensional portions of said gaseous volume intersects a path of a respective one of said image signals (200), and wherein said selected portions of each of said set are spatially located together in a substantially unbroken three-dimensional configuration and selectable orientated and configured to simulate an electromagnetic radiation path modifying element (208) for directing a respective image signals incident thereon to a selected location within a viewing region (210).
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公开(公告)号：AU2019285841A1
公开(公告)日：2021-01-07
申请号：AU2019285841
申请日：2019-06-13
Applicant: BAE SYSTEMS PLC
Inventor： COLOSIMO NICHOLAS GIACOMO ROBERT , RIGBY KEITH ANTONY
IPC: F41H13/00
Abstract: XA5299 20Apparatus for a Directed-Energy Weapon An apparatus for a directed-energy weapon comprises: anassessment systemarranged to, during an assessment phase,perform an assessment of a target environment, wherein the target environment comprises a target, and the assessment comprises determining a possible engagement efficiency of the target by the directed-energy weapon; and a controller arranged to, during an engaging phase, control the directed-energy weapon to direct energy towards the target environment conditionally upon the possible engagement efficiency. Figure 4
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公开(公告)号：AU2016344527A1
公开(公告)日：2018-05-10
申请号：AU2016344527
申请日：2016-10-28
Applicant: BAE SYSTEMS PLC
Inventor： WRIGHT JULIAN DAVID , COLOSIMO NICHOLAS GIACOMO ROBERT , WARSOP CLYDE
Abstract: An air vehicle (10) comprising a main body (12)and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body (12), at least a first propulsion device (16) associated with a first of said wing members (14a) and a second propulsion device (16) associated with a second of said wing members (14b), each said propulsion device (16) being arranged and configured to generate linear thrust relative to said main body (12), in use, the air vehicle further comprising a control module for generating a control signal configured to change a mode of flying of said air vehicle, in use, between a fixed wing mode (Figure 2) and a rotary wing mode (Figure 3), wherein, in said fixed wing mode of flying, the direction of thrust generated by the first propulsion device (16) relative to the main body (12) is the same as the direction of thrust generated by the second propulsion device (16), and in said second mode of flying, the direction of thrust generated by the first propulsion device (16) relative to the main body is opposite to that generated by the second propulsion device (16).
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公开(公告)号：AU2016245376A1
公开(公告)日：2017-10-26
申请号：AU2016245376
申请日：2016-04-07
Applicant: BAE SYSTEMS PLC
Abstract: A directed-energy weapon counter measure apparatus and method for modifying a path of a focused electromagnetic energy beam(204) emitted by a directed energy weapon system so as to deflect it from a platform(200), the apparatus comprising an electromagnetic radiation source, communicably coupled to a control system. The control system is configured to create an atmospheric element (202) operative to simulate a physical electromagnetic radiation path modifying device within an atmospheric volume located in the path of the focused electromagnetic radiation beam(204) by causing electromagnetic radiation from the source to be applied to a selected plurality of three-dimensional portions of said atmospheric volume so as to heat and/or ionise the air within said portions, wherein said selected portions are spatially located together in a substantially unbroken, three-dimensional configuration.
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