A long-range reconnaissance pod comprises a cylindrical body and a hollow enclosure forward to said body within which an optical sensor configured to image areas of interest during a long-range reconnaissance mission is housed, wherein a casing of said forward hollow enclosure comprises a target-facing section and a target-opposing section that both extend to a leading edge of said pod, and wherein an optical window adapted to protect said optical sensor from external flow is secured to said target-facing section, and both sections are configured with an external aerodynamic design that renders the optical window substantially optically distortion-free.
A receiver system has at least one antenna that receives a plurality of signals, including a desired signal, across a wide band of frequencies. At least one tunable filter is in signal communication with the at least one antenna, and filters the plurality of signals to produce a plurality of filtered signals. Gain control circuitry is in signal communication with the at least one tunable filter, and produces a gain adjusted version of the filtered signals. A processing unit processes received signals in a portion of the wide band to extract signal characteristics of at least one undesired signal in the portion of the wide band. The at least one tunable filter is tuned based at least in part on the signal characteristics of the at least one undesired signal to maintain the SNR of the desired signal above a threshold level at the output of the gain control circuitry.
A thermally-compensated optical system (30) has a thermally-responsive actuator assembly (38) between first and second optical components (32,34) arrayed along an optical axis. The actuator assembly has actuators (10) integrated into a collar encircling the optical axis. Each actuator has two interconnected beams (12a,12b) from a first 5 material and a rod (18) associated with the ends of both beams such that a distance between the ends is determined by a length of the rod. The rod is formed from a second material having a coefficient of thermal expansion different from that of the first material such that a variation in temperature causes deformation of the actuators, thereby varying a height of the actuators according to an effective coefficient of thermal expansion with 10 a magnitude greater than that of both materials. This adjusts a relative position of the first and second components along the optical axis.
A system for illuminating a target in the presence of atmospheric turbulence includes a coherent beam combining (CBC) subsystem, an atmospheric wave-front sensor (AWS) subsystem, a multi-channel photo-detector (MCPD) subsystem, an auxiliary light source, and a receiving optical aperture. The CBC subsystem forms a multiplicity of CBC sub-beams and an reference beam, all of which fall in a wavelength band that is different from that of the auxiliary light source. The auxiliary light source may be a laser or a portion of the solar spectrum of the Sun. An AWS controller provides closed-loop compensation of atmospheric turbulence for low power auxiliary reflection and reference beams. A MCPD controller provides closed-loop compensation of high-frequency laser noise and transfers the wavefront correction from the reference to the high power CBC laser. The frequency of the MCPD controller is at least an order of magnitude greater than the bandwidth of the AWS controller.
A multi-communication (MC) system supporting mitigation plan for interfering spurious products, comprising: a) at last one first client that is configured to perform wireless communication; b) at least one second client that is capable of generating spurious product that potentially interferes with said first client communication; c) a Clock-Frequency-Base Band Management Unit (CFBBMU) module configured to repeatedly: i. generates a spurious map based on data collected from one or more of said clients; and ii. utilizes said generated spurious map to mitigate clients' interference.
A secure video conferencing system designed to operate within isolated network environments, ensuring secure and efficient communication without direct network connectivity between segregated systems. The system includes a workstation configured to initiate video conferencing sessions, a client computer associated with an organization's main or isolated network, and security isolators that mediate unidirectional data flow between these components. The security isolators prevent unauthorized bidirectional data exchange, ensuring strict cybersecurity protocols are maintained.
Disclosed is an opening system for a container that is closed with a lid, which is located under pressure. The system includes a) an arrangement suitable to allow the opening of said lid of said container; b) a flexible element suitable to be connected to said container, and suitable to be inflated; and c) a pressure-regulating subsystem suitable to produce an increase of pressure inside said container up to a value that causes the inflation of said flexible element and its tearing.
B65D 51/22 - Caps, lids, or covers co-operating with an inner closure arranged to be opened by piercing, cutting, or tearing having means for piercing, cutting, or tearing the inner closure
B65D 81/20 - Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents providing specific environment for contents, e.g. temperature above or below ambient under vacuum or superatmospheric pressure, or in a special atmosphere, e.g. of inert gas
F16K 17/14 - Safety valvesEqualising valves opening on surplus pressure on one sideSafety valvesEqualising valves closing on insufficient pressure on one side with fracturing member
8.
RESOURCE MANAGEMENT AND ROUTING IN MOBILE AD-HOC NETWORKS THAT EMPLOY MULTI-CHANNEL RECEPTION AND COOPERATIVE RELAYING
MANET nodes have a transceiver, operative in a first plurality of frequencies, having a transmitter that selects at least one frequency for transmission and a receiver that simultaneously receives signals in a second plurality of frequencies selected from the first plurality of frequencies. A resource allocation table is generated and has time-slots and frequencies to be allocated amongst the nodes. Data is maintained in the resource allocation table that is representative of session plans, where each session plan corresponds to a message to be propagated through the MANET from a source node to a destination node. Each session plan includes time-slot and frequency allocations associated with the source node. At each time-slot, each node of one or more nodes decides which one or more messages to broadcast during the time-slot on one or more frequencies selected from the first plurality of frequencies.
A system (10) for testing a laser proximity fuse (PF) (12) by simulating a closing velocity to a target along a line of sight (14) includes a static spiral surface (16) and a support arrangement (18) for supporting the proximity fuse (12) with the line of sight (14) directed towards an inside of static spiral surface (16). A folding mirror (20) is driven by a drive motor (22) so as to deflect the line of sight (14) towards progressively closer regions of static spiral surface, thereby simulating a closing velocity. The system can be miniaturized by employing converging optics (24). An alternative embodiment employs a shaped rotor (32) to achieve a similar effect.
A multispectral image capture device includes an imaging platform having arranged thereon an image sensor comprising a photosensitive surface and an optical unit, a gimbals system for controlling a line of sight of the image sensor, a filter wheel comprising a series of n spectral filters arranged between the image sensor and an imaging target; and a drive system configured to rotate the filter wheel at a constant velocity so as to bring each of the spectral filters into a line of sight between the image sensor and the imaging target. A controller is adapted to synchronize movement of the imaging platform, control of line of sight of the image sensor with the gimbals, and constant rotation of the filter wheel, such that the image sensor captures a sequence of overlapping step-and-stare images through the series of rotating spectral filters without changing a speed of rotation of the filter wheel.
H04N 23/11 - Cameras or camera modules comprising electronic image sensorsControl thereof for generating image signals from different wavelengths for generating image signals from visible and infrared light wavelengths
H04N 23/12 - Cameras or camera modules comprising electronic image sensorsControl thereof for generating image signals from different wavelengths with one sensor only
H04N 23/55 - Optical parts specially adapted for electronic image sensorsMounting thereof
H04N 23/695 - Control of camera direction for changing a field of view, e.g. pan, tilt or based on tracking of objects
Flown munition that is rocket-propelled for hitting a target behind a barrier, and which comprises a rocket motor; and a successive payload that is mounted behind the rocket motor in a tandem configuration and is towed by it; and wherein the rocket motor is used for accelerating the munition towards the barrier and also serves as a sort of kinetic penetrator to clear a passage through the barrier for the successive pay load, which is connected to it and towed by it, and the successive payload (e.g.—a high-explosive charge) is adapted for delayed detonation following and just after said rocket motor hits the barrier.
F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
12.
FREQUENCY SYNCHRONIZATION IN DECENTRALIZED COMMUNICATION NETWORKS
Frequency synchronization methods provide synchronization among nodes of a decentralized communication network. At each of one or more nodes of a plurality of nodes that form a decentralized communication network, information is acquired that is indicative of a frequency associated with at least one other node of the plurality of nodes. For each of the one or more nodes, a frequency offset between a frequency of the node and a frequency of the at least one other node is determined, based in part on the acquired information.
Methods, systems, and computer program products simulate image-capture of a scene at having least one object of interest (OOI) by a camera. A plurality of rendered images is obtained and includes: i) a first image, at a first resolution, that is an image of the scene and excludes the OOI, ii) a second image, at a second resolution higher than the first resolution, that is an image of the OOI, iii) a third image, at the second resolution, that is an image of a region that bounds the OOI, wherein the OOI at least partially affects one or more other objects in the region, and iv) a fourth image, at the second resolution, wherein for each pixel of the fourth image, a pixel value of the pixel indicates a contribution of the OOI in the pixel. The images are processed to produce a high-resolution image of the OOI.
A method of assessing safety of a trajectory of units under test over a flight range includes: setting a mission trajectory of a unit under test, wherein nominal and dispersion trajectories of the unit under test are within a delineated area; extracting from the mission trajectory a plurality of initial conditions of the unit under test; for each extracted initial condition, simulating a malfunction, and calculating an orientation of the unit under test following each simulated malfunction using an orientation transfer function of the unit under test to simulate a malfunction maneuver. The method further includes, on the basis of this calculated orientation for each simulated malfunction, determining an impact point of the unit under test with a particular plane.
A CBC system includes an array of beam sources generating coherent beams directed towards a target. The beam sources have associated adjustable phase modulators and beam steering arrangements. For each of the beams in a subset of the beams, the corresponding beam steering arrangement is actuated to steer the beam, and the corresponding phase modulator is actuated to modulate a current phase of the beam between at least three phase states. A detector monitors an intensity parameter that varies as a function of an intensity of radiation impinging on the target. A controller calculates, for each of the beams in the subset, a current value that is representative of a relative intensity of the beam based at least in part on the monitored intensity parameter at each of the at least three phase states. The calculated value is indicative of a current position of the beam relative to the target.
A receiver system has at least one antenna that receives a plurality of signals, including a desired signal, across a wide band of frequencies. At least one tunable filter is in signal communication with the at least one antenna, and filters the plurality of signals to produce a plurality of filtered signals. Gain control circuitry is in signal communication with the at least one tunable filter, and produces a gain adjusted version of the filtered signals. A processing unit processes received signals in a portion of the wide band to extract signal characteristics of at least one undesired signal in the portion of the wide band. The at least one tunable filter is tuned based at least in part on the signal characteristics of the at least one undesired signal to maintain the SNR of the desired signal above a threshold level at the output of the gain control circuitry.
A system for multi-agent mission planning comprises a) a mission generator (MG) configured to compute a set of Mission Agent Language (MAL) missions; b) a group of agents (TGPs), each capable of performing at least one MAL mission; and c) at least one Multi-Agent Planner (MAP) adapted to receive said set of MAL missions from said MG to build an allocation vector between said MAL missions and said agents in said group;
wherein each agent (TGP) is further capable of performing its assigned MAL mission per said allocation vector, while considering all other agents in its corresponding tactical group.
A method for creating a dedicated optimal local grid around a place of interest comprises: a) iteratively updating the local grid size such as to satisfy statistical constraints; and b) discontinuing the iterative process of step (a) when a predefined threshold of said statistical constraint is reached.
A mechanism for orienting a payload support includes first and second transversely deployed drive assemblies, each having a motor that drives a drive arm. The payload support is directly pivotally mounted to a first drive arm. Connection between the second drive arm and the payload support is via a coupling linked to the second drive arm via a coupling rotary joint, and to the payload support via a support rotary joint. Both the first drive arm and the second drive arm are supported relative to the frame by sets of two bearing assemblies located on opposite sides of the center of rotation. Each of the bearing assemblies is preferably implemented as a loaded duplex bearing assembly, and most preferably with a back-to-back loaded duplex bearing assembly on each axis.
F16M 11/14 - Means for attachment of apparatusMeans allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction with ball-joint
F16C 19/18 - Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load with two or more rows of balls
F16M 11/18 - Heads with mechanism for moving the apparatus relatively to the stand
G02B 27/64 - Imaging systems using optical elements for stabilisation of the lateral and angular position of the image
A temperature compensated spacer includes first and second anchoring configurations for anchoring the spacer relative to first and second elements, and a frame providing a mechanical connection between the anchoring configurations. The frame has a polygonal opening with a first diagonal extending across the width of a gap between the elements and a second diagonal extending transversely to the first diagonal. A crossbar is associated with the polygonal opening so as to span the second diagonal. The frame and the crossbar are formed from materials having differing coefficients of thermal expansion. The crossbar is deployed so as to determine a length of the second diagonal such that variation in temperature causes deformation of the frame, thereby varying a length of the first diagonal.
G02B 7/18 - Mountings, adjusting means, or light-tight connections, for optical elements for prismsMountings, adjusting means, or light-tight connections, for optical elements for mirrors
21.
Coherent beam combination (CBC) systems and methods
c) allow adjustment of relative phase offsets of the beams. A detector (16) monitors an intensity of the radiation impinging on an area of the target (T). A controller (18) receives the intensity parameter and controls a phase adjustment of the beams according to a deterministic (i.e., quantitative) measurement of a phase offset of each beam relative to a representative phase of the sum of all the other beams. This is achieved by using interferometric techniques, referred to herein as Target In-the-Loop Interferometry (TILI).
H01S 3/10 - Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating
H01S 3/23 - Arrangement of two or more lasers not provided for in groups , e.g. tandem arrangement of separate active media
G01S 7/481 - Constructional features, e.g. arrangements of optical elements
H01S 5/40 - Arrangement of two or more semiconductor lasers, not provided for in groups
22.
DEVICES HAVING A PHASED-ARRAY ANTENNA AND CALIBRATION METHOD THEREFOR
Methods and devices provide a test signal to each of a plurality of antenna channels via a test signal line. Each antenna channel includes an amplitude adjustor and a phase adjustor associated with at least one antenna element. For each antenna channel, the test signal provided to the antenna channels is modulated to produce a modulated test signal. The modulated test signal is produced by: i) controlling the amplitude adjustor of the antenna channel to vary a current amplitude of the test signal between a plurality of amplitude states, and ii) controlling the phase adjustor of the antenna channel to vary a current phase of the test signal between a plurality of phase states. A received test signal received from the antenna channels is processed to determine amplitude and phase errors associated with the modulated test signals associated with the antenna channels.
H01Q 3/26 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture
H04B 17/12 - MonitoringTesting of transmitters for calibration of transmit antennas, e.g. of amplitude or phase
H04B 17/21 - MonitoringTesting of receivers for calibrationMonitoringTesting of receivers for correcting measurements
A reactive armor for defeating threats comprises one or more fragile reactive plates consisting of reactive material sandwiched between two fragile layers, said fragile reactive plates being contained in a housing, the void space of said housing being filled with a polymeric foam.
A reactive armor for defeating threats comprises an outer shell having outer and inner surfaces, an inner reactive plate, and explosive material disposed between said inner surface and said reactive plate, wherein said reactive plate is configured to be displaced away from said inner surface upon activation of said explosive material.
A coherence reconstruction apparatus generates measurements of atmospheric turbulence from light reflected by a target. The apparatus is in communication with a coherent beam combining (CBC) system which illuminates a target with one or more partially coherent beams from a seed laser. The apparatus includes a variable delay module and a phase shift interferometer (PSI). The delay module uses a measurement of target time-of-flight to form a coherent delayed reference signal from the CBC seed reference laser. The delay module may incorporate an electromagnetically induced transparency medium and/or an electro-optical modulator. The PSI combines the delayed reference optical signal with a target-reflected optical signal to form an interference pattern and to determine one or more turbulence phase correction measurements. The apparatus may include a controller for generating feedback and dynamic tuning signals.
A targeting receiver operates with beam emitters. Each emitter generates coherent beams directed towards a target as a composite beam having an associated signature. For each composite beam, the target reflects a proportion of radiation intensity as a reflected radiation component. A receiver telescope collects target-reflected radiation and directs the radiation to a spatial filter. The reflected radiation includes radiation components, at least some of which are combined as a combined radiation composed of the reflected radiation components. Intensity of the combined radiation indicates the intensity of the composite beams impinging on the target. The spatial filter filters the reflected radiation by selectively passing the combined radiation. Each component of the combined radiation is identifiable by the signature associated with the composite beam corresponding to the component of the combined radiation. In certain embodiments, a distinguishing module is associated with the receiver and distinguishes the components based on the signature.
G01S 17/86 - Combinations of lidar systems with systems other than lidar, radar or sonar, e.g. with direction finders
G02B 23/04 - Telescopes, e.g. binocularsPeriscopesInstruments for viewing the inside of hollow bodiesViewfindersOptical aiming or sighting devices involving prisms or mirrors for the purpose of beam splitting or combining, e.g. fitted with eyepieces for more than one observer
G02B 26/08 - Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
G02B 27/00 - Optical systems or apparatus not provided for by any of the groups ,
The invention relates to a thermal contact apparatus, comprising: a first plate, suitable to be connected to a heat source, absorb heat from said heat source, and transfer the heat to other components of the apparatus; a first set of fibers, suitable to absorb heat from said first plate and transfer the heat to other components of the apparatus, wherein said first set of fibers is connected to said first plate; a second set of fibers, suitable to absorb heat from said first set of fibers and thansfer the heat to other components of the apparatus, wherein said first and second sets of fibers are in contact; and a second plate, suitable to absorb heat from said second set of fibers and transfer the heat out of the apparatus, wherein said second set of fibers is connected to said second plate.
A range-finding apparatus and method for measuring the range of a target illuminated by a coherent beam combining (CBC) system having at least two partially coherent sub-beams. The apparatus includes a phase modulation controller and a signal processor. The controller provides one or more optical phase modulation signals to the CBC system. The signal processor receives an initial measurement of target range, provided by either the CBC system or an external range-finding device and having a relatively large uncertainty, and a time-varying received intensity signal provided by the CBC system. The signal processor calculates frequency components of the intensity signal, forms rotated frequency components corresponding to a time-of-flight correction, calculates an objective function depending upon the rotated frequency components, determines a global minimum of the objective function, and calculates a corrected measurement of target range having an uncertainty which is less than that of the initial measurement of target range.
A power amplifier with improved stability, gain, flatness and return loss and reduced the size, which comprises a two-stage power amplifier in balanced cascode topology that consists of a first common-source stage feeding into a first common-gate stage; a second common-source stage feeding into a second common-gate stage; an input matching network for matching the input impedance of the a two-stage power amplifier to a desired signal source impedance; an output matching network for matching the output impedance of the a two-stage power amplifier to a desired load; a first positive feedback path between the gate of the first common-source stage and the drain of the second common-gate (CG) stage and a second positive feedback path between the gate of the second common-source stage and the drain of the first common-gate (CG) stage; a first negative feedback path between the drain of the first common-gate (CG) stage and the gate of the first common-source stage and a second negative feedback path between the drain of the second common-gate (CG) stage and the gate of the second common-source stage; a first inter-stage matching network between the first common-source (CS) stage and the first common-gate (CG) stage; and a second inter-stage matching network between the second common-source (CS) stage and the second common-gate (CG) stage.
A mechanism for steering and maneuvering an airborne body comprised of at least one actuator comprising an electric motor having a first axis, and a gear transmission for transmitting power from the electric motor to an angular motion axis of a fin that has an angular motion around a second axis to steer the airborne body, and wherein the mechanism is characterized in that the gear transmission is a beveloid gear type of transmission, an airborne body that comprised the mechanism, and a method for achieving the desired flight path of an airborne body implementing the mechanism.
A first transceiver has a beam emitter that generates first coherent beams, and first optics that direct the first coherent beams towards a target and collect radiation reflected from the target. A second transceiver has a beam emitter that generates second coherent beams, a detector, and second optics having an aperture. The second optics directs the second coherent beams towards the target via the aperture, collects radiation reflected from the target via the aperture, and guides a first radiation component of the collected radiation, that corresponds to the first coherent beams, to the detector. The detector generates, from the first radiation component, a signal indicative of an intensity of radiation impinging on the target corresponding to the first coherent beams. A control subsystem is associated with the transceivers and modifies at least one parameter of the first transceiver based on the intensity signal.
G01S 17/86 - Combinations of lidar systems with systems other than lidar, radar or sonar, e.g. with direction finders
G02B 23/04 - Telescopes, e.g. binocularsPeriscopesInstruments for viewing the inside of hollow bodiesViewfindersOptical aiming or sighting devices involving prisms or mirrors for the purpose of beam splitting or combining, e.g. fitted with eyepieces for more than one observer
G02B 26/08 - Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
G02B 27/00 - Optical systems or apparatus not provided for by any of the groups ,
An armed aerial platform (100) includes a weapon for firing a projectile from a barrel (102) that defines a weapon axis (104). The weapon is supported by a single-axis gimbal mechanism (116) within a central vertical slot (112) in a rigid body (108) of a UAV (108) carried by a propulsion system (114) including at least four rotary propulsion units. The gimbal mechanism (116) provides an elevation adjustment of the weapon axis (104), while the azimuth adjustment is provided by motion of the UAV (108) itself.
B64U 10/14 - Flying platforms with four distinct rotor axes, e.g. quadcopters
B64D 7/06 - Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraftAdaptations of armament mountings for aircraft the armaments being firearms movably mounted
B64U 101/18 - UAVs specially adapted for particular uses or applications for conventional or electronic warfare for dropping bombsUAVs specially adapted for particular uses or applications for conventional or electronic warfare for firing ammunition
B64U 101/20 - UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high altitude platforms
B64U 101/30 - UAVs specially adapted for particular uses or applications for imaging, photography or videography
A process for determining frequency allocations for efficient spectrum management and reuse, in communication between multiple users of moving platforms and ground stations using directional antennas, comprises: (a) generating a preferential ranking list; and (b) repeatedly recalculating desirable frequency allocations for communication between platforms and stations according to said preferential ranking list and user-to-user interference data.
A canister for storing and launching a self-propelled projectile comprises: a) an inner layer comprising an aluminum foil; b) a top layer consisting of an injected thermoplastic polymer; and c) optionally, a primer and/or a topcoat.
B29C 45/00 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor
B29C 45/14 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
B29K 77/00 - Use of polyamides, e.g. polyesteramides, as moulding material
F15B 15/16 - Fluid-actuated devices for displacing a member from one position to anotherGearing associated therewith characterised by the construction of the motor unit of the straight-cylinder type of the telescopic type
F15B 21/00 - Common features of fluid actuator systemsFluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
36.
Ultra-wideband attenuator with low phase variation and improved stability with respect to temperature variations
3b by the second control input; controlling the first and the second control inputs to obtain a desired attenuation between the input and output of the attenuator.
A total inner reflection (TIR) prism comprises two essentially triangular prisms separated by an optical coating or by a thin layer of air, wherein one of said two triangular prisms is shaped as an isosceles triangle.
A dielectric high gradient insulator device comprises a stack of at least two dielectric layers which are in physical contact with each other and which have different dielectric constants. At least two dielectric layers are configured to form a shaped electric field, when the device is placed between electrodes having a voltage difference. The shaped electric field is in a region proximal to a surface of the at least two dielectric layers, and causes deflection of negatively charged particles away from the surface, thereby inhibiting voltage breakdown of the device. A method of manufacturing the device is also presented.
H01B 3/10 - Insulators or insulating bodies characterised by the insulating materialsSelection of materials for their insulating or dielectric properties mainly consisting of inorganic substances metallic oxides
H01B 3/00 - Insulators or insulating bodies characterised by the insulating materialsSelection of materials for their insulating or dielectric properties
H01B 3/12 - Insulators or insulating bodies characterised by the insulating materialsSelection of materials for their insulating or dielectric properties mainly consisting of inorganic substances ceramics
39.
Transformer-based matching network for enhanced IC design flexibility
An Integrated Circuit (IC) containing at least one printed transformer-based matching network, which comprises: a) at least one printed transformer-based matching network with reduced size, which comprises a printed transformer with multiple internal ports in the form of electromagnetic discontinuities, introduced along the transverse dimension of the printed transformer; reactive elements, added to of the internal ports to thereby increase the order of the transformer-based matching network, the one or more reactive elements are printed along the transverse dimension of the matching network; a printed component connected to the input port of the matching network; a printed component connected to the output port of the matching network.
H03H 1/00 - Constructional details of impedance networks whose electrical mode of operation is not specified or applicable to more than one type of network
40.
Coherent beam combination (CBC) systems and methods
c) allow adjustment of relative phase offsets of the beams. A detector (16) monitors an intensity of the radiation impinging on an area of the target (T). A controller (18) receives the intensity parameter and controls a phase adjustment of the beams according to a deterministic (i.e., quantitative) measurement of a phase offset of each beam relative to a representative phase of the sum of all the other beams. This is achieved by using interferometric techniques, referred to herein as Target In-the-Loop Interferometry (TILI).
H01S 3/10 - Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating
H01S 3/23 - Arrangement of two or more lasers not provided for in groups , e.g. tandem arrangement of separate active media
G01S 7/481 - Constructional features, e.g. arrangements of optical elements
H01S 5/40 - Arrangement of two or more semiconductor lasers, not provided for in groups
41.
Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight
Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight and a method to prevent the ignition of the armaments rocket even in the event of actuation of the armaments pyrotechnic assembly, which normally serves to eject the armament from the launcher and to ignite its rocket motor, wherein the armament comprises a gas dispersion assembly, which when the armament is not encased in the tubular launcher, prevents the ignition of the rocket motor even if the armaments pyrotechnic assembly is actuated; and a cutting and separation assembly that is actuated by the pressure of the rocket motor gases for mechanically cutting a structural connection between the rocket motor and the armaments effective payload and separate them during their flight.
F42B 39/20 - Packages or ammunition having valves for pressure-equalisingPackages or ammunition having plugs for pressure release, e.g. meltable
F42C 15/28 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
F42C 15/31 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids generated by the combustion of a pyrotechnic or explosive charge within the fuze
A coating applied to a surface to minimize or prevent the ability of drops of super-cooled water that impact on the surface from transforming into ice, comprises one or more layers collectively providing: a) thermal insulation between the surface to be protected and the drop; and b) a superhydrophobic surface on the top.
A heaterless hollow cathode provides electron emission current in an electric space propulsion system. A mechanical, thermal, and electromagnetic design of the cathode apparatus is presented, and a method of operation for rapid ignition and stabilization of the cathode is provided. The keeper of the cathode apparatus has a thickness change which reduces the flow of heat away from the cathode's emitter assembly. The method for heating the emitter assembly includes controlling applied voltages so that the current flowing from the emitter assembly to the keeper is maintained at a predetermined fixed value. By this method, damage to the electron emitting surfaces of the emitter assembly by electric arcing and/or by depletion of dopant materials is avoided.
System for balancing series of cells, including circuits each having three or four cells, including: one or two central cells and additional neighboring cells in each circuit, each neighboring cell being adjacent to one central cells; a local capacitor for each neighboring cell, within a local section of each circuit; one global capacitor at a global section which is common to all the circuits; a plurality of controlled switches; a controller which periodically, repeatedly, and alternately opens and closes some switches to: within each circuit, connect each local capacitor in parallel to a respective neighboring cell; within each circuit, connect each local capacitor in parallel to the central cell if one central cell exists, or to another central cell if two central cells exist, respectively; within each circuit, connect said central cells of all circuits separately or simultaneously to said global capacitor.
A flexible protection element for reactive protection against shaped charge warheads and kinetic energy projectiles comprises a formable doughy mixture of a powder dispersed within a matrix of plastic explosive and a binder.
An explosive system and corresponding method employ a number of explosive portions, each of sub-critical dimensions so that initiation of the portion would result in incomplete detonation. A selectively-deployable spacer arrangement or deployment mechanism is deployed between a storage state in which gaps or misalignments are maintained between the explosive portions so that the explosive system remains undetonatable, and a detonable state in which the portions are brought together sufficiently to function as a combined explosive charge having effective dimensions larger than critical dimensions, rendering the explosive system detonatable.
F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
47.
System and method for detecting a cyber-attack at SCADA/ICS managed plants
System for detecting a cyber-attack of a SCADA system managed plant. Each industrial computerized device of the system comprises a processor configured with a data validation module to determine whether data flow outputted from a SCADA-connected controller is authentic, and with an alert issuing mechanism activated following detection that the outputted data flow is indicative of a cyber-attack. The at least one dedicated industrial computerized device is operable to passively monitor in parallel data communicated between each of the controllers and the SCADA system including the outputted data at the nearest points of each of the controllers; seek mismatches between the plant state and the physical operation model; if a mismatch is detected, determine whether the mismatch is indicative of a cyber-attack perpetrated with respect to one of the controllers or an operational malfunction; and upon detecting a cyber-attack, activate the alert issuing mechanism to issue a security alert.
G06F 21/55 - Detecting local intrusion or implementing counter-measures
H04L 29/06 - Communication control; Communication processing characterised by a protocol
H04L 12/12 - Arrangements for remote connection or disconnection of substations or of equipment thereof
G06F 21/85 - Protecting input, output or interconnection devices interconnection devices, e.g. bus-connected or in-line devices
G06F 21/57 - Certifying or maintaining trusted computer platforms, e.g. secure boots or power-downs, version controls, system software checks, secure updates or assessing vulnerabilities
H04L 29/08 - Transmission control procedure, e.g. data link level control procedure
G05B 19/042 - Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
G05B 19/418 - Total factory control, i.e. centrally controlling a plurality of machines, e.g. direct or distributed numerical control [DNC], flexible manufacturing systems [FMS], integrated manufacturing systems [IMS] or computer integrated manufacturing [CIM]
48.
Warhead for generating a blast on an extended region of a target surface
The present invention relates to warheads with blast wave conditioners and in particular to devices for quickly removing a door to permit entry through the doorway. It discloses a device and method of shaping the pressure wave pattern by the use of inert material. The inert material of the present invention is used to reduce localized directional effects occurring at the point of impact, instead generating a more diffuse pressure-wave pattern across the target surface.
F42B 10/00 - Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missilesArrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
F42B 12/00 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
F42B 30/00 - Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
A directed energy weapon includes a number of laser units, each including a fiber laser generating an output beam with a power of at least 1 kW from a fiber, an objective lens arrangement for focusing the output beam into a focused beam directed towards a target, and a fine adjustment mechanism for adjusting a direction of the focused beam. A beam deflector arrangement is deployed to deflect a portion of the focused beam from each laser unit as a deflected beam in a direction in predefined relation to a direction of the focused beam. An angle sensing unit generates an output indicative of a current direction of said deflected beam for each of said laser units. A controller actuates the fine adjustment mechanisms based on the output from the angle sensing unit to maintain a desired relative alignment between directions of the focused beams.
The invention relates to an interceptor type system for neutralizing a shaped charge threat, which comprises: (a) a detection system for detecting an approach of a shaped charge projectile, for calculating upon such detection its course of approach, and for activating an interceptor to create a flux of intercepting fragments within a destruction corridor; and (b) one or more of said interceptors, each comprising one or more magazines of fragments, each magazine comprises said fragments and an explosive layer which in turn explodes thereby to create said flux of intercepting fragments within said destruction corridor.
The present invention relates to electro-optic guided missile systems and, in particular, it concerns systems and methods providing enhanced navigation capabilities based on ego-motion processing of seeker images. The missile system comprising: a missile; a seeker located at a nose portion of said missile, said seeker comprising an electro-optic imaging sensor; and a control arrangement for steering the missile along a flight path to a target, characterized in that the missile system further comprises: a navigation subsystem receiving images from said imaging sensor, said navigation subsystem being configured to: co-process a plurality of said images from said imaging sensor to derive ego-motion of said missile relative to a region viewed by said imaging sensor; derive from said ego-motion a calculated target direction from said missile to a target.
G05D 1/10 - Simultaneous control of position or course in three dimensions
F42B 15/01 - Arrangements thereon for guidance or control
F41G 7/20 - Direction control systems for self-propelled missiles based on continuous observation of target position
F41G 7/34 - Direction control systems for self-propelled missiles based on predetermined target position data
G01C 21/12 - NavigationNavigational instruments not provided for in groups by using measurement of speed or acceleration executed aboard the object being navigatedDead reckoning
G01S 5/16 - Position-fixing by co-ordinating two or more direction or position-line determinationsPosition-fixing by co-ordinating two or more distance determinations using electromagnetic waves other than radio waves
F41G 7/00 - Direction control systems for self-propelled missiles
A shutter mechanism for covering a wing's spreading opening formed in an airborne body and a method for covering such opening while implementing the shutter mechanism, wherein the shutter comprises at least one flap assembly, and wherein from the instant that a deployed wing of the airborne body passed and moved over it, it is biased by traction of at least one springy element to an angular motion around an axis, unto a condition where the flap component of the assembly is positioned so that it is substantially conformal to the outline of the outer surface of the fuselage of the airborne body and while it covers the opening through which the wing passed in its motion; and from an instant that the wing returned and connected to the flap component of the assembly, the flap is biased to an angular motion counter the spring, to the state that the wing returns and is relocated on its top surface.
RCWS (Remote Controlled Weapon System or Station) of the deck-penetrator type and a method for protected reloading of a weapon system that is fed by belt of rounds from an ammunition container that is positioned in the RCWS, wherein the RWCS includes a system for protected reloading of the weapons system, that comprises—a bracket, that on it the ammunition container is mounted, and the bracket is amenable to be propelled via an opening in the deck of the vehicle upon which the RCWS is positioned, unto an inner space of the carrier vehicle and back from this space to the RCWS; and means for movably positioning the bracket, in at least two states—a first state wherein the bracket is positioned inside the inner space of the carrier vehicle and for reloading anew the weapons system; and a second state wherein the bracket is a least substantially embedded in the RCWS for feeding the weapons system by a belt of rounds from inside of the ammunition container that is positioned on the bracket.
The invention is a method and apparatus for creating mode division multiplexed channels capable of integration into photonic integrated circuits with direct spatial separation at the receiver end, thus removing the need for a DMUX module or at least significantly simplifying it. This is achieved by using a set of actuators that induce controllable mode mixing in a multi-mode fiber (MMF) at the transmitter in such a way that spatially separated channels are achieved at the receiver. As a result, no DMUX is required and failure of a single channel does not cause total communication link failure as occurs in links implemented with MUX/DMUX.
H04B 10/00 - Transmission systems employing electromagnetic waves other than radio-waves, e.g. infrared, visible or ultraviolet light, or employing corpuscular radiation, e.g. quantum communication
Wing deployment mechanism for deploying a pair of wings from an airborne body, wherein their deployment in motion, each one around an axis, defines the wings' deployment plane relative to the airborne body, and wherein the mechanism is characterized by that it comprises a propelable assembly mounted in the airborne body and suited to a rotational motion around an axis that is substantially orthogonal in its direction to the wings' deployment plane, a pair of arms that are linked, each one, on its one side to the assembly and at distance from the assembly's rotation axis, and on its other side to an end of one of the wings and at a distance from the axis around which the rotational motion of the wing in the wings' deployment plane is enabled, and wherein the link of each one of the arms is performed in a manner that enables angular motion of each of the arms relative to the assembly and to the end of the wing unto which it is linked, and wherein propelling the assembly to rotational motion and actuating a momentum for turning the wing as a result by the arm that is connected to it bring about concurrent rotational motion of the pair of wings in opposing directions and to their deployment on the wings' deployment plane, a method for deploying a pair of wings from an airborne body that is implementable in such mechanism and an airborne body equipped with such mechanism.
Firing preventing and stoppage apparatus for remotely operated automatic weapon such as installable in RCWS (Remotely Controlled Weapon Station), that comprises a barrier component and an actuator connected to the barrier component, wherein the barrier component is suited to movement through a cartridges ejection port from an automatic weapon, to a movement path of the breech block of the weapon, for preventing in advance or stoppage of runaway firing from it, and outwards from it in a manner that enables firing, an RCWS equipped with such apparatus and a method for preventing and stopping runaway firing of automatic weapons that are mountable in an RCWS and comprises a breech block and a cartridges ejection port that is implemented in such apparatus.
F41A 17/58 - Sear safeties, i.e. means for rendering ineffective an intermediate lever transmitting trigger movement to firing pin, hammer, bolt or sear automatically operated, i.e. operated by breech opening or closing movement
F41A 17/06 - Electric or electromechanical safeties
F41A 17/42 - Safeties for locking the breech-block or bolt in a safety position
Spent cartridges router means in a configuration of a four bars or four bar linkage mechanism for routing spent cartridges ejected from a chain fed automatic weapon towards means for gathering cartridges that is installable as an ad-on and independent (stand alone) mechanism on a weapon station of the type that comprises a base assembly that is rotatable for traverse motion, a cradle assembly that is located on the base assembly and linked with it in axial (pivotally) manner and chain fed automatic weapon that is affixable on the cradle assembly in a manner that it will be rotatable for elevation and lowering around the cradle's axis.
The invention relates to an improved Inertial Navigation System (INS), which comprises: (a) an INS unit which comprises (a.1) an IMU which in turn comprises a set of at least three gyros and at least three accelerometers, all mounted on a rotatable stage; and (a.2) an INS algorithm for measuring the behavior of said gyros and said accelerometers during a mission, and calculating a navigation solution based on said measurements; and (b) a north finding determination unit, which comprises: (b.1) one or more from said IMU gyros and one or more from said IMU accelerometers; and (b.2) a north finding algorithm which utilizes measurements from said one or more north finding gyros and one or more north finding accelerometers during an initial conditions stationary state in which the stage is positioned in at least two separate stationary orientations, said north finding algorithm determines a north finding solution which is provided to the INS unit for initializing its said INS algorithm.
G01C 21/16 - NavigationNavigational instruments not provided for in groups by using measurement of speed or acceleration executed aboard the object being navigatedDead reckoning by integrating acceleration or speed, i.e. inertial navigation
G01C 19/38 - Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
59.
Belt/metallic link chain loaded ammunition feeder in a remote controlled weapon station
Belt/Metallic Link Chain Loaded Ammunition Feeder in a Remote Controlled Weapon Station (RCWS). The feeder includes a feeding mechanism for routing chained ammunition from ammunition reservoir means towards the weapon's bullets entrance opening. The feeding mechanism has a first chute assembly for routing chained ammunition from the ammunition reservoir means towards the region of the RCWS's elevating/lowering axis, and a second chute assembly for continuing routing the chained ammunition from the region of the elevating/lowering axis towards the entry opening of the bullets entrance of the weapon. The chained ammunition traverses over the elevating/lowering axis region by passing from the first chute assembly to the second chute assembly. The first chute assembly remains static and the second chute assembly is dynamic and propelled together with the mounting bracket assembly around the elevating/lowering axis.
The invention relates to adaptive optics techniques applied to alter the modal structure of light propagating in an optical fiber. In particular the invention relates to altering the modal structure in a multimode beam propagating in a multimode fiber by lowering the number of higher modes. The method comprises combining a wavefront sensor and/or a power sensor with a phase control actuator and actuator control algorithms, to alter the phase structure of the beam thereby to eliminate higher modes. The corrected beam can be then effectively coupled into a smaller diameter fiber with minimum loss of energy and concentrated to smaller spot sizes limited by diffraction.
G02F 1/035 - Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating or modulatingNon-linear optics for the control of the intensity, phase, polarisation or colour based on ceramics or electro-optical crystals, e.g. exhibiting Pockels or Kerr effect in an optical waveguide structure
G02F 1/01 - Devices or arrangements for the control of the intensity, colour, phase, polarisation or direction of light arriving from an independent light source, e.g. switching, gating or modulatingNon-linear optics for the control of the intensity, phase, polarisation or colour
A Remote Controlled Weapon Station is provided wherein it comprises a weapon mounting bracket that is remotely adjustable in elevating/lowering and a rotatable turret assembly adapted to be mounted on vehicles, remotely adjustable in rotation, and wherein the weapon mounting bracket is pivotally mounted on it, and the Remote Controlled Weapon Station is converted into a remote controlled Non Lethal weapon station by that at least one non lethal means is installed in it, chosen from a group consisting of—a multi barreled means for firing grenades; multi-barrels launcher means for pyrotechnically firing plurality of charges; acoustic means for producing tones; illuminating means; observation means and means for providing sniper firing capabilities of small caliber kinetic bullet.
F42B 5/145 - Cartridges, i.e. cases with propellant charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
F41H 13/00 - Means of attack or defence not otherwise provided for
A mobile communication system which consists of a plurality of MANETs and nodes, which comprises a transceiver at each node. Each transceiver is a combination of a hopping transmitter operating according to a predetermined hopping sequence and rate and a wideband reference receiver, that can simultaneously receive at once, the whole operating band assigned to the system. Each transceiver further includes a circuitry for reallocating simultaneously receiving channels, dynamically spread over a wideband frequency range and circuitry for determining transmission hopping patterns to use the least possible number of frequencies according to the active population status of nodes that belong to the plurality of MANETs. This circuitry is also used for adapting the transmission scheme of the alien transceivers by finding time slots, in which a counterpart receiver at each remaining active node is not transmitting and a frequency channel, in which no other active node, neighboring the counterpart receiver transmits, while determining proper transmission frequency for each transmitting node.
The invention is an energetic unit comprised of: a container comprised of a base, an upper part, and a cover; a substrate located in the base and comprised of a thin, ribbon-like strip of flexible material that provides electrical contact to external firing circuits; a semiconductor bridge (SCB) chip electrically and physically attached to the substrate; and one or more layers of energetic material which, are packed into the upper part of the container between the SCB chip and the cover.
A Safe-and-Arm system for the prevention of unintentional operation of an explosive device by interrupting a detonation train, the system employing an interruptive transfer assembly made of silicon and suitable for implementing in a MEMS device, the assembly including a silicon based transfer charge carrier on a porous explosive passageway made by etching, the passageway extending between at least two ports on the circumference of the transfer assembly, and a drive means that can mechanically bring about at least one armed state of a detonation train.
F42C 15/18 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved
F42C 15/184 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a slidable carrier
F42C 15/188 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a rotatable carrier
F42C 15/28 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
A system and method for sampling multi-spectral images of a dynamically changing scene facilitates independently dynamically adjusting the exposure of a photosensor based on a first group of sequences of images, while disregarding a second group of sequences of images, where each sequence of images is of a distinct color of light. In addition, the current description presents an innovative technique for constructing a multi-spectral image of a scene based on individually contrast-enhanced images of the scene. Applications include video photography and high quality true color stills camera with separate sensor arrays for each color channel. The control of the present embodiment can be used to produce photographs with truer color than conventional techniques.
A turret assembly without deck penetration for minimizing exposure of combatants to enemy forces when accessing above deck equipment comprises a base plate on top of which is mounted at least one finable and remotely operable combatant interfaceable implement, the base plate being rotatable about a substantially vertical axis and supported for rotation by bearing means mounted within a deck of a military facility; a hatch displaceably connected to the base plate, for normally covering a hatchway formed in said base plate and for exposing said hatchway when displaced; and a rotatable disc of a slip ring unit carried by the hatch, by which electricity for operating equipment mounted on top of the deck and for initiating control signals is transmitted to the equipment.
A method of operating a mobile device with a camera, a display and a position sensor to provide a display of supplementary information aligned with a view of a scene. One or more image obtained from the camera is uploaded to a remote server together with corresponding data from the position sensor. Image processing is then performed to track image motion between that image and subsequent images obtained from the camera, determining a mapping between the uploaded image and a current image. Data is then received via the network indicative of a pixel location for display of supplementary information within the reference image. The mapping is used to determine a corresponding pixel location for display of the supplementary information within the current image, and the supplementary information is displayed on the display correctly aligned with the view of the scene.
G09G 5/00 - Control arrangements or circuits for visual indicators common to cathode-ray tube indicators and other visual indicators
G06T 19/00 - Manipulating 3D models or images for computer graphics
G01S 5/16 - Position-fixing by co-ordinating two or more direction or position-line determinationsPosition-fixing by co-ordinating two or more distance determinations using electromagnetic waves other than radio waves
C06B 45/00 - Compositions or products which are defined by structure or arrangement of component or product
C06B 45/12 - Compositions or products which are defined by structure or arrangement of component or product having contiguous layers or zones
C06B 25/00 - Compositions containing a nitrated organic compound
C06B 25/34 - Compositions containing a nitrated organic compound the compound being a nitrated acyclic, alicyclic or heterocyclic amine
C06B 25/10 - Compositions containing a nitrated organic compound the compound being nitroglycerine
D03D 23/00 - General weaving methods not special to the production of any particular woven fabric or the use of any particular loomWeaves not provided for in any other single group
The invention relates to an airborne reconnaissance system which comprises: (a) optical unit for acquiring light rays from a terrain portion, said optical unit comprises a plurality of optical components that are positioned along an optical path and designed to maneuver said light rays to produce at a focal plane an acquired image of a terrain portion, said acquired image having an area S which is several times larger than the area A of a focal plane array which is positioned at same focal plane; (b) gimbals unit for performing a continuous back and forth across-track scanning movement of a respective line of sight formed between said optical unit and the terrain below the aircraft; (c) a first back-scanning mirror along said optical path, for compensating for said continuous across track movement of the line of sight, said compensation is performed during a respective integration period for a section of said acquired image of area S which falls during said period on said focal plane array; and (d) a second, along-track mirror also positioned along said optical path, which alternates between plurality of along track states, each state causes a different diversion of the light rays within said optical path thereby to impinge on said focal plane array another along-track section of said acquired image of area S; and (e) capturing means for recording in each state of said along-track mirror the corresponding section of the terrain image which is impinged during said state on the focal plane array.
G03B 15/00 - Special procedures for taking photographsApparatus therefor
G01C 11/02 - Picture-taking arrangements specially adapted for photogrammetry or photographic surveying, e.g. controlling overlapping of pictures
H04N 3/08 - Scanning details of television systemsCombination thereof with generation of supply voltages by optical-mechanical means only having a moving reflector
A combined fan-compressor impeller comprises a single hub and a plurality of spaced main blades extending outwardly from the hub such that an air passage channel is defined between two of the main blades. Each of the main blades is a mixed flow blade which continuously extends from a fan section at an inlet end of a channel to a compressor section at an outlet end of the channel without any axial clearance between the fan section and the compressor section, providing aerodynamic matching of pressurized air flowing through the channel from the fan section to the compressor section.
F02C 3/04 - Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
F02K 3/06 - Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type with front fan
F04D 17/02 - Radial-flow pumps specially adapted for elastic fluids, e.g. centrifugal pumpsHelico-centrifugal pumps specially adapted for elastic fluids having non-centrifugal stages, e.g. centripetal
F04D 29/28 - Rotors specially adapted for elastic fluids for centrifugal or helico-centrifugal pumps
F04D 29/32 - Rotors specially adapted for elastic fluids for axial-flow pumps
An attitude determination system provided with North-finding capability, comprises: a) a stage consisting of a rotating platform provided with a high precision positioning controller; b) an Inertial Navigation System (INS) comprising inertial sensors, wherein said inertial sensors comprise gyroscopes and accelerometers, and wherein at least one gyroscope is of a precision suitable to find the direction of true North; and, c) a control unit for controlling input signals and output signals of the stage and the INS and combining the signals in order to provide attitude data of the system.
G01C 21/10 - NavigationNavigational instruments not provided for in groups by using measurement of speed or acceleration
G01C 19/36 - Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by magnetic means, e.g. gyromagnetic compasses
G01C 19/38 - Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
G01C 19/42 - Rotary gyroscopes for indicating rate of turnRotary gyroscopes for integrating rate of turn
72.
Method and system of generating a three-dimensional view of a real scene for military planning and operations
Generation of views of a real scene is based on selection of view criteria and the content of multiple types of source data. The viewpoint and at least one other criterion area used to determine which texture to sue for each surface, or portion of a surface, of a three-dimensional model. Regions of the images of the scene are associated with at least one portion of at least one surface of the three-dimensional model of the scene, wherein at least one of the portions is associated with the regions of at least two of the images. View selection criteria includes a criterion other than viewpoint. Based on the view selection criteria, selecting at least one of the regions for at least one of the portions and rendering a multi-view using the selected regions in combination with the three-dimensional model of the scene.
A system and method for providing information for performing a registration correction for artillery employs two spaced apart optical imaging systems associated with a processing system. Outputs from the two imaging systems are monitored to detect potential shell trajectory events and then correlated to eliminate potential shell trajectory events not viewed by both optical imaging systems. Locations are determined for potential shell trajectory events viewed by both optical imaging systems. Shell firing data relating to firing of at least one shell is provided to determine at least one predicted trajectory time point for the shell, and this is used to identify a corresponding detected shell trajectory event. The time and location of the detected shell trajectory event can then be used in determining a registration correction for the artillery
An apparatus for facilitating sequential viewing of streams of images of a common scene. The images are captured by an image sensor system having different viewing configurations generating visually dissimilar views. The electronic circuitry is configured, on transition between a first and a second viewing configurations, to input images captured using the first or second viewing configurations, and to generate a signal, derived from the input images. The signal corresponds to a gradual graphic transition between images captured using the first and the second viewing configurations, thus simulating a continuous viewing of the common scene. The gradual graphic transition includes transition due to a change of viewing direction, a change of aspect ratio, a change of sensor technology, a change of spectral sensitivity, a change of sensor sensitivity, a change of spatial resolution a change of sensor location, a change of binning level a change of displayed region of interest.
A micro-opto-electromechanical rotation rate sensor (MOERRS) device, in which a rotation rate sensor is associated with peripheral circuitry. The magnitude of the output signal of the MOERRS is adaptable to correspond to a range of mechanical stimuli to which the sensor is sensitive, in order to accommodate the signal magnitude to the dynamic range available in the MOERRS device. The signal emanating from the rotation rate sensor is facilitated to exploit the dynamic range of said MOERRS device, by modifying some properties of one or more items on the MOERRS.
A missile nose fairing system includes sections attached at an aft end thereof to a missile body, a restraint for normally preventing aftward displacement of the plurality of sections, and a drive unit for releasing the restraint in response to a received signal. Each of the sections has an outer surface that converges to a common forward pointed tip for enclosing and protecting a guidance head when in an extended position and is retractable into a corresponding recessed region formed within a missile nose when the drive unit is activated releasing the restraint.
A ceramic armor tile for attaching internally behind a wall of a structure and for cooperation in conjunction therewith, such that the wall acts as an external protective layer of the armor.
A Safe-and-Arm system for the prevention of unintentional operation of an explosive device by interrupting a detonation train, the system employing an interruptive transfer assembly made of silicon and suitable for implementing in a MEMS device, the assembly including a silicon based transfer charge carrier on a porous explosive passageway made by etching, the passageway extending between at least two ports on the circumference of the transfer assembly, and a drive means that can mechanically bring about at least one armed state of a detonation train.
F42C 15/184 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a slidable carrier
F42C 15/188 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a rotatable carrier
F42C 15/34 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by a blocking-member in the pyrotechnic or explosive train between primer and main charge
79.
System and a method for protected reloading of a remote controlled weapon station
RCWS (Remote Controlled Weapon System or Station) of the deck-penetrator type and a method for protected reloading of a weapon system that is fed by belt of rounds from an ammunition container that is positioned in the RCWS, wherein the RWCS includes a system for protected reloading of the weapons system, that comprises—a bracket, that on it the ammunition container is mounted, and the bracket is amenable to be propelled via an opening in the deck of the vehicle upon which the RCWS is positioned, unto an inner space of the carrier vehicle and back from this space to the RCWS; and means for movably positioning the bracket, in at least two states—a first state wherein the bracket is positioned inside the inner space of the carrier vehicle and for reloading anew the weapons system; and a second state wherein the bracket is a least substantially embedded in the RCWS for feeding the weapons system by a belt of rounds from inside of the ammunition container that is positioned on the bracket.
A system and method for generating compressed video with geographically-anchored-video functionality includes processing frames from a source video sequence by matching image content of the frames to image data from a geographic database to derive the geographic locations of pixels within at least part of the frames. The source video sequence is then compressed by a lossy video compression technique to generate a compressed video sequence, and the compressed video sequence is encoded together with data indicative of the geographic locations of pixels as a composite data stream. Also disclosed are methods for selective video archiving and retrieval based on the geographical footprint of the image content.
H04N 21/231 - Content storage operation, e.g. caching movies for short term storage, replicating data over plural servers or prioritizing data for deletion
H04N 21/266 - Channel or content management, e.g. generation and management of keys and entitlement messages in a conditional access system or merging a VOD unicast channel into a multicast channel
H04N 21/84 - Generation or processing of descriptive data, e.g. content descriptors
81.
Armoring combatants' compartment in a wheeled vehicle against explosive charges
A Wheeled vehicle comprises a chassis and a combatants' compartment for protection from an explosion, where the combatants' compartment is formed with an internal space and a bottom area sector attachable to the chassis and where the compartment has a plurality of inner beams that are formed with anchoring means along their lengths and installed in the combatants compartment's inn space and a plurality of outer beams attached to the chassis, where the anchoring means pass through openings formed in the bottom area sector of the combatants' compartment and protrude outwards from it for connecting the inner beams to the outer beams.
A damping suspension for an add-on armor system of an ACV (Armored Combat Vehicle), comprises mounting means for mounting said add-on armor system to an ACV; and damping means coupled to said mounting means and to said add-on armor system's armor means, in order to damp vibrations and restrain shocks unto which said armor means might be exposed as an outcome of said ACV's travel; and wherein said damping suspension is characterized by that said damping suspension includes a device of the ‘wire rope isolator’ type.
A micro-opto-electro-mechanical system having a proof mass; at least one illumination source for providing illumination; an illumination detector; peripheral electronics; and an illumination mitigating mechanism for mitigating the effect of illumination emitted from the at least one illumination source on the peripheral electronics. According to various embodiments, the illumination mitigating mechanism includes handles disposed on the proof mass, an illumination collimating device, a substrate with a recess, a narrow beam light source, an illumination absorbing layer or optical limiters.
G01J 1/32 - Photometry, e.g. photographic exposure meter by comparison with reference light or electric value intensity of the measured or reference value being varied to equalise their effects at the detector, e.g. by varying incidence angle using variation of intensity or distance of source using electric radiation detectors adapted for automatic variation of the measured or reference value
A firing mechanism security apparatus prevents runaway machine gun fire by first sensing rounds being fired and sensing that the trigger mechanism is not instructing the weapon to fire. A mechanical actuator may block a path of the ammunition between the ammunition storage box and the machine gun or blocks spent ammunition from being ejected. Without engaging the trigger mechanism directly, a stopper signaled by a controller or motor may move from a first position to a second position and thereby be interposed between rounds of ammunition adjacent the ammunition storage box or between the ammunition feeder and the machine gun. The ammunition feeder may, alternatively, include a mechanical actuator that receives a signal from a motor or controller, the actuator capable of blocking the feeder's advancement of ammunition. Additionally, the gun may be elevated as a safety precaution.
Substantially removing shadows in video images obtained from a camera viewing a scene, at variable pointing angles and magnification, by digital processing of a sequence of frames in the video signal, the processing including—(a) creating and maintaining a model image of the scene, by accumulating image data from a plurality of video frames; (b) in the model image, detecting and defining model shadow zones; (c) calculating correction factors for the model shadow zones; (d) for each frame of the video signal—defining, in the image carried by the signal, shadow zones that correspond to respective model shadow zones; and (e) correcting video signal values in shadow zones accordingly.
A method for identifying an object based at least in part on a reference database including two-dimensional images of objects includes the following steps: (a) providing a three-dimensional model reference database containing a plurality of estimated three-dimensional models, wherein each estimated three-dimensional model is derived from a corresponding two-dimensional image from the two-dimensional reference database; (b) sampling at least one image of an object to be identified; (c) implementing at least one identification process to identify the object, the identification process employing data from the three-dimensional model reference database.
A method for combining power of separate directed energy beams each associated with a separate firing unit, on a common spot on target. The firing units are coordination and synchronization unit (FUSU) tracks a target and assigns a master firing unit and slave firing units. The master firing unit sends a guide beam to the target, forming a local coordinate system on said target, while the slave firing units track the target and track at least one spot of EM (electromagnetic) radiation on the target. The slave units calculate a direction vector, and fire a power beam at the target, together with the master unit.
The provided optical system allows selective spectral transfer of radiation, and provides a reflecting field of view at an undesired range directed towards cold surfaces. A removable spectral filter having a high transmittance at a first spectral range and a low transmittance at a second spectral range is disposed outside a cold shield. A reflective surface faces the detecting device and provides the detector a reflecting field of view at the second spectral range directed back towards the cold shield, and a blackened cold skirt thereof. Alternatively, a dichroic mirror is disposed inside the cold shield and has a high reflectance at a first spectral range and a high transmittance at a second range. The detecting device includes a first and a second arm of the cold shield to accommodate respective optical channels.
G01N 21/35 - Investigating relative effect of material at wavelengths characteristic of specific elements or molecules, e.g. atomic absorption spectrometry using infrared light
G01J 5/06 - Arrangements for eliminating effects of disturbing radiationArrangements for compensating changes in sensitivity
A method for displaying to an operator a rectangular image having a wide field of view of a scene, includes forming a virtual cylinder from the rectangular image, as if it was first printed on a transparent sheet such that it is visible from both sides of the sheet, and then rolled to form the cylinder. A perspective view of the cylinder is provided, vertically dividing the cylinder into two halves. One of the cylinder halves is vertically shifted until there is no overlap between the two halves. The ellipse which is formed between the two halves following the shifting step is defined as an orientation plane.
Provided is an RPG disruption system (RDS) for protecting an enclosure against RPG's, the system including a casing fixed in close proximity to a wall of the enclosure facing an anticipated RPG threat. The casing includes an anvil accommodating a propelling mechanism for propelling the disrupting element, and an activating system for activating the propelling mechanism so as to propel the disrupting element towards an approaching RPG, to thereby neutralize it.
An artillery projectile for firing from an artillery gun, mortar or artillery rocket launcher. The artillery projectile includes a body, a payload with a number of inert fragments located within the body, a booster motor associated with the body for accelerating the body with the payload to a penetration velocity, and an opening arrangement associated with the body and deployed for initiating release of the fragments. The artillery projectile further includes a control system causally associated with the booster motor and the opening arrangement. The control system is configured to generate a first command to actuate the booster motor and a second command to actuate the opening arrangement.
F42B 15/10 - Missiles having a trajectory only in the air
F42B 12/64 - Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile the submissiles being of shot- or flechette-type
A system for providing a spatially aligned head-up display to a user viewing a scene through a display the system includes: an image sensing system including at least one image sensor deployed to sample images of the user's face, the image sensing system generating data derived at least in part from the images; a display for displaying visible indications to the user superimposed on the scene; and a control system associated with the image sensing system and the display, the control system being configured to: process data from the image sensing system to determine a position and attitude of the user's face, determine a viewing direction from at least one eye of the user to a point of interest within the scene, and actuate the display to display a visible indication aligned with the viewing direction that provides a spatially aligned head-up display to the user.
A method for operating a guided munition with a switchable fuze arrangement includes launching the guided munition towards a target. During flight of the guided munition, images are provided to a remote operator, who supplies a switching input. Responsive to said switching input, the fuze arrangement is switched to either of at least two of the following states: a delayed detonation state in which detonation of the explosive charge is delayed by a time delay after impact of the guided munition, an impact detonation state in which detonation of the explosive charge occurs on impact of the guided munition, a proximity detonation state in which detonation of the explosive charge is triggered by a proximity sensing arrangement, and a disabled state in which the guided munition functions as a guided kinetic shell without detonation of the explosive charge.
In accordance with one embodiment, a method for remote identification of at least one gas includes sampling a plurality of spectral images of a scene wherein each spectral image is sampled at a different wavelength, providing a reference spectral image, and generating a spatial displacement expression by detecting the spatial misregistration in at least one region of the spectral images between the reference spectral image and at least one of the plurality of spectral images. At least one reference spatial displacement expression is provided corresponding to at least one gas, and at least one identification process is implemented to identify at least one gas. The identification process employs the generated spatial displacement expression and the at least one reference spatial displacement expression. Optionally the reference image is one of the sampled spectral images, the reference spatial displacement expression is provided from a general or adapted library, and the concentration of the gas can be determined.
G06K 9/00 - Methods or arrangements for reading or recognising printed or written characters or for recognising patterns, e.g. fingerprints
G06K 9/62 - Methods or arrangements for recognition using electronic means
G06K 9/64 - Methods or arrangements for recognition using electronic means using simultaneous comparisons or correlations of the image signals with a plurality of references, e.g. resistor matrix
G06K 9/68 - Methods or arrangements for recognition using electronic means using sequential comparisons of the image signals with a plurality of reference, e.g. addressable memory
G01N 31/00 - Investigating or analysing non-biological materials by the use of the chemical methods specified in the subgroupsApparatus specially adapted for such methods
H01L 31/00 - SEMICONDUCTOR DEVICES NOT COVERED BY CLASS - Details thereof
96.
Apparatus and method for splitting and removing a shroud from an airborne vehicle
The present invention relates to an apparatus for splitting and removing a shroud from an airborne vehicle, that comprises a shroud that includes two components, linkable one to another along their lengths, and wherein upon being fastened one to the other, they form a shroud with a lengthwise axis and an inner space, and having a base sector around the circumference of the bottom part of said shroud, and wherein said base is connectable to said airborne body and a fastening assembly for fastening said two components of said shroud one to the other, and wherein said fastening assembly is given to be torn on stretching upon detonation of a pyrotechnic charge and a piston assembly that disassembled at the completion of the piston's stroke, and is operable by said pyrotechnic charge, and wherein said piston assembly serves for timed tearing of said fastening assembly.
A method for identifying within a working image of a scene a point of interest designated within a designation image of a scene, the designation image being taken along a first viewing direction and the working image being taken along a second viewing direction, the second viewing direction being significantly non-parallel to the first viewing direction, the method comprising the steps of: obtaining a designation image of the scene; obtaining a working image of the scene; correlating said designation image and said working image with each other, directly or by correlating each of said designation image and said working image with a common reference image, so as to derive an interrelation between said designation image and said working image; and employing said interrelation between said designation image and said working image to derive a location within said working image of a point of interest designated within said designation image, characterized in that the method further comprises: obtaining a secondary designation image taken along a viewing direction displaced from, but similar to, the first viewing direction; and co-processing said designation image and said secondary designation image to derive range information relating to a plurality of pixels in said designation image, thereby defining a partial relative three-dimensional model of a portion of the scene relative to the viewing direction of said designation image, wherein said partial relative three-dimensional model is used in said step of correlating.
A method, a system, and a product for enhancing the start of a turbine engine by providing a replaceable ignition module including a solid combustible substance, that when ignited, or a solid oxidizer substance, that when heated, releases hot gases rich in oxidizing species. The module includes a solid substance(s) appropriately selected as: a solid-propellant grain (SPG) and a solid oxidizer (SO); or an oxygen-rich burning substance (OBSS); or a solid-propellant grain and an oxygen-rich burning substance; or an oxygen-rich burning solid substance and a solid oxidizer. The replaceable module further contains an initiator for the initiation of the solid combustible substance, or solid-propellant grain by an initiation command (IC). The hot gases released by the ignition module start and enhance the combustion process of the air-and-fuel mixture by successive fuel heating and vaporization, followed by ignition.
A miniature lightweight high-maneuverability missile (10) has a missile body (12) with three sets of at least two aerodynamic control surfaces (14, 16, 18) for independent control of roll, pitch and yaw of the missile. Each set of control surfaces (14, 16, 18) is independently controlled by a corresponding actuator (20) deployed within the missile body (12). Other preferred features include selection of an elevation angle of incidence at a target, and switching between explosive and kinetic modes of operation.
F42B 10/62 - Steering by movement of flight surfaces
F41G 7/00 - Direction control systems for self-propelled missiles
F42B 10/00 - Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missilesArrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
An arrow-type warhead (100,200,300,400,500,600,700) comprises an envelope (102,202), a filling (108), a hardened head section (104) to promote penetration of the target and a stabilizing mechanism (106,210,302,402,502,602) to stabilize the warhead in flight, hi some embodiments the filling (108) is pyrophoric and undergoes an exothermic reaction with the envelope upon impact. In other embodiments the filling is incendiary and undergoes reaction with the envelope upon impact in an oxygen rich-environment. In yet other embodiments, the filling is explosive. In all embodiments, the warhead may be equipped with a mini-rocket propulsion mechanism (802) for propelling the warhead to the target.
F42B 12/44 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materialsProjectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for producing chemical or physical reactionProjectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for signalling of incendiary type
patents
