| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 261 | Tracking radar device | JP4628381 | 1981-03-31 | JPS57161574A | 1982-10-05 | ISHIMARU TADASHI; WATANABE SEINI; ONOKI MAKOTO |
| PURPOSE:To prevent the tracking of the image under a horizontal plane and the tracking of clutters by controlling an antenna in accordance with the movement information of the target position obtained during normal tracking. CONSTITUTION:When the radar device tracks an image while tracking at a low altitude, an antenna 1 directs downward, and the difference between the smoothing depression and elevation angle signal E* which was under reproduction and calculation by a computer 9 in accordance with the movement of the target till then and the current antenna depression and elevation angle signal E increases. Hence it is compared in a comparator 11' in an input switch 10' and when said difference exceeds the predetermined value, a relay 12' is changed over to feed the differential signal epsilonE=E-E* between the smoothing depression and elevation angle signal and the antenna depression and elevation angle signal to an antenna controlling mechanism 5' so that the tracking is continued on the premise that the target flies at the speed and course before the changing over. Thereby, the antenna 1 is prevented from tracking the image appearing under the horizontal plane. | ||||||
| 262 | Tracking system | JP3845381 | 1981-03-17 | JPS57153282A | 1982-09-21 | IKEDA AKIRA |
| PURPOSE:To improve the performance for separation of crossing of plural targets, by using signal intensity besides position information to track targets correlatively. CONSTITUTION:A range R1, an azimuth theta1, and a signal intensity S1 detected by a radar receiver are stored temporarily in a buffer 1. Target data R1, theta1, and S1 stored in the buffer 1 are compared with tracking forecasted data Rp, thetap, and Sp, which are stored in a buffer 6, by correlators 2, 3, and 4 concerning the range, the azimuth, and the signal intensity, respectively; and if the input difference is within an allowable range, data R1, theta1, and S1 stored in the buffer 1 are transferred to a format register 5. The forecasting operation based on correlated target data R1, theta1, and S1 is performed in a forecasting operator 8, and operation results Rp, thetap, and Sp are transferred to a tracking information memory 7 to update forecasted data. | ||||||
| 263 | Tracking ladar | JP7400180 | 1980-06-02 | JPS57568A | 1982-01-05 | HARAYAMA MITSUHARU |
| PURPOSE:To eliminate the need for man to judge side lobe tracking or not by utilizing a nature of a monopulse antenna pattern to prohibit automatically antenna sidelobe tracking. CONSTITUTION:A signal received by a monopulse antenna 1 is inputted to amplitude detectors 4a-4c and phase detectors 5a, 5b through mixers 2a-2c and amplifiers 3a-3c. Outputs from the phase detectors 5a, 5b are inputted to a tracking signal processor 7. Outputs from the amplitude detectors 4a-4c are inputted to an amplitude comparator 9 through weighting circuits 8a, 8b. The amplitude comparator 9, when a sum channel signal is smaller than a difference channel signal, actuates a tracking prohibition controlling circuit 10 to cause a tracking prohibition. | ||||||
| 264 | Radio wave transmitter | JP16988379 | 1979-12-26 | JPS5692480A | 1981-07-27 | SAWADA MICHIHIRO; SUGIE KIYOKAZU |
| PURPOSE:To decrease the function of a tracking radar for Doppler frequency tracking by mixing a Doppler signal for transmission and an incoming signal from the tracking radar and generating a transmission signal having a Doppler frequency. CONSTITUTION:The signal outputted from a frequency memory circuit 3 which stores the incoming radio waves from a tracking radar is inputted to a transmission wave control switch 4. A transmission time is controlled by said switch 4 and the signal is applied to a mixer 10. On the other hand, the output from a Doppler frequency oscillator 9 is applied to the mixer 10. The output of the mixer 10 is transmitted from a transmission antenna 6 through a transmitter 5. | ||||||
| 265 | JPS513636B1 - | JP6978271 | 1971-09-10 | JPS513636B1 | 1976-02-04 | |
| 266 | JPS4874192A - | JP12634072 | 1972-12-18 | JPS4874192A | 1973-10-05 | |
| 267 | DUAL-SIDED RADAR SYSTEMS AND METHODS OF FORMATION THEREOF | EP18198538.3 | 2018-10-04 | EP3467536A2 | 2019-04-10 | Trotta, Saverio; Baheti, Ashutosh; Jungmaier, Reinhard-Wolfgang; Mikolajczak, Adrian |
A radar system includes a substrate that includes a first surface and a second surface. The first surface is opposite the second surface. The radar system further includes transmitter front-end circuitry attached to the substrate and configured to transmit a transmitted radio frequency (RF) signal in a first direction away from the first surface and in a second direction away from the second surface. The radar system also includes a first receive antenna and a second receive antenna. The first receive antenna is disposed at the first surface and is configured to receive a first reflected RF signal propagating in the second direction and generated by the transmitted RF signal. The second receive antenna is disposed at the second surface and is configured to receive a second reflect RF signal propagating in the first direction and generated by the transmitted RF signal.
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| 268 | METHODS AND APPARATUS FOR DETERMINING ANGLE OF ARRIVAL (AOA) IN A RADAR WARNING RECEIVER | EP15742131.4 | 2015-01-15 | EP3123197B1 | 2018-05-02 | GUDIM, Eric, J.; WELLMAN, William, H. |
| Methods and apparatus for determining an angle of arrival in a radar warning system that uses tracking to provide a more accurate angle of arrival than conventional systems. In exemplary embodiments, angle of arrival and range are mapped from measured body angles to a 3D coordinate system where modern tracking techniques are applied to improve accuracy and stabilization of measurements, then mapped back into body angles for display. | ||||||
| 269 | SYSTEM AND METHOD FOR STANDOFF DETECTION OF HUMAN CARRIED EXPLOSIVES | EP05858447.5 | 2005-10-11 | EP1810052B1 | 2018-01-24 | DOUGLASS, Robert J.; GORMAN, John D.; BURNS, Thomas J. |
| The system and method for standoff detection of human carried explosives (HCE) automatically detects HCE (112) up to a range of (200) meters and within seconds alerts an operator to HCE (112) threats. The system (100) has radar only, or both radar and video sensors, a multi-sensor processor (102), an operator console (120), handheld displays (122), and a wideband wireless communications link. The processor (102) receives radar and video feeds and automatically tracks and detects all humans (110) in the field of view. Track data continuously cues the narrow beam radar (118) to a subject of interest (110), (112) the radar (106), (108) repeatedly interrogating cued objects (110), (112), producing a multi-polarity radar range profile for each interrogation event. Range profiles and associated features are automatically fused over time until sufficient evidence is accrued to support a threat/non-threat declaration hypothesis. Once a determination is made, the system (100) alerts operators through a handheld display (122) and mitigates the threat if desired. | ||||||
| 270 | METHOD FOR FOCUSING A HIGH-ENERGY BEAM ON A REFERENCE POINT ON THE SURFACE OF A FLYING OBJECT IN FLIGHT | EP16171803.6 | 2016-05-27 | EP3098561B1 | 2017-12-13 | Schlosser, Wolfgang |
| A method for focusing a beam (30) of a high energy radiation source (3), particularly a laser beam, on a reference point (HP) on the surface of a flying object in flight (1), comprises the following steps: a) Recording a number of consecutive two-dimensional images of the flying object (1) in flight with an imaging method using an image acquisition device (2); b) Determining the trajectory (T) of the flight path of the flying object (1) as a sequence of three-dimensional waypoints; c) Simultaneously determining the line of sight angle between the image acquisition device (2) and the position of the flying object (1) in synchronisation with the image; d) Calculating a three-dimensional model of the flying object (1) from the two-dimensional images recorded in step a) on the basis of the relative geometry to be calculated from the line of sight angles calculated in step c) and the trajectory (T) obtained in step b), and on the basis of predefined model assumptions about the flying object (1); e) Displaying the currently acquired two-dimensional image (1') of the flying object (1) in flight via an image reproduction device (4); f) Marking the reference point (HP') on the displayed two-dimensional image (1') of the flying object (1); g) Calculating the three-dimensional reference point (HP) on the surface of the flying object (1) starting from the two-dimensional reference point (HP') marked in step f) using the three-dimensional model of the flying object (1) calculated in step d), and h) Focusing the beam (30) of the high energy radiation source (3) on the three-dimensional reference point (HP) and causing the focus point of the beam (30) directed at the reference point (HP) to track said reference point (HP). | ||||||
| 271 | An apparatus for estimating the height at which a target flies over a reflective surface | EP08172016.1 | 2008-12-17 | EP2199825B1 | 2017-05-17 | Driessen, Hans; Podt, Martin |
| 272 | Application agnostic sensor, control computer and methods for operating | EP14161623.5 | 2014-03-25 | EP2923642B1 | 2017-03-15 | Scholten, Ulrich; Moskwa, Eric |
| A multi-application-transceiver device (100), control computer, computer implemented method and computer program product for operating the multi-application-transceiver device is disclosed. At least one signal transceiver (110) receives a reflected signal (S2) in response to an original signal (S1) sent by the at least one signal transceiver (110). The reflected signal (S2) is reflected from at least one target object (1). A signal conversion unit (150) converts the reflected signal (S2) into digital format. A digital signal processor component (120) pre-processes the converted reflected signal using an alterable rule engine (121) with a received rule set to discriminate a state in change of the at least one target object (1) against an earlier state of the at least one target object (1) in the context of a particular monitoring application. A middleware component (130) communicates with at least one remote computing device (300) wherein communicate includes to send the pre-processed signal to the remote computing device (300), and to receive from the at least one remote computing device (300) the rule set for the alterable rule engine (121). The received rule set defines an application specific setting for the at least one signal transceiver (110) and for the digital signal processor component (120) to enable the particular monitoring application. | ||||||
| 273 | VERFAHREN ZUR AUTOMATISCHEN KLASSIFIKATION VON RADAROBJEKTEN | EP16001346.2 | 2016-06-15 | EP3112894A1 | 2017-01-04 | Neumann, Christoph; Senkowski, Hermine |
Die Erfindung betrifft ein Verfahren zur Klassifikation von Radarobjekten, wobei |
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| 274 | Photonic-assisted digital radar system | EP12164336.5 | 2012-04-16 | EP2511731B1 | 2016-11-30 | Pierno, Luigi; Dispenza, Massimiliano; Gatta, Alessandro; Fiorello, Annamaria; Secchi, Alberto; Ricci, Massimo |
| 275 | ON-BOARD RADAR APPARATUS AND REGION DETECTION METHOD | EP15196636.3 | 2015-11-27 | EP3032273A1 | 2016-06-15 | HAMADA, Asako; NISHIMURA, Hirofumi; KOBAYASHI, Kiyotaka; SHIKATANI, Maiko |
An on-board radar apparatus includes a transmitter/receiver that transmits a radar signal to a detection range every frame and receives one or more reflected signals which are the radar signal reflected by one or more objects; a detector that detects, every frame in each direction within the detection range, a position of a reflection point closest to the on-board radar apparatus as a boundary candidate position, which serves as a boundary with a region where no object exists within the detection range, among one or more reflection points detected on the basis of the one or more reflected signals; a calculator that calculates movement amount concerning an amount of movement of the on-board radar apparatus; an estimator that generates, every frame in each direction within the detection range, an estimated boundary position by converting the boundary candidate position detected in a past frame into a boundary position in a current frame on the basis of the movement amount; and a smoother that performs, every frame in each direction within the detection range, smoothing processing by using the boundary candidate position in the current frame and the estimated boundary position to calculate a boundary position with the region where no object exists within the detection range and outputs the calculated the boundary position to a driving support apparatus.
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| 276 | Method and distributed system for flying objects tracking using consumer electronics devices | EP13197043.6 | 2013-12-13 | EP2884298A1 | 2015-06-17 | Micewicz, Jaroslaw; Bordych, Maciej |
A consumer electronics terminal for use in a distributed system for flying objects tracking, the terminal comprising: a location determination signal receiver; a controller; a memory; and a data transmitter, the terminal further comprising: the controller being configured to receive data from the location determination signal receiver and to communicate, using the data transmitter information regarding change of signal strength of a given available at least one satellite to at least one server. The invention also concerns a radar facility for flying objects tracking using consumer electronics devices, the radar facility comprising: a database configured to store information received from a plurality of consumer electronics terminals according to the invention; a data processor configured to filter the data stored in the database according to rules stored in a rules database; the data processor being further configured to recognize, based on the filtered data, coherent changes in time denoting a route of a flying object.
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| 277 | CODED APERTURE BEAM ANALYSIS METHOD AND APPARATUS | EP12872244.4 | 2012-12-21 | EP2798370A2 | 2014-11-05 | LYNCH, Jonathan J. |
| A method and apparatus for determining the range, radial velocity, and bearing angles of scattering objects reflecting RF signals or for determining the range, radial velocity, and bearing angles of sources RF signals. An array of antenna elements is utilized, the array of antenna elements each having an associated two state modulator wherein transmitted and/or received energy is phase encoded according to a sequence of multibit codes, the bits of the multibit codes each preferably having two states with approximately a 50% probability for each of the two states occurring within each given multibit code in said sequence of multibit codes, thereby allowing the determination of range, radial velocity, and bearing angles through digital computation after the scattered signals have been received. | ||||||
| 278 | RADAR DEVICE | EP12761206.7 | 2012-03-12 | EP2690458A1 | 2014-01-29 | ITOHARA, Hiroyuki; AOYAGI, Yasushi |
A radar device capable of reducing load of a clustering process and improving the tracking performance is provided. A tracking calculation unit 116 of a radar device 100 performs a clustering process, in which an input detected data set is grouped into clusters, and a tracking process, in which an averaged value and a prediction value are calculated for each of the clusters. In the radar device 100, the shape of cluster areas for grouping the detected data is defined to be a fan shape. The clustering process and tracking process using fan-shaped cluster areas can reduce the load of the clustering process and improve the tracking performance. |
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| 279 | Fast ray trace to identify radar multipaths | EP12166395.9 | 2012-05-02 | EP2544021A1 | 2013-01-09 | Valentine, Mark L. |
A method of detecting a target in a room using a radar system having a transmitter for irradiating the object, a sensor for receiving reflected radiation, and circuitry for analyzing the reflected radiation to determine at least one characteristic thereof, the method including determining at least one parameter for each wall of a plurality of walls of a room containing the target; determining possible signal paths between the target and the sensor for paths including up to N reflections based on the at least one parameter of each wall and the location of the sensor; calculating target image locations based on the possible signal paths; and processing the received radiation to determine a target location based on target image locations.
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| 280 | PROCEDE D'ESTIMATION DU SITE D'UN PROJECTILE BALISTIQUE | EP07847610.8 | 2007-11-30 | EP2092366B1 | 2012-06-27 | DURAND, Bernard; CAVALLERI, Christian; ADRIAN, Odile |
| The present invention relates to the implementation of a method making it possible to determine in an accurate manner, the elevation of a projectile along a ballistic trajectory by means of the information provided by a conventional Doppler surveillance radar. The method according to the invention consists, on the basis of the quantities (A) and (B) representing respectively the first derivative and the second derivative with respect to time of the Doppler speed d of the projectile, in calculating firstly the estimate (C) of the value of the radial component Γρ of the acceleration of the projectile, then in calculating on the basis of d, (A) and (C) the estimate (D) of the speed V of the projectile, then finally in calculating on the basis of d and (D) the estimate Ê of its angle of elevation E. The method according to the invention applies in particular to the protecting of sensitive zones from the firing of ballistic projectiles. | ||||||
