Patents Assigned to BAE SYSTEM
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Patent number: 9367819Abstract: A method and apparatus for processing data, the data including: a set of one or more system inputs; and a set of one or more system outputs; wherein each system output corresponds to a respective system input; each system input includes a plurality of data points, a first data point in the plurality and a second data point in the plurality being from a same raw data source, and the first data point being pre-processed using a different pre-processing method relative to a pre-processing method used to pre-process the second data point, the method including: for each of the first and second data points, inferring a value indicative of a significance of the pre-processing method used to pre-process that data point; wherein the inferring includes performing a machine learning algorithm on a given system input from the data and a further system input.Type: GrantFiled: May 31, 2012Date of Patent: June 14, 2016Assignee: BAE SYSTEMS PLCInventors: David Nicholson, Christopher Mark Lloyd, Steven Reece, Stephen John Roberts
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Patent number: 9369438Abstract: An apparatus and method are provided for controlling a transfer of data between data communications networks.Type: GrantFiled: May 21, 2012Date of Patent: June 14, 2016Assignee: BAE SYSTEMS plcInventors: Henry Noel Arnold Harrison, Brenton Shane Cooper, Jason Ross Westmacott
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Patent number: 9366856Abstract: A method of combining and co-aligning a plurality of radiation beams each having a respective waveband, includes the steps of passing each of said radiation beams to a respective lateral deflector to impart a selected lateral displacement to said beam. Each of said radiation beams with respective imparted lateral displacements is then passed to an optical collimating element which passes said radiation beams to an optical deflecting element which applies a wavelength dependent deflection to the radiation beams. The respective lateral displacements are selected having regard to the waveband of each beam to cause all to exit the optical deflecting element at the same angle so they are co-aligned.Type: GrantFiled: June 21, 2013Date of Patent: June 14, 2016Assignee: BAE SYSTEMS plcInventors: Craig Daniel Stacey, Christopher Stace
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Publication number: 20160161257Abstract: A method and apparatus for determining routes vehicles (4, 6), the method comprising: measuring positions of a first vehicle and a second vehicle (6); providing a specification of a region (12) having a fixed position in relation to the first vehicle (4); using the measurements and the region specification, determining a first route for the first vehicle (4) and a second route for the second vehicle (6). Determining the routes comprises: constructing a graph (34) within a joint state space (X) of the vehicles (4, 6); identifying, within the graph (34), a path from a first vertex to a second vertex, the first vertex corresponding to the measured positions of the vehicles (4, 6), and the second vertex corresponding to the second vehicle (6) being at least partially located within the region (12); and, using the identified path, determining the first and second routes.Type: ApplicationFiled: July 7, 2014Publication date: June 9, 2016Applicant: BAE SYSTEMS plcInventors: RICHARD EDWARD SIMPSON, ARTHUR GEORGE RICHARDS
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Publication number: 20160161604Abstract: A radar apparatus (5) for detecting multipath signal propagation when determining an elevation angle of an object, comprising an antenna array with which the radar apparatus is arranged to form at least three separate antenna beams (11, 12, 13) comprising a first antenna beam (11) having an angle of elevation above horizontal, and a separate second antenna beam (12) having an angle of elevation at or above horizontal which is less than that of the first antenna beam, and a separate third antenna beam (13) having an angle of elevation below horizontal. The apparatus is arranged to transmit radio pulses from the antenna array; to receive return radio signals within the first, second and third antenna beams; to calculate a measure of the magnitude of a return radio signal received within the third antenna beam using all of said received radio signals collectively; and, to detect multipath signal propagation using said measure.Type: ApplicationFiled: July 2, 2014Publication date: June 9, 2016Applicant: BAE SYSTEMS plcInventor: MARCUS EDWARD CLARK
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Publication number: 20160161235Abstract: The invention relates to an igniter device for igniting energetic materials, more specifically to the area of the initiation of munitions, and methods of forming said ignition devices. There is provided an igniter device, for use in an explosive train, comprising a first synthetic polymer layer, a second synthetic polymer layer, wherein said first layer and second layer envelope a portion of an energetic material, wherein said synthetic polymer is capable of being sealed.Type: ApplicationFiled: July 14, 2014Publication date: June 9, 2016Applicant: BAE SYSTEMS plcInventor: ANNE MARIE WILTON
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Publication number: 20160161221Abstract: Apparatus and method are disclosed for guiding a payload to a target location. The apparatus comprises a laser radiation source, a laser radiation reflecting arrangement for generating substantially spatially homogeneous reflected laser radiation, an activator for activating the radiation source to generate laser radiation and an electrical power source for powering the apparatus.Type: ApplicationFiled: July 14, 2014Publication date: June 9, 2016Applicant: BAE SYSTEMS plcInventor: RICHARD DESMOND JOSEPH AXFORD
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Publication number: 20160161262Abstract: A method and apparatus for determining a route for a vehicle (6), the method comprising: measuring a position of the vehicle (6); providing a specification of a region (12) into which the vehicle (6) is to be moved; and, using the measurements and specification, determining the vehicle route. The route determination process comprises constructing a graph (34) within a state space (X) of the vehicle (6), identifying, within the graph (34), a path for the vehicle (6), performing a path shortening algorithm on the identified path, and, using the shortened path, determining the vehicle route. The path shortening algorithm comprises: selecting two vertices along the path that are separated by at least two edges; connecting the two selected vertices with an additional edge; and, depending on certain cost values, removing the edges and vertices by which the selected vertices are connected, and including, in the path, the additional edge.Type: ApplicationFiled: July 7, 2014Publication date: June 9, 2016Applicant: BAE SYSTEMS plcInventor: RICHARD EDWARD SIMPSON
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Patent number: 9360625Abstract: Techniques are disclosed for improving pump absorption and efficiency for fiber lasers and amplifiers, for instance. In some embodiments, the techniques are implemented by applying a partially reflective coating on a fiber end-face to double-pass any unabsorbed or otherwise excess pump light in the cladding of a fiber. While being reflective to pump wavelengths, the coating can be non-reflective at the lasing wavelength, so as to avoid unwanted feedback into the system. The benefits of this approach include that excess pump power can be effectively utilized to add more power to the laser output. In addition, the double-pass technique allows for the use of a shorter fiber length, which in turn allows for more compact system designs, saves on material costs, and facilitates manufacturability.Type: GrantFiled: November 6, 2014Date of Patent: June 7, 2016Assignee: BAE Systems Information and Electronic Systems Integration Inc.Inventor: Daniel J. Creeden
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Patent number: 9360286Abstract: The invention relates to a rotationally stabilized projectile (1) for launching from a barrel, which projectile (1) comprises a front projectile part (22), a rear projectile part (20) comprising a rotating band (4), and an intermediate projectile part (21) comprising a freely rotatable middle section (2) arranged with guide wings (3) for improving the gliding capability and guidance capability during the gliding phase and end phase of the projectile. The guide wings (3) are arranged extensibly on the freely rotatable middle section (2), and the intermediate projectile part (21) also comprises a regulator device (14) for regulating the rotation of the middle section (2). The invention also relates to a method for guiding a rotationally stabilized projectile.Type: GrantFiled: June 26, 2012Date of Patent: June 7, 2016Assignee: BAE Systems Bofors ABInventors: Thomas Pettersson, Daniel Brohede
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Patent number: 9360279Abstract: The invention pertains to a device for signature adaptation, comprising at least one surface element (100; 300; 500) arranged to assume a determined thermal distribution, wherein said surface element comprises at least one temperature generating element (150; 450a, 450b, 450c) arranged to generate at least one predetermined temperature gradient to a portion of said at least one surface element. Said at least one surface element (100; 300; 500) comprises at least one radar suppressing element (190), wherein said at least one radar suppressing element (190) is arranged to suppress reflections of incident radio waves. The invention also concerns an object provided with a device for signature adaptation.Type: GrantFiled: June 5, 2012Date of Patent: June 7, 2016Assignee: BAE SYSTEMS HÄGGLUNDS AKTIEBOLAGInventor: Peder Sjölund
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Patent number: 9360372Abstract: Disclosed is a system and method for using a portable near (infrared light emitting diode) IR LED light source and photogrammetry for boresight harmonization of aircraft and ground vehicle components. In one embodiment, orientation and positional parameters of two or more fixed points and distances between the two or more fixed points are measured using the portable near IR LED light source with a photogrammetric system. The two or more fixed points are reference points within the aircraft or the land vehicle. Further, the measured orientation and positional parameters of the two or more fixed points and the distances between the two or more fixed points on the aircraft or the land vehicle are compared with specified design parameters of the component in the aircraft or the land vehicle. Furthermore, the component in the aircraft or the land vehicle is harmonized based on an outcome of the comparison.Type: GrantFiled: June 13, 2012Date of Patent: June 7, 2016Assignee: BAE Systems Information and Electronic Systems Integration Inc.Inventor: Michael W. Hale
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Patent number: 9363915Abstract: A system and method for building an electronic system with line-replaceable units (LRUs) is presented. The system includes a first LRU electronic module with a first connector on a side of the first LRU electronic module and a second LRU electronic module with a second connector on a side of the second LRU electronic module. To build the electronic system, the first connector on the first LRU electronic module is connected to the connector on the second LRU electronic module to form a first LRU electronic module and a second LRU electronic module combination with the first connector and the second connector interior to the module combination formed by the first LRU electronic module and the second LRU electronic module. The first connector and the second connector cannot be seen from outside the module combination formed by the first LRU electronic module and the second LRU electronic module.Type: GrantFiled: December 12, 2012Date of Patent: June 7, 2016Assignee: BAE Systems Information and Electronic Systems Integration Inc.Inventors: Richard E. Berkenbush, Edward D. O'Neill, Christopher Errick
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Publication number: 20160153791Abstract: Disclosed are methods and apparatus for determining a path (4) for a vehicle (2). The method comprises providing starting and final positions for the vehicle (2), and using the provided positions, determining an ordered sequence of points, thereby providing the path (4) for the vehicle (2). Performing the optimisation process comprises: minimising a distance between the final position and a last point in the sequence; for each point other than a last point in the sequence, constraining a distance between that point and the next point to be equal to a predefined distance; and, for each path point other than the first and last points, constraining an angle between a line that connects that point to the point that precedes it and a line that connects that point to the next point to be greater than or equal to a predefined angle.Type: ApplicationFiled: July 4, 2014Publication date: June 2, 2016Applicant: BAE SYSTEMS plcInventor: MARKUS DEITTERT
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Publication number: 20160154150Abstract: An apparatus is disclosed for producing an optical display comprising an optical waveguide (1) and a pair (10, 16) of switchable diffraction gratings that are switchable between a diffractive state and a non-diffractive state. A pair of non-switchable diffraction gratings (2, 14) is arranged to receive diffract light from one switchable grating for guided propagation along the optical waveguide and out to the other switchable grating for viewing. The pair of non-switchable gratings are tuned to a first operating wavelength of light, while the pair of switchable gratings are tuned to a different operating wavelength of light to diffract that light into/from a field of view in common with that of the non-switchable gratings such that light of two wavelengths occupies the same field of view.Type: ApplicationFiled: December 2, 2013Publication date: June 2, 2016Applicant: BAE SYSTEMS plcInventors: MICHAEL DAVID SIMMONDS, MOHMED SALIM VALERA
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Patent number: 9354028Abstract: The invention relates to a method for determining the roll angle of a guidable and substantially or partially roll-stable projectile comprising control system, radio-based positioning receiver and sensor for measuring roll angular velocity, in which the following steps are included: actuation of the actuators of the projectile by the control system, included in the projectile, for maneuvering of the projectile; estimation of a first signal, the projectile control force, on the basis of the control system included in the projectile; measurement of a second signal, the velocity of the projectile relative to the ground-fixed coordinate system, with the radio-based positioning receiver mounted in the projectile; measurement of a third signal, the rotational velocity, with the sensor for roll angular velocity mounted in the projectile; calculation of a roll angle on the basis of the first, second and third signals, estimated projectile control force, measured projectile velocity, and measured rotational velocity,Type: GrantFiled: September 13, 2012Date of Patent: May 31, 2016Assignee: BAE Systems Bofors ABInventor: Daniel Brohede
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Patent number: 9354393Abstract: A method for polishing photonic chips is described. A gauge is placed in a photonic chip adjacent to an edge to be polished. The gauge includes a set of bars of various lengths. The bar lengths can be progressively ordered from shortest to longest or vice versa. The photonic chip is then secured in a chip polishing jig to get ready for polishing. When the photonic chip is being polished, an operator can visually inspect the gauge by looking at the polishing edge to estimate a polishing depth in order to determine a stopping point for polishing. Once the stopping point has been reached, the polishing of the photonic chip can be stopped.Type: GrantFiled: July 2, 2015Date of Patent: May 31, 2016Assignee: BAE Systems Information and Electronic Systems Integration Inc.Inventors: Andrew T S Pomerene, Matthew A. Gregory
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Patent number: 9347750Abstract: The invention relates to a method for determining angle of incidence for a projectile in the path of the projectile from launcher to target, which projectile is guidable and substantially or partially roll-stable and comprises a control system and at least two actuators with associated control members, in which the following steps are included: determination of applied force for pitch control by evaluation of the moment upon the actuators of the projectile, determination of applied force for yaw control by evaluation of the moment upon the actuators of the projectile, calculation of the pitch component a of the angle of incidence and of the yaw component ? of the angle of incidence, based on comparison between the evaluated moments and reference data for moments. The invention also relates to a GNC system.Type: GrantFiled: September 13, 2012Date of Patent: May 24, 2016Assignee: BAE Systems Bofors ABInventor: Mats Larsson
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Patent number: 9350106Abstract: An electrical connector assembly adapted for military use comprising a high density maintenance connector which supports high bandwidth video export and low level maintenance functions, a lower density I/O connector, the stacking feature allows multiple branches in distribution center, custom to each user, and the programmability allows for identical cables/stacking connectors to be used in different configurations.Type: GrantFiled: October 3, 2013Date of Patent: May 24, 2016Assignee: BAE Systems Information and Electronic Systems Integration Inc.Inventors: Michael J. Choiniere, Mark P. Devins, David A. Richards, Kevin D. Galli
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Publication number: 20160137044Abstract: The present invention relates to an electrical drive arrangement for driving a motor vehicle comprising an electric motor, a drive shaft driven by means of the electric motor, a housing in which the electric motor is accommodated, which housing has an envelope surface and a substantially annular cross section wherein the horizontal direction of the envelope surface of said housing and hereby said drive shaft are arranged to run substantially transverse to the longitudinal direction of said vehicle, comprising a pendulum suspension for suspension of the electrical drive arrangement, where the pendulum suspension comprises a fastening configuration fixedly connected to the vehicle and at least one pendulum attachment fixedly connected to the envelope surface of the housing and pivotally journaled relative to said fastening configuration by means of a bearing configuration. The invention also relates to a motor vehicle.Type: ApplicationFiled: May 27, 2014Publication date: May 19, 2016Applicant: BAE Systems Hägglunds AktiebolagInventor: Daniel ENGBLOM