Monopulse Patents (Class 342/80)
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Patent number: 6661366Abstract: A radar system and technique provide the capability to detect a target of interest and maintain the detection in the presence of multiple mainlobe and sidelobe jamming interference. The system and technique utilize digital beamforming to form sub-arrays for canceling jamming interference. Jamming is adaptively suppressed in the sub-arrays prior to using conventional deterministic methods to form the sum, &Sgr;, and difference, &Dgr;, beams for monopulse processing. The system and technique provide the ability to detect a target of interest, provide an undistorted monopulse ratio, m, and maintain target angle estimation, in the presence of multiple mainlobe and multiple sidelobe jammers.Type: GrantFiled: June 15, 2001Date of Patent: December 9, 2003Assignee: Lockheed Martin CorporationInventor: Kai-Bor Yu
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Patent number: 6630902Abstract: A radar receiver is shown wherein the frequency of a first local oscillator is changed to bring an intermediate frequency signal representative of a moving target into frequency coincidence with a signal from a reference oscillator of fixed frequency.Type: GrantFiled: July 28, 1977Date of Patent: October 7, 2003Assignee: Raytheon CompanyInventors: Andrew F. Fenton, Thomas D. Shovlin
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Patent number: 6618008Abstract: A monopulse phased array system comprises antenna elements with T/R modules controlled a beam steering computer. The space in which the antenna elements are arranged is divided into quadrants which are defined relative to the main axis of the radar beam. From the signals received by means of separate antenna elements, sum signals and first and second angle difference signals are derived: After combination of these signals delivered by the T/R modules, control signals are obtained for resteering the radar beam generated under the control of the computer mentioned. Each of the T/R modules is provided with two 180° phase shifters for determining the angle difference signals.Type: GrantFiled: February 4, 2002Date of Patent: September 9, 2003Assignee: Nederlandse Organisatie voor toegepast-natuurwetenschappelijk Pnderzoek TNOInventor: John Arthur Scholz
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Publication number: 20030164791Abstract: To realize a monopulse radar system wherein the velocity of a mobile body, distance between an obstacle and the mobile body and relative velocity can be detected and simultaneously, the direction of the obstacle can be detected, in a monopulse radar system wherein an azimuth is detected depending upon amplitude difference or phase difference between signals respectively received by plural receiving antennas, an array antenna composed of plural antenna elements is used for each transmitting antenna and each receiving antenna, at least one of the transmitting antenna and the receiving antenna is provided with an antenna switch for switching an antenna beam shape to a short angle/long distance or a wide angle/short distance and a switch control device that controls the switching of the antenna switch is provided.Type: ApplicationFiled: March 12, 2003Publication date: September 4, 2003Applicant: Hitachi, Ltd.Inventors: Hiroshi Shinoda, Hiroshi Kondoh
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Publication number: 20030160718Abstract: A monopulse radar system aims to correct an amplitude error and a phase error developed between receiving channels and improve the accuracy of a detected angle.Type: ApplicationFiled: August 26, 2002Publication date: August 28, 2003Applicant: Hitachi, Ltd.Inventor: Toshiyuki Nagasaku
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Patent number: 6603421Abstract: A combined defense and navigational system on a naval vessel is disclosed. The disclosed system includes a track-while-scan pulse radar which is controlled to provide either navigational information or tracking information on selected targets. Additionally, the disclosed system includes a plurality of guided missiles, each of which may be vertically launched and directed toward intercept of a selected target either by commands from the track-while-scan radar or from an active guidance system in each such missile.Type: GrantFiled: July 28, 1977Date of Patent: August 5, 2003Assignee: Raytheon CompanyInventors: George W. Schiff, David K. Barton, Robert E. Millett, Carroll D. Phillips
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Publication number: 20030112172Abstract: To realize a monopulse radar system wherein the velocity of a mobile body, distance between an obstacle and the mobile body and relative velocity can be detected and simultaneously, the direction of the obstacle can be detected, in a monopulse radar system wherein an azimuth is detected depending upon amplitude difference or phase difference between signals respectively received by plural receiving antennas, an array antenna composed of plural antenna elements is used for each transmitting antenna and each receiving antenna, at least one of the transmitting antenna and the receiving antenna is provided with an antenna switch for switching an antenna beam shape to a short angle/long distance or a wide angle/short distance and a switch control device that controls the switching of the antenna switch is provided.Type: ApplicationFiled: February 27, 2002Publication date: June 19, 2003Applicant: Hitachi, Ltd.Inventors: Hiroshi Shinoda, Hiroshi Kondoh
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Patent number: 6567034Abstract: In a radar system, sampled aperture data are received from an antenna array. The sampled aperture data include data that do not correspond to echo returns from a beam transmitted by the antenna. A covariance matrix is generating using the sampled aperture data. An eigenvalue decomposition is performed on the covariance matrix. A direction of arrival is determined from which at least one jammer is transmitting a signal included in the sampled aperture data, based on the eigenvalue decomposition.Type: GrantFiled: September 5, 2001Date of Patent: May 20, 2003Assignee: Lockheed Martin CorporationInventor: Kai-Bor Yu
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Publication number: 20030020646Abstract: A radar system and technique provide the capability to detect a target of interest and maintain the detection in the presence of multiple mainlobe and sidelobe jamming interference. The system and technique utilize the versatility of digital beamforming to form sub-arrays for canceling jamming interference. Jamming is adaptively suppressed in the sub-arrays prior to using conventional deterministic methods to form the sum, &Sgr;, and difference, &Dgr;, beams for monopulse processing. The system and technique provide the ability to detect a target of interest, provide an undistorted monopulse ratio, m, and maintain target angle estimation, in the presence of multiple mainlobe and multiple sidelobe jammers. Further, this system and technique are not constrained by requiring a priori knowledge of the jamming interference.Type: ApplicationFiled: June 15, 2001Publication date: January 30, 2003Inventor: Kai-Bor Yu
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Patent number: 6498581Abstract: A system identifies a number of targets within a main beam of an antenna array that transmits the main beam and receives echo returns from the main beam. A covariance matrix is generated using the echo returns. The presence of at least one target within a single range cell is detected. A plurality of consecutive pulses are transmitted in a direction of the single range cell within a sufficiently short period that the at least one target remains within the single range cell while the plurality of consecutive pulses are transmitted. An echo signal is sampled from each of the plurality of pulses. An updated covariance matrix is estimated each time the echo signal is sampled. An eigenvalue decomposition is updated each time the covariance matrix is updated. The number of targets in the single range cell is estimated, based on the updated eigenvalue decomposition.Type: GrantFiled: September 5, 2001Date of Patent: December 24, 2002Assignee: Lockheed Martin CorporationInventor: Kai-Bor Yu
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Publication number: 20020190892Abstract: A circuit (100) for performing base 10 logarithmic calculations of a binary signal in a digital system that optimizes accuracy of the calculation. The circuit comprises a priority encoder (108) for determining a most significant bit position of the binary number, with the most significant bit representing a base 2 logarithmic integer component of the input binary signal. A decimal selector (120) selects a predetermined number of bits to follow the base 2 logarithmic integer component determined by the priority encoder, with the predetermined number of bits representing a base 2 logarithmic fractional component following the integer component of the input binary signal. An adder (116) combines the integer component with the fractional component to thereby output a base 2 logarithmic value of the input binary signal. A multiplier (132) divides the base 2 logarithmic value of the input binary signal by a base 2 logarithmic value of 10 to thereby output a base 10 logarithmic value of the input binary signal.Type: ApplicationFiled: March 19, 2002Publication date: December 19, 2002Inventor: Brian L. Hallse
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Patent number: 6476760Abstract: A method and a radar sensor for determining an elevation angle error of a multibeam radar sensor are described. In order to detect an elevation angle of the multibeam radar system with respect to a predefined target, a plurality of laterally arranged cutting planes at a predefined distance are formed. The values of the corresponding antenna diagrams in each plane are stored in a suitable form, for example, normalized and in a parametric form taking into account the elevation angle &agr;. In order to reduce the size of the memory, it is sufficient to store one symmetry half for reasons of symmetry if additional information, for example, road clutter values are added, so that the upward or downward direction of the angle can be recognized. By comparing the measured echo values obtained by normalization and application of a quality factor, a corresponding elevation angle &agr; is obtained for each cutting plane.Type: GrantFiled: October 11, 2001Date of Patent: November 5, 2002Assignee: Robert Bosch GmbHInventors: Klaus Winter, Klaus-Peter Wagner, Sonja Eder, Herbert Olbrich, Jörg Schneemann
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Patent number: 6456238Abstract: An antenna array system with dynamic signal routing to a set of receivers. A monopulse electronically scanned antenna (ESA) has a plurality of antenna elements divided into subarrays. ESA beam steering phase shifters are associated with the respective subarrays of antenna elements, such that the output signals from the respective antenna elements associated with the respective quadrants are phase shifted and summed to provide respective subarray signals. A monopulse network responsive to the subarray signals provides monopulse outputs to a set of receivers. A beam steering controller provides phase shift commands to the ESA phase shifters to set the phase shift associated with the respective phase shifters of the subarrays. The controller commands the ESA phase shifters to modulate the phase shift of selected quadrants.Type: GrantFiled: May 15, 2001Date of Patent: September 24, 2002Assignee: Raytheon CompanyInventor: William P. Posey
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Publication number: 20020130808Abstract: An AC power source applies power to a primary coil that is provided in a fixed part. An AC current flowing through the primary coil induces electromotive force in a secondary coil that is provided in a movable part. The AC electromotive force induced in the secondary coil is converted by an AC/DC converter into DC power, which is input to a drive control section.Type: ApplicationFiled: November 5, 2001Publication date: September 19, 2002Applicant: MITSUBISHI DENKI KABUSHIKI KAISHAInventors: Tomoaki Fukushima, Ichiro Shirokawa, Hidetaka Yamauchi, Yoshihiko Konishi, Akio Iida
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Patent number: 6404379Abstract: A method and system for identifying the locations of plural targets lying within a main beam of a monopulse antenna including four ports for generating sum, elevation difference, azimuth difference and double difference signals. The method comprises the steps of forming a monopulse ratio matrix from the sum, elevation difference, azimuth difference and double difference signals; and determining eigenvalues of the monopulse ratio matrix. These eigenvalues are then used to determine the angular locations of the plural targets. Preferably, the eigenvalues are determined by performing an eigenvalue decomposition of the monopulse ratio matrix to generate eigenvalues, and the angles of the targets may be determined from the eigenvalues by the use of a look-up table.Type: GrantFiled: June 29, 2000Date of Patent: June 11, 2002Assignee: Lockheed Martin CorporationInventors: Kai-Bor Yu, Yibin Zheng
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Patent number: 6369746Abstract: A radar system includes a null processor coupled to transmit receive modules. The null processor inserts nulls in the sum pattern at locations for suppressing a jamming source. The null processor determines the difference pattern based upon the product: sum*sin(x), where sum is the sum pattern and x is the azimuth angle.Type: GrantFiled: July 13, 2000Date of Patent: April 9, 2002Assignee: Raytheon CompanyInventors: Leon Green, Joseph Preiss, Kai-Chiang Chang
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Patent number: 6297763Abstract: A method is provided of optimizing, within an area which itself contains a number of part areas, the coverage of a sensor which has an angle-dependent range in a least one plane, and which sensor is in addition arranged on a mobile platform. The method includes determining at least two movement directions for the sensor platform, determining a center of movement for the two movement directions, and also determining periods of time during which the sensor platform is to move in each of the two movement directions. The center of movement of the platform is preferably located within the search area.Type: GrantFiled: December 22, 1998Date of Patent: October 2, 2001Assignee: Telefonaktiebolaget LM Ericsson (publ)Inventors: Ola Thomson, Benny Bentland
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Patent number: 6246365Abstract: A radar apparatus comprising: a receiving antenna having an array antenna in which a plurality of antenna elements are arrayed in a horizontal direction; and a signal processing section for carrying out recognition of a target existing in a predetermined horizontal bearing range from receive signals received by the receiving antenna, by electrically carrying out horizontal scanning of an antenna pattern of the receiving antenna, wherein at least one of the antenna elements is placed with a shift in a vertical direction, and wherein the signal processing section detects an altitudinal bearing of the target by a monopulse method by use of a receive signal from the antenna element with the shift in the vertical direction.Type: GrantFiled: March 15, 1999Date of Patent: June 12, 2001Assignee: Toyota Jidosha Kabushiki KaishaInventor: Setsuo Tokoro
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Patent number: 6195035Abstract: A monopulse antenna system comprising an inner antenna and an outer antenna disposed symmetrically about a central axis of symmetry. A central aperture is located at the axis of symmetry through which a weapon system may fire or an additional sensor may be located. The inner antenna is preferably annular in shape and produces a relatively broad antenna pattern. The outer antenna is also preferably annular and produces a beam pattern with many lobes. The received signals A and B, from each beam pattern, are combined in a hybrid to produce sum signals (A+B) and difference signals (A−B), which are then processed to produce a target off-axis radius relative to the antenna main beam axis, i.e., the axis of symmetry.Type: GrantFiled: October 12, 1984Date of Patent: February 27, 2001Assignee: Textron Systems CorporationInventor: Joseph R. Wood
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Patent number: 6133866Abstract: A method of operating a radar to track echo signals from a target in the presence of a barrage jammer is shown to comprise the steps of actively determining the apparent direction of the combination of echo signals from a target and jamming signals, passively determining the actual direction and average power of a barrage jammer, calculating, from the foregoing, the actual direction of the target and instituting range and angle tracking of the target when the target is clear of the jamming signals.Type: GrantFiled: May 1, 1981Date of Patent: October 17, 2000Assignee: Raytheon CompanyInventor: Irving Kanter
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Patent number: 6087974Abstract: A monopulse system generates sum (.SIGMA.), elevation difference (.DELTA..sub.EL), azimuth difference (.DELTA..sub.AZ), and double difference (.DELTA..sub..DELTA.) signals, and generates a covariance matrix. The covariance matrix is decomposed to produce at least the principal eigenvector. The location or angular direction within the main beam of a single target is determined from the real component of the quotient of elements of the principal eigenvector, by the use of a look-up table. In another embodiment of the invention, the eigenvalues are generated from the covariance matrix, and the number of significant eigenvalues determines the number of targets within the main beam. If a single target is found, its location is found as described above. If two targets are found in the main beam, the locations of the two targets are determined by a closed-form solution of quadratic equations.Type: GrantFiled: August 3, 1998Date of Patent: July 11, 2000Assignee: Lockheed Martin CorporationInventor: Kai-Bor Yu
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Patent number: 6040795Abstract: Data is acquired by transmitting radio waves or by receiving radio waves by means of a fixed beam provided in a vehicle-mounted radar apparatus, and an antenna unit is provided which has such an antenna gain that a straight line-of-sight distance with respect to each straight line-of-sight angle from a subject vehicle to a preceding vehicle traveling on a subject-vehicle lane is set as a maximum detection distance. Therefore, it is possible to detect a preceding vehicle traveling on a subject-vehicle lane from a subject vehicle, and not detect objects such as vehicles which are present in a longer distance than is necessary, thereby alleviating a burden on signal processing.Type: GrantFiled: January 16, 1998Date of Patent: March 21, 2000Assignee: Mitsubishi Denki Kabushiki KaishaInventor: Masahiro Watanabe
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Patent number: 6005512Abstract: A radar system and method for obtaining low sum and difference side lobe patterns from a phased array antenna comprising radiators distributed amongst four quadrants A, B, C, and D. The quadrants are arranged in a clockwise order of A, B, D, and C. Each quadrant is further divided into an inner portion and an outer portion. The monopulse sum pattern is determined by adding signals received by radiators in the A quadrant, B quadrant, C quadrant, and D quadrant. The elevation difference pattern is determined by subtracting a CD sum consisting of signals received by radiators in the C outer portion and the D outer portion from an AB sum consisting of signals received by radiators in the A outer portion and the B outer portion. The azimuth difference pattern is determined by subtracting a BD sum consisting of signals received by radiators in the B outer portion and the D outer portion from an AC sum consisting of signals received by radiators in the A outer portion and the C outer portion.Type: GrantFiled: June 16, 1998Date of Patent: December 21, 1999Assignee: Boeing North American, Inc.Inventor: Sam H. Wong
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Patent number: 5847675Abstract: This radar with a wide instantaneous angular field and a high instantaneous angular resolution, in particular for a missile homing head, includes essentially:a transmitting antenna with a relatively wide radiation pattern, transmitting a quasi-continuous wave;a receiving antenna including a plurality of radiating elements;means for formation of beams associated with said receiving antenna, to achieve a linear combination of the signals from the various radiating elements of said receiving antenna, in order to obtain a group of simultaneous reception beams allowing the instantaneous scanning of the airspace covered by said transmitting antenna.Type: GrantFiled: September 28, 1990Date of Patent: December 8, 1998Inventor: Henri Poinsard
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Patent number: 5831570Abstract: A method and apparatus for improving resolution of targets in a monopulse radar beam.Type: GrantFiled: September 15, 1997Date of Patent: November 3, 1998Assignee: AlliedSignal, Inc.Inventors: Danny F. Ammar, Randall C. Spires, Steven R. Sweet
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Patent number: 5808578Abstract: A method for calibrating the radar system includes the steps of: replacing stored statistically generated "average" error correction coefficients with error correction coefficients personal to a missile under test. More particularly, stored in the missile's memory are: (a) first personalized error correction coefficients generated in response to test signals produced internal to the missile and injected into a monopulse arithmetic unit for the missile's receiver/processor; and (b) a second set of personalized error coefficients generated in response to test signals external to the missile and injected through the missile's antenna to the receiver/processor. The missile includes a radio frequency (R.F.) energy test signal generator for performing a test during the missile's flight to determine "in-flight" personalized error correction coefficients. The test is performed in-flight by injecting the R.F.Type: GrantFiled: December 20, 1996Date of Patent: September 15, 1998Inventors: Peter F. Barbella, Malcolm F. Crawford, William M. Kaupinis, Jeffrey E. Carmella, Michael A. Davis
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Patent number: 5784022Abstract: The process and the corresponding phase or amplitude-single pulse radar device are used to locate a first and possibly a second target (TT1, TT2) detected by the radar beam from the direction x1, y1; x2, y2. The extended single-pulse aerial of the radar device has at least three partial aerials for a first measuring axis x (e.g. azimuth) which are arranged in such a way, have such directional characteristics and the signals of which are combined together and weighted in such a way that two mutually linearly independent, purely real or purely imaginary aerial functions which are independent of target displacements perpendicular to the first measuring axis are formed. The function course of these aerial functions F1(x) and F2(x) is measured for the individual case and the functional values dependent upon the target displacement x are stored in the storage unit (MEM). Measurements are found for the targets of the position x1 and x2 detected by the radar beam according to the aerial functions F1 and F2.Type: GrantFiled: May 2, 1997Date of Patent: July 21, 1998Assignee: Siemens Switzerland AGInventor: Hanspeter Kupfer
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Patent number: 5619206Abstract: A secondary radar uses monopulse reception techniques to improve the estimate of the aircraft position and to improve the reliability of the reply decoding process. Digital signal processing techniques are utilized to replace the analog circuit used in the prior implementations. The secondary radar implements monopulse processing using a half angle phase method wherein the sum and difference signals are encoded in a complete phasor. The detection of the signal and extraction of the azimuth angle data is implemented using a digital receiver concept. The complex phasor is sampled at an intermediate frequency, down converted to baseband and detected. The azimuth angle is computed using arithmetic methods implemented by digital signal processing circuitry.Type: GrantFiled: November 20, 1995Date of Patent: April 8, 1997Assignee: Northrop Grumman Corp.Inventors: Elbert L. Cole, Jr., Richard A. Enstrom, Terence E. Olver
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Patent number: 5506589Abstract: An array system with radiating elements and a wideband monopulse power divider network with dual channel input ports and multiple output ports. Each input channel of the network excites a uniquely different RF amplitude and phase distribution out of each of the corresponding "n" output ports. All ports are matched and isolated from each other across a wide instantaneous frequency. Also the RF power distribution will track in amplitude and phase across a wide frequency band. This is achieved through a special arrangement of air-stripline matched power dividers, attenuator, phase shifters, and Magic-Tee couplers. The output ports of the network can be connected directly to the radiating elements or to partitioned feed circuits which are in turn connected to sub-sets of the radiating elements.Type: GrantFiled: April 19, 1993Date of Patent: April 9, 1996Assignee: Hughes Aircraft CompanyInventors: Clifton Quan, Donald E. Bostrom, Mark Y. Hashimoto, Ruth Dean, deceased, Rosie M. Jorgenson
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Patent number: 5486831Abstract: A multi-mode seeker which comprises a stationary antenna and electronic circuitry responsive to signals received by the antenna to cause the antenna to scan a field of view determined by the signals received by the antenna. The seeker has a nose region positioned at the forward portion thereof and an adjunct sensor disposed in the nose region ahead of the antenna. The electronic circuitry includes circuitry for performing a Sum/Delta monopulse processing technique on the signals received by the antenna the Sum/Delta monopulse processing including calculating each of a standard Sum signal, Delta-Azimuth signal and Delta-Elevation signal. The seeker has a boresight axis, the center of the field of view being off boresight, in general. The seeker has a field of regard, the field of regard having plural sectors, each of the sectors having separate predefined compensation.Type: GrantFiled: April 12, 1995Date of Patent: January 23, 1996Inventors: Landon L. Rowland, Richard K. Lowder, Lester W. Dyer, Charles H. Turner
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Patent number: 5402130Abstract: In a monopulse radar processor, the usual sum (s) and difference (d) signals are manipulated to produce two other signals (s+ad and s+bd, in which a and b are constants). The phase of each of these derived signals with respect to the sum signal is then determined. The real part of d/s and, if desired, the imaginary part of d/s are calculated from these measured phase angles. The real part of d/s is the conventional output from a monopulse processor.Type: GrantFiled: May 28, 1981Date of Patent: March 28, 1995Assignee: Martin Marietta CorporationInventor: Samuel M. Sherman
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Patent number: 5270718Abstract: A method and apparatus to determine angles .theta..sub.1 and .theta..sub.2 between paths of two sets of reflected radar waves and a radar boresight utilizes the electrical angles .beta..sub.1 or .beta..sub.2 and two successive radar target observations. One set of radar waves may travel a path from a target and the second set may travel a multipath from the same target. Alternatively, the two sets of radar waves may follow direct paths from two targets. For coherent radar hardware, signals from two halves of an array are processed through a linear coherent receiver, analog-to-digital converter and processing unit with associated memory. The memory contains a database and program which calculates the electrical angles .beta..sub.1 and .beta..sub.2 and angles .theta..sub.1, and .theta..sub.2. For non-coherent radar hardware, mixers, a phase detector and two magnitude detectors are substituted for the linear coherent receiver.Type: GrantFiled: August 21, 1992Date of Patent: December 14, 1993Assignee: Technology Service CorporationInventor: Richard DiDomizio
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Patent number: 5192955Abstract: A target tracking system and methods that can isolate and maintain stable track on a selected target in multiple-target environment. In multiple-target environments, the signal returns received at the sum and difference channels are composites of individual targets. By decomposing received signals into individual components, angle measurements to each target are computed, and consequently, a specified target is isolated and accurately tracked in a stable manner. The present invention provides for apparatus and methods that compute angle measurements to each individual airborne target in a multiple target environment. The composite return signals from a number of targets that are closely spaced in Doppler are decomposed into their individual components, and hence, tracking measurements to each target are obtained without interference from other targets. The present invention may be used to determine the angular position of individual airborne targets within a multiple target environment.Type: GrantFiled: September 25, 1991Date of Patent: March 9, 1993Assignee: Hughes Aircraft CompanyInventor: Bao N. Hoang
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Patent number: 4837577Abstract: A method of electronically stabilizing a monopulse antenna mounted on a movable body is disclosed. According to the disclosed invention, the monopulse antenna is electronically steered in a fixed direction despite motion of the movable body in relation to that direction. Compensated azimuthal and elevation difference signals are formed by approximately weighting and adding the the uncompensated azimuthal and elevation difference signals formed by the monopulse antenna.Type: GrantFiled: May 16, 1988Date of Patent: June 6, 1989Assignee: Raytheon CompanyInventors: Theadore J. Peregrim, Frank A. Okurowski, Rosario Mangiapane
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Patent number: 4788547Abstract: A static-split tracking radar system with substantially improved performance. The system includes parallel signal processing channels for processing sum and difference signals from a target-seeking aerial array, to produce target tracking signals. Novel means are provided for trimming relative phase and gain of these channels to achieve substantially perfect matching, which gives a receiver stability sufficient for homing head use in a guided missile system. The system also includes a receiver for acquiring a reference frequency signal, the receiver having novel bandwidth adaptation and doppler tracking facilities. Other novel features provide improved clutter rejection and jamming immunity.Type: GrantFiled: October 16, 1973Date of Patent: November 29, 1988Assignee: The Marconi Company LimitedInventors: Michael A. Jones, John R. G. Woods
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Patent number: 4768034Abstract: A radar system for tracking a plurality of individual objects that form a cluster. The system comprises means for producing in real time reference information indicative of the position of a reference point associated with the mean position of the objects, and means for producing in real time displacement information indicative of the relative position of each object with respect to the reference point. The system may handle a transmitter, and the means for producing the displacement information may include a interferometer system comprising a central receiver, a pair of first satellite receivers positioned on opposite sides of the central receiver along a first axis that passes through the central receiver, and a pair of second satellite receivers positioned on opposite sides of the central receiver along a second axis that passes through the central receiver and that is inclined with respect to the first axis.Type: GrantFiled: March 26, 1984Date of Patent: August 30, 1988Inventors: Fritz K. Preikschat, Ekhard Preikschat
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Patent number: 4752779Abstract: A missile guidance system having means for deriving from a target angle tracking loop a signal indicative of an apparent movement of a target off a missile-to-target sight line caused by a change in missile attitude, and means for feeding said apparent movement signal into a space stabilization loop to adjust the position of the aerial to compensate for said apparent movement.Type: GrantFiled: December 20, 1977Date of Patent: June 21, 1988Assignee: The Marconi Company LimitedInventors: Michael A. Jones, Richard H. Campbell, Christopher D. Huggett, Anthony J. Benson, John A. Gurr
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Patent number: 4743907Abstract: A radar system for low-level target tracking comprises a first and a second radar apparatus, both apparatus operating at their own frequency, but employing one and the same tracking antenna. A target being tracked in range and angle coordinates by the first radar apparatus can be tracked in angle coordinates by the second apparatus and in range by the first radar apparatus when the target arrives within the range of the second radar apparatus. A preferred digital embodiment of this system is obtained by utilizing a common signal processing unit including a matched filter.Type: GrantFiled: May 5, 1986Date of Patent: May 10, 1988Assignee: Hollandse Signaalapparaten B.V.Inventor: Bernard Gellekink
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Patent number: 4700193Abstract: A monopulse receiving arrangement is shown to comprise orthogonally polarized and electrically separate monopulse antenna arrays, one such array being made up of juxtaposed slotted waveguides and the other being made up of at least one monopulse array of dipoles printed on a dielectric material.Type: GrantFiled: August 19, 1983Date of Patent: October 13, 1987Assignee: Raytheon CompanyInventors: Norbert Sa, William F. Miccioli, A. Robert Chinchillo, John F. Toth