Patents Assigned to General Dynamics
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Publication number: 20130047833Abstract: A weapon system is provided. The weapon system includes a receiver and an operating group. The operating group includes a barrel extension at least partially housed within the receiver and arranged to axially translate relative to the receiver; an operating rod (op-rod) assembly arranged to axially translate within the barrel extension; and a bolt assembly arranged to axially translate within the barrel extension. The system further includes a gas accelerator coupled to the barrel and the op-rod assembly; a buffer assembly including a self-centering spring and a hydraulic piston assembly having a first end coupled to the receiver and a second end coupled to the barrel extension; and a feeder coupled to the receiver and configured to provide the round to the operating group.Type: ApplicationFiled: July 30, 2012Publication date: February 28, 2013Applicant: GENERAL DYNAMICS ARMAMENT AND TECHNICAL PRODUCTS, INC.Inventors: David Steimke, Glenn Rossier, Larry Hayes, Douglas Parker
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Patent number: 8376373Abstract: The present embodiments relate to a semi-active suspension control system that utilizes controllable dampers for the purpose of improving maneuverability and vehicle hull stabilization. The disclosed semi-active control system can work in conjunction with a height management unit and on vehicles having variable ride heights, and hull stability and maneuverability can be achieved regardless of vehicle payload and ride height.Type: GrantFiled: November 22, 2010Date of Patent: February 19, 2013Assignee: General Dynamics Land SystemsInventor: Daniel Francois Conradie
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Patent number: 8379752Abstract: Embodiments include methods for determining synchronization/pilot sequences (SPS) to be utilized in conjunction with transmissions by antennas of a multiple-antenna transmitter. The SPS include pilot signals that are positioned at subcarriers that are orthogonal in frequency with subcarriers at which pilot signals of other antennas are positioned. The pilot signals may be unevenly spaced across the in-band subcarriers. The multiple-antenna transmit system generates a plurality of wireless signals, each of which may include an SPS having synchronization information in a first plurality of in-band subcarriers and the pilot signals in a second plurality of in-band subcarriers. The wireless signals are simultaneously radiated over a wireless communication channel using a different antenna. A receiver receives channel-affected versions of the wireless signals, and produces a corrected signal by applying corrections to the received signal based on estimated channel perturbations within the received signal.Type: GrantFiled: March 17, 2010Date of Patent: February 19, 2013Assignee: General Dynamics C4 Systems, Inc.Inventors: John E. Kleider, Benjamin Russell Hamilton
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Patent number: 8358644Abstract: An embodiment includes a method for generating a set of synchronization/pilot sequences (SPS) by generating a plurality of candidate SPS using different initial conditions. Correlations are performed among the candidate SPS to generate a plurality of correlation values, and a plurality of permutations of the candidate SPS are determined, where each permutation includes a different set of candidate SPS, and wherein each permutation includes a number, D, of candidate SPS. In addition a selected permutation is identified from the plurality of permutations, where the selected permutation corresponds to the set of SPS being generated. A system includes a transmitter adapted to generate a wireless signal in which an SPS is embedded by combining each SPS of the set with phase shifted input data, determining peak-to-average power ratios (PARs) for at least some of the combined signals, and identifying a selected combined signal based on the PARs.Type: GrantFiled: March 19, 2008Date of Patent: January 22, 2013Assignee: General Dynamics C4 Systems, Inc.Inventors: Robert John Baxley, John Eric Kleider
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Patent number: 8355466Abstract: A method and system are provided for reducing power amplifier induced distortion. Power amplifier induced distortion is iteratively estimated and cancelled. When the difference between the current estimated power amplifier distortion and the previous estimated power amplifier distortion is less than a convergence threshold, particular M-QAM constellation points that are still in error are determined A M-QAM constellation point correction routine is provided that can move the incorrectly estimated M-QAM constellation points that are in error towards their expected quadrants by generating updated M-QAM constellation points. The remaining estimated non-linear power amplifier induced distortion in the received signal can then be estimated and canceled.Type: GrantFiled: September 25, 2009Date of Patent: January 15, 2013Assignee: General Dynamics C4 Systems, Inc.Inventors: John Kleider, Anthony Smith
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Patent number: 8342074Abstract: A system and method for visual awareness that replaces transparent armor with opaque armor while still providing for clear vision for the occupants of a vehicle. The system and method may include a number of components with at least one partially mirrored surface. A component may have an armored base and a reflective surface or other means for directing light. The components may be arranged in a manner to block the direct path of a threat while still allowing a given optical path through the system.Type: GrantFiled: May 20, 2011Date of Patent: January 1, 2013Assignee: General Dynamics Armament and Technical Products, Inc.Inventors: Ajit Yeshwant Sane, William E. Howard, Russell J. Mitchell, Paul A. Palmer
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Patent number: 8331863Abstract: An embodiment for wirelessly communicating a signal includes a transmitter combining a plurality of phase shifted input data signals with a plurality of synchronization/pilot sequences to produce a plurality of combined signals, performing frequency domain-to-time domain transformations of the combined signals to produce a plurality of candidate signals, determining peak-to-average ratios for at least some of the plurality of candidate signals, identifying a selected signal from the plurality of candidate signals based on the peak-to-average ratios, and transmitting the selected signal over a wireless communication channel.Type: GrantFiled: January 26, 2012Date of Patent: December 11, 2012Assignee: General Dynamics C4 Systems, Inc.Inventors: John Eric Kleider, Robert John Baxley
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Patent number: 8330614Abstract: A telemetry system is described in which a plurality of channels are coupled to a bus. A control subsystem controls the channels so that one of the channels presents to the bus during its designated time period a channel characteristic. The control subsystem interrogates in the analog domain each of the channels during its designated time period, and forms a signal representative of the channel characteristic. The control subsystem may combine one or more of the signals into a digital packet, and transmit the same via transceiver over a wireless network. The channels may be contained within a submersible enclosure and displaced at intervals along the bus, thereby forming an array for monitoring waterborne threats. The array may lie along an ocean floor, may be towed by a marine vehicle, or may suspended from a deployable buoy containing the control subsystem, transceiver, and a remote power source. The array may further comprise a defensive countermeasure deployable responsive to detecting a threat.Type: GrantFiled: September 15, 2009Date of Patent: December 11, 2012Assignee: General Dynamics Advanced Information SystemsInventors: Michael D. Holt, Kenneth B. Tysinger, J. Lamar Chancey
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Patent number: 8331420Abstract: Embodiments of methods and apparatus for wirelessly communicating signals include one or more transmitters configured to generate a plurality of wireless signal for transmission. Each of the wireless signals includes a plurality of pilot signals represented in a plurality of unevenly spaced, in-band subcarriers. Pilot signals of each wireless signal are positioned at subcarriers that are orthogonal in frequency with subcarriers at which pilot signals of all other wireless signals are positioned. According to an embodiment, subcarrier indices each the plurality of pilot signals are determined using a third order or higher order polynomial parameterization of pilot subcarriers in conjunction with a convex optimization algorithm to produce pilot signals having near-optimal channel estimate mean square error (MSE) performance. The wireless signals are simultaneously radiated over a wireless communication channel using a plurality of co-located or distributed antennas.Type: GrantFiled: December 30, 2009Date of Patent: December 11, 2012Assignee: General Dynamics C4 Systems, Inc.Inventors: John E. Kleider, Benjamin Russell Hamilton
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Patent number: 8312813Abstract: A deployable fairing is driven off of high-pressure gun gases to reduce aerodynamic drag and extend the range of the artillery shell. An artillery shell is provided with a fabric fairing and a piston attached thereto in a rear section of the shell in a stowed state and a chamber. During launch high-pressure gun gasses are captured and stored in the chamber. Once the shell clears the end of the artillery tube, the pressure aft of the shell drops from the high pressure inside the tube to atmospheric pressure outside the tube. The high pressure gun gasses stored in the chamber act over the top surface of the piston to drive the piston aft against the much lower pressure behind the projectile to deploy the fabric fairing attached thereto to reduce the base area of the projectile creating or extending the boat-tail of the shell, hence reduce aerodynamic drag. The aft driven piston engages a locking mechanism that locks the piston in a deployed position.Type: GrantFiled: July 30, 2010Date of Patent: November 20, 2012Assignees: Raytheon Company, General Dynamics Ordnance and Tactical SystemsInventors: Brian K. McDermott, Kevin R. Greenwood, James D. Streeter
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Patent number: 8311035Abstract: An embodiment of a method for communicating call control signaling information in a communications system that includes a user equipment (UE) and a base includes the UE formatting the call control signaling information, transmitting the call control signaling information over a first logical channel that is mapped to a first transport channel, and transmitting user traffic over a second logical channel that is mapped to a second transport channel. In an embodiment, the base receives the call control signaling information from the UE over the first logical channel, receives the user traffic from the UE over the second logical channel, and transmits the call control signaling information to a core network. In an embodiment, the communication system is an IP network in which information is exchanged between the UE and the base using a W-CDMA transmission protocol. The base may form a portion of a satellite-based radio network.Type: GrantFiled: September 30, 2008Date of Patent: November 13, 2012Assignee: General Dynamics C4 Systems, Inc.Inventors: Dan Bossler, Elizabeth Marie Raslavsky, Nicole Marie Loomis
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Patent number: 8290147Abstract: Systems and methods efficiently process digests, hashes or other results by performing multiplicative functions in parallel with each other. In various embodiments, successive processing stages are provided, with each stage performing parallel multiplicative functions and also combining input terms to reduce the total number of terms that remain to be processed. By progressively combining the active terms into a smaller number of terms for subsequent processing, the time needed to process a result can be significantly reduced.Type: GrantFiled: October 30, 2009Date of Patent: October 16, 2012Assignee: General Dynamics C4 Systems, Inc.Inventors: Gerardo Orlando, David King, Mark Krumpoch
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Publication number: 20120250733Abstract: A global positioning system (GPS) receiver that is configured to rapidly acquire GPS signals in space applications and a method for rapidly acquiring GPS signals in space applications is disclosed. In an embodiment, the GPS receiver includes, but is not limited to, a GPS signal acquisition component comprising a time domain correlation module. The GPS signal acquisition component is adapted to acquire a GPS signal by receiving data from the GPS signal and processing the data to detect the GPS signal.Type: ApplicationFiled: April 2, 2012Publication date: October 4, 2012Applicant: GENERAL DYNAMICS ADVANCED INFORMATION SYSTEMSInventor: Thomas Michael King
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Publication number: 20120239247Abstract: An active blast mitigation system includes one or more sensors configured to produce a set of acceleration signals indicative of a dynamic response of the vehicle. A control system communicatively coupled to the plurality of sensors is configured to determine the dynamic response of the vehicle based on the set of acceleration signals and determine whether mitigation is required based on the dynamic response of the vehicle. If it is determined that mitigation is required, the control system produces one or more countermeasure signals selected to at least partially counteract the dynamic response. Countermeasure assemblies communicatively coupled to the control system are configured to activate in response to the one or more countermeasure signals.Type: ApplicationFiled: August 17, 2011Publication date: September 20, 2012Applicant: GENERAL DYNAMICS LAND SYSTEMS, INC.Inventor: James Michael Eridon
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Publication number: 20120225683Abstract: Systems and methods are described for managing channel selection among a plurality of mesh points in a wireless network. In one embodiment, a method includes receiving a first announcement that includes channel exclusion information from a first mesh point; managing a distributed channel exclusion list based on the announcement; and generating a second announcement to the first mesh point based on the channel exclusion list.Type: ApplicationFiled: February 24, 2012Publication date: September 6, 2012Applicant: GENERAL DYNAMICS C4 SYSTEMS, INC.Inventors: Gary Matulis, Magued Barsoum, Owais Hassan, John Pacheco
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Patent number: 8259779Abstract: A wireless network (20) with at least a first radio communication unit (24) and a second radio communication unit (26) transmits and receives signals with minimal interference from the surrounding environment of the first unit (24) and second unit (26). The first radio communication unit (24) determines frequencies (54) having power level above a threshold (52), and creates a list of these frequencies (50) to be transmitted to the second radio communication unit (26). The second radio communication unit (26) places notches (140) in its transmission band (88) based on frequencies (54) in the list (50), reserved frequencies (132), and local frequencies (92) having signal energy above a threshold (90). When transmitting a signal (42), the second radio communication unit (26) avoids transmitting in frequencies that have notches (140).Type: GrantFiled: December 9, 2008Date of Patent: September 4, 2012Assignee: General Dynamics C4 Systems, Inc.Inventors: Scott David Blanchard, Randall K. Bahr
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Publication number: 20120216036Abstract: Systems and methods are described for securely transmitting data in a mesh network. The method includes: performing on a processor, assembling a header with a recipient address, wherein the recipient address designates an encryption endpoint; associating encrypted data with the header; and presenting a packet for transmittal on the mesh network, wherein the packet includes the header and the encrypted data.Type: ApplicationFiled: February 20, 2012Publication date: August 23, 2012Applicant: GENERAL DYNAMICS C4 SYSTEMS, INC.Inventors: Magued Barsoum, Tong Zhu
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Publication number: 20120211593Abstract: The invention is a projectile, device and system having a roll control device which may be fixed or deployable, for providing torque counter to the spin of the projectile and providing drag on the projectile. The roll control device includes a guidance collar rotatably attached to the projectile located near a front end of the projectile wherein the guidance collar includes one or more guidance collar aero-surfaces shaped to provide torque counter to the spin on the projectile. The guidance collar aero-surfaces may be controlled by a brake and guidance electronics on the projectile. The invention also includes a body collar fixedly attached to the projectile aft of the guidance collar, wherein the body collar includes one or more body collar aero-surfaces and fixed or deployable drag devices. Another embodiment use only a guidance collar aero-surfaces to orient a fixed drag device relative to an Earth inertial reference frame to create asymmetrical drag on the projectile and thereby altering its trajectory.Type: ApplicationFiled: November 12, 2009Publication date: August 23, 2012Applicant: General Dynamics Ordnance and Tactical Systems, Inc.Inventors: Joseph P. Morris, Douglas L. Smith
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Publication number: 20120193481Abstract: A payload mount adapter assembly for use with an aircraft is disclosed. The payload mount adapter assembly includes, but is not limited to an upper section that is configured for mounting to the aircraft and a lower section that is configured to receive a payload. The lower section is releasably engaged with the upper section such that the lower section is substantially unadjustable with respect to the upper section when the lower section is in a fixed state and the lower section is substantially adjustable with respect to the upper section when the lower section is in a released state.Type: ApplicationFiled: January 27, 2011Publication date: August 2, 2012Applicant: GENERAL DYNAMICS ARMAMENT AND TECHNICAL PRODUCTS, INC.Inventors: Thomas M. DOYLE, JR., Travis L. JOHNSTON
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Publication number: 20120182417Abstract: Systems and methods are provided to automatically determine a position of a reticle of a rifle scope or other telescope that provides a visual image to an eye of a viewer. A near-infrared or other illuminating light is generated and applied to illuminate the reticle of the telescope. The illuminated image of the reticle is optically transmitted to a camera or other detector that captures an image of the reticle. Processing electronics then automatically determine the position of the reticle based upon the position of the illuminated image of the reticle within the captured image. Appropriate feedback about the determined position of the reticle or any other information may be displayed in the visual image provided by the telescope.Type: ApplicationFiled: January 19, 2012Publication date: July 19, 2012Applicant: GENERAL DYNAMICS ADVANCED INFORMATION SYSTEMSInventor: Jonathan Edward Everett