US20030048214A1 - Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming - Google Patents
Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming Download PDFInfo
- Publication number
- US20030048214A1 US20030048214A1 US09/948,959 US94895901A US2003048214A1 US 20030048214 A1 US20030048214 A1 US 20030048214A1 US 94895901 A US94895901 A US 94895901A US 2003048214 A1 US2003048214 A1 US 2003048214A1
- Authority
- US
- United States
- Prior art keywords
- accordance
- echo signal
- hrr
- target
- waveform
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/42—Simultaneous measurement of distance and other co-ordinates
- G01S13/426—Scanning radar, e.g. 3D radar
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/003—Bistatic radar systems; Multistatic radar systems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/08—Systems for measuring distance only
- G01S13/10—Systems for measuring distance only using transmission of interrupted, pulse modulated waves
- G01S13/26—Systems for measuring distance only using transmission of interrupted, pulse modulated waves wherein the transmitted pulses use a frequency- or phase-modulated carrier wave
- G01S13/28—Systems for measuring distance only using transmission of interrupted, pulse modulated waves wherein the transmitted pulses use a frequency- or phase-modulated carrier wave with time compression of received pulses
- G01S13/282—Systems for measuring distance only using transmission of interrupted, pulse modulated waves wherein the transmitted pulses use a frequency- or phase-modulated carrier wave with time compression of received pulses using a frequency modulated carrier wave
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/08—Systems for measuring distance only
- G01S13/32—Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/28—Details of pulse systems
- G01S7/2813—Means providing a modification of the radiation pattern for cancelling noise, clutter or interfering signals, e.g. side lobe suppression, side lobe blanking, null-steering arrays
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/36—Means for anti-jamming, e.g. ECCM, i.e. electronic counter-counter measures
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/41—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00 using analysis of echo signal for target characterisation; Target signature; Target cross-section
- G01S7/411—Identification of targets based on measurements of radar reflectivity
Definitions
- the present invention relates generally to radar processing and more specifically, to a radar process and system for creating and maintaining the quality of a high resolution range profile for a target in the presence of jamming.
- Modern radar systems having high resolution capability are useful in many situations, such as target detection, target discrimination, target recognition, and terrain imaging.
- Such radar systems are frequency agile and operate at rapidly varying frequencies.
- These radar systems are vulnerable to diverse threats such as intentional jamming, spoofing, and radar frequency interference (RFI).
- RFID radar frequency interference
- the target platform may also comprise countermeasures such as jamming and chaff.
- HRR high range resolution
- jamming is in the form of a high power transmission designed to impair a radar system's performance.
- Jamming may comprise a signal modulated with noise or other disruptive information.
- the object of typical jammers is to impair the performance of a radar system's receiving electronics and/or obscure display of potential targets of interest.
- the source of jamming interference may be mobile or may be relatively stationary (e.g., land based systems).
- HRR processing is vulnerable to interference due to jamming because it requires a relatively wide operational bandwidth, thus increasing the chances that a jammer at a particular frequency will be in the operational bandwidth.
- HRR processing is also vulnerable to jamming interference because of the relatively long coherent integration time associated with HRR processing. This increases the likelihood that a jammer will transmit while the HRR echoes are being received. Therefore, to avoid performance degradation due to jamming interference, it is desirable to eliminate jamming interference from the received signal (e.g., via cancellation, attenuation).
- Jamming interference is typically cancelled by adaptively forming beam patterns, wherein nulls of the beam patterns are steered in the direction of the source(s) of jamming interference.
- Many existing adaptive techniques require a training period in which a signal is not present (such as during a passive listening period), or a period in which the signal value is low compared to jamming interference (such as in a search radar system) in order to distinguish signal energy from jammer energy.
- signal content is available in all frequency samples.
- conventional adaptive techniques may cancel desired signal content in addition to canceling jamming interference.
- conventional adaptive techniques tend to modulate the signal of interest, causing degradation in sidelobe performance, as a result of changing adaptive weight values. Thus, conventional adaptive techniques may degrade the image quality of an HRR profile.
- a system and method for creating a high resolution range (HRR) profile for a radar target of interest in the presence of jamming interference include transmitting an HRR waveform and receiving an echo signal resulting from the transmitted HRR waveform. Beam patterns are formed for each echo signal segment of the echo signal such that at least one null of each beam pattern is steered toward at least one interference and a frequency dependent gain of each beam pattern is maintained toward the center of the target of interest.
- the HRR profile is created from the beam patterns.
- FIG. 1A is a graph of an exemplary relationship between time and frequency of a chirp waveform, in accordance with an embodiment of the present invention
- FIG. 1B is a diagram of an envelope of an exemplary stepped frequency waveform 36 in accordance with an embodiment of the present invention.
- FIG. 2 is a functional block diagram of an exemplary HRR processing system in accordance with an embodiment of the present invention
- FIG. 3 is a flow diagram of an exemplary process for creating an HRR profile in accordance with an embodiment of the present invention.
- FIG. 4 is a block diagram of a radar system comprising an antenna array 60 and computer processor 62 in accordance with an exemplary embodiment of the invention.
- HRR High range resolution
- One means for accomplishing this objective is to transmit an HRR waveform, which provides the desired average power (thus providing desired detection range) and decoding the received echoes resulting from the HRR waveform(s) via pulse compression, and performing a weighted inverse fast Fourier Transform (FFT).
- FFT weighted inverse fast Fourier Transform
- An HRR waveform may comprise a continuous LFM (linear frequency modulated) chirp waveform or a stepped frequency waveform (pulses of energy).
- FIG. 1A is a graph of an exemplary relationship between time and frequency of a chirp waveform, in accordance with an embodiment of the present invention.
- a chirp waveform is a waveform wherein the frequency of the waveform is either increased or decreased at a constant rate with respect to time.
- Curve 34 indicates the frequency of an exemplary chirp waveform as a function of time. Curve 34 is monotonically increasing, although in another embodiment of the invention, curve 34 is monotonically decreasing. Curve 34 is depicted as a straight line, indicating a linear relationship between the frequency and time of the generated waveform.
- a linear HRR waveform is described herein, a nonlinear HRR waveform, such a parabolic HRR waveform, is also envisioned.
- FIG. 1B is a diagram of an envelope of an exemplary stepped frequency waveform 36 in accordance with an embodiment of the present invention.
- Waveform 36 comprises a plurality of waveform segments 35 each having a different frequency, f 1 through f N-1 .
- Frequencies f 0 through f N-1 may increase or decrease with respect to time.
- the duration, in time, of each waveform segment is denoted as T 1 through T N , respectively. In an exemplary embodiment of the invention, durations T 1 through T N are equal.
- the separation between waveform segments 35 is ⁇ f. In an exemplary embodiment of the invention, ⁇ f is the same between all segments 35 of waveform 36 .
- Pulse compression comprises a delay line or filter (or similar means), that introduces a time delay into a signal.
- the time delay is inversely proportional to the frequency of the signal.
- the introduced time delay decreases with frequency at the same rate as the frequency of the echoes increases. For example, referring to FIG. 1B, if f 0 is the highest frequency and f N-1 is the lowest frequency, f 1 will take less time to pass through the pulse compressor than f N-1 .
- echoes resulting from each segment 35 of a transmitted HRR waveform will be delayed in the same manner. The result is that all frequencies are aligned at the output of the pulse compressor to the same time.
- the information contained in each echo resulting from each transmitted waveform segment 35 are superimposed upon one another.
- echoes from closely spaced targets are merged in the received echo resulting from the HRR waveform, but are separate at the output of the pulse compressor.
- FIG. 2 is a functional block diagram of an exemplary HRR processing system 200 in accordance with an embodiment of the present invention.
- antenna 12 is an antenna array.
- Transmitter 14 receives a modulated center frequency from waveform generator/oscillator 20 .
- Waveform generator/oscillator 20 is a frequency agile oscillator, thus being capable of changing frequencies rapidly.
- Transmitter 14 is a radar transmitter of any appropriate type well known in the art.
- Waveform generator 20 generates HRR waveforms used to create a HRR profile in accordance with the present invention.
- the waveforms generated by waveform generator 20 comprise chirp waveforms and/or stepped frequency waveforms.
- Waveform generator 20 may also generate the waveform(s) used for detecting radar targets of interest. Waveforms may include LFM and stepped frequency waveforms.
- Antenna 12 transmits radar signals 13 and receives reflected radar signals 15 (echoes), and provides signals 17 corresponding to these echoes to dechirper 16 .
- Dechirper 16 dechirps the received echo signal. Dechirping comprises multiplying the chirped signal by a signal provided by the waveform generator/oscillator 20 having the same slope as the chirped signal. Dechirping produces a baseband signal, which is provided to digital beamformer 18 .
- Adaptive digital beamformer 18 is a frequency dependent beamformer. Beam patterns are formed for each received echo from each segment of the transmitted HRR waveform in beamformer 18 . In an exemplary embodiment of the invention, beams are adaptively formed in adaptive digital beamformer 18 .
- Beamformer 18 provides beamformed signals 19 to range bin selector 22 .
- a target tracker operates in conjunction with HRR processing system 200 (tracker not shown in FIG. 2).
- the tracker updates information pertaining to the location of a target of interest (e.g., updates estimated angle of arrival and estimation range).
- Tracker information 25 is provided to range bin selector 22 to determine the target center, and the resultant signal 23 is provided to pulse compressor 24 .
- the resultant signal is pulse compressed by pulse compressor 24 using the same type of waveform that was used to generate the HRR waveform (i.e., LFM or stepped frequency waveform).
- Pulse compression comprises a matched filtering process, wherein the provided signal is convolved with a replica of the HRR waveform.
- the compressed signal 31 is motion compensated and then provided to an inverse FFT processor 32 to create an HRR profile.
- Quadratic phase motion compensation comprises multiplying the phase component of the compressed signal 31 by its complex conjugate to remove higher order (quadratic) terms, which are related to velocity. If this term is not removed, the HRR profile image may comprise modulation distortion.
- the quadratic phase motion compensated signal is
- a target of interest is detected and tracked using conventional narrowband waveforms.
- These narrowband waveforms may include CW and/or FM (linear and nonlinear) waveforms.
- Target tracking comprises updating and maintaining positional information pertaining to a target of interest (e.g., estimated arrival angel, estimated range).
- HRR processing is commenced.
- HRR processing in accordance with an exemplary embodiment of the invention, comprises transmitting an HRR waveform, receiving echo signals resulting from the transmitted HRR waveform, adaptively beamforming segments of the received echo signals to produce beamformed data, performing pulse compression on the beamformed data, performing quadratic phase motion compensation on the compressed data, providing the compensated compressed signal to an inverse FFT processor for producing an HRR profile (image).
- FIG. 3 is a flow diagram of an exemplary process for creating an HRR profile in accordance with an embodiment of the present invention.
- a target of interest is detected in step 40 and tracked in step 42 .
- This detection and tracking may comprise any means known in the art.
- HRR processing in accordance with the present invention may be accomplished independent of the detection and tracking of the target of interest. However, the quality of the HRR profile may be improved if motion compensation is performed in accordance with information provided by the tracker.
- the HRR waveform is transmitted in step 44 .
- the HRR waveform may comprise an FM chirp waveform and/or a stepped frequency waveform.
- Echoes resulting from the interaction of the transmitted HRR waveform and objects including the target(s) of interest, ground clutter, targets not of interest, and other objects, are received in step 46 .
- the chirped received echo signal is dechirped in step 47 using an LFM dechirping waveform having the same slope as the transmitted chirped signal.
- Beamforming is performed in step 48 .
- beamforming is performed adaptively.
- Each echo signal corresponding to each segment 35 of the transmitted HRR waveform is beamformed. That is, a beam pattern is formed for each received echo signal corresponding to each segment 35 , and weights are calculated for each beam pattern. If the transmitted HRR waveform is a chirp waveform, the received echo is separated into segments and beamforming is performed for each segment.
- HRR processing is vulnerable to interference due to jamming because it requires a relatively wide operational bandwidth. This increases the chances that a jammer at a particular frequency will be in the operational bandwidth. HRR processing is also vulnerable to jamming interference because of the relatively long coherent integration time associated with HRR processing, thus increasing the likelihood that a jammer will transmit while the HRR echoes are being received. Therefore, it is generally desirable to eliminate jamming interference from the received signal (e.g., via cancellation or attenuating) in order to avoid performance degradation. Jamming interference may be canceled adaptively or manually.
- jamming interference is cancelled adaptively by forming beam patterns, wherein nulls of the beam patterns are steered in the direction of the source(s) of jamming interference.
- Many existing adaptive techniques require a training period where no signal is present (such as during a passive listening period), or a period where the signal value is low compared to the jamming interference signal (such as in a search radar system) in order to distinguish signal energy from jammer energy.
- signal content is available in substantially all frequency samples.
- conventional adaptive techniques may cancel desired signal in addition to canceling jamming interference.
- conventional adaptive techniques tend to modulate the signal of interest, causing degradation in sidelobe performance as a result of changing adaptive weight values.
- An HRR process in accordance with the present invention tends to overcome these problems by tracking the target center, with respect to range, for each pulse and constrain the adaptive processing such that the frequency dependent gain is maintained toward the target center for each adaptive processing block.
- beams are formed with respect to the target center in accordance with information provided by the tracker.
- Weights are adaptively calculated for each received echo signal corresponding to each waveform segment 35 (see FIG. 1B) of the transmitted HRR waveform, and the weights are calculated to steer at least one null toward an interference, and within the constraints that frequency dependent gain is maintained toward the target center.
- the frequency measurement for each range bin of the received echo is in accordance with the following equation.
- r i is the vector of the array (or sub-array) measurement for the selected range bin of the i th pulse
- g SA is the array (or sub-array) gain vector at frequency f i and steering direction (T x , T y )
- J i and n i are the jamming interference and noise component, respectively
- c is the speed of light in a in the transmission medium
- R k is the position of the k th scattering center
- T x is the azimuth directional cosine
- T y is the elevation directional cosine calculated in accordance with the following equations.
- ⁇ is the steering angle, in azimuth, off boresight of the antenna array
- ⁇ is the steering angle, in elevation, off boresight of the antenna array
- W i C i - 1 ⁇ g S ⁇ ⁇ A ⁇ ( T x S , T y S , f i ) g S ⁇ ⁇ A ⁇ ( T x S , T y S , f i ) H ⁇ C i - 1 ⁇ g S ⁇ ⁇ A ⁇ ( T x S , T y S , f i ) ⁇ g ⁇ ⁇ ( T x S , T y S , f i ) , ( 4 )
- the index i indicates the number of processing blocks into which the received echoes are separated for processing
- C i is the covariance matrix estimate of the i th processing block
- W i is the adaptive weight of the i th block
- g SA (T x , T y , f i ) is the array (or sub-array) gain vector used as the steering vector
- H indicates the complex conjugate transpose
- g ⁇ (T x S , T y S , f i ) is the sum beam gain (tapered beam pattern steered toward the target) at frequency f i and steering direction (T x S , T y S )
- the superscript S indicates the steering direction toward the target center, which is constant for each processing block.
- a sum beam is typically the weighted sum of the sub-array measurements.
- Sum beam antenna patterns usually peak at the desired signal direction and have low sidelobes. Accordingly, a desired sum beam gain is achieved and maintained towards the target reference for all pulses while jamming is cancelled. In this manner, the image or HRR profile quality is maintained with low range sidelobes and can be used for target discrimination or recognition applications.
- pulse compression is then performed on the beamformed data at step 50 .
- the selection of the bin representing the target center is determined in accordance with target range information provided by the tracker. This is followed by pulse compression and quadratic phase motion compensation. This information aids in compensating for target motion.
- Target motion compensation improves the quality of the HRR profile (image) by reducing quadratic phase error.
- Stretched, inverse FFT processing is performed on the quadratic phase motion compensated data at step 52 .
- Weighted tapering is optional, however weighted tapering processing may enhance the quality of the HRR profile.
- Processing a wideband signal using narrowband techniques e.g., dechirping with a linear frequency modulated waveform followed by a bandpass filter
- Stretch processing is described in a document entitled “Nulling Over Extremely Wide Bandwidths When Using Stretch Processing”, proceedings of Adaptive Sensor Array Processing (ASAP), March 1999, which is hereby incorporated by reference in its entirety.
- Stretch processing is a process, which enables processing of wideband waveforms (e.g., HRR waveforms) with narrowband processing techniques.
- Stretch processing comprises converting pulse delay time, in range, to frequency.
- the received energy from any one range has a constant frequency, and the received energy from different ranges may be separated by well know narrowband processing techniques, such as narrowband filtering with a plurality of narrowband filters via a Fast Fourier Transform (FFT).
- FFT Fast Fourier Transform
- targets which are relatively closely spaced in range, are distinguishable in the HRR profile.
- the pulse compressed, weighted, tapered, inverse FFT signals are formed into images in step 54 .
- the present invention may be embodied in the form of computer-implemented processes and apparatus for practicing those processes.
- the present invention may also be embodied in the form of computer program code embodied in tangible media, such as floppy diskettes, read only memories (ROMs), CD-ROMs, hard drives, high density disk, or any other computer-readable storage medium, wherein, when the computer program code is loaded into and executed by computer processor 32 , the computer processor 32 becomes an apparatus for practicing the invention.
- the present invention may also be embodied in the form of computer program code, for example, whether stored in a storage medium, loaded into and/or executed by computer processor 32 , or transmitted over some transmission medium, such as over electrical wiring or cabling, through fiber optics, or via electromagnetic radiation, wherein, when the computer program code is loaded into and executed by computer processor 32 , the computer processor 32 becomes an apparatus for practicing the invention.
- the computer program code segments configure the processor to create specific logic circuits.
- FIG. 4 is a block diagram of a radar system comprising an antenna array 60 and computer processor 62 in accordance with an exemplary embodiment of the invention.
- HRR waveforms are created by processor 62 and provided to antenna array 60 .
- HRR waveforms are transmitted by antenna array 60 .
- Reflected energy resulting for the transmission of the HRR waveforms is received by antenna array 60 and is provided to computer processor 62 .
- Computer processor 62 performs processes for forming beam patterns, performing pulse compression, performing stretch processing, and generating images in accordance with the present invention, as herein described. Processing may also be performed by special purpose hardware.
- the present invention may be embodied in the form of computer-implemented processes and apparatus for practicing those processes.
- the present invention may also be embodied in the form of computer program code embodied in tangible media, such as floppy diskettes, read only memories (ROMs), CD-ROMs, hard drives, high density disk, or any other computer-readable storage medium, wherein, when the computer program code is loaded into and executed by computer processor 62 , the computer processor 62 becomes an apparatus for practicing the invention.
- the present invention may also be embodied in the form of computer program code, for example, whether stored in a storage medium, loaded into and/or executed by computer processor 62 , or transmitted over some transmission medium, such as over electrical wiring or cabling, through fiber optics, or via electromagnetic radiation, wherein, when the computer program code is loaded into and executed by computer processor 62 , the computer processor 62 becomes an apparatus for practicing the invention.
- the computer program code segments configure the processor to create specific logic circuits.
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Description
- The present invention relates generally to radar processing and more specifically, to a radar process and system for creating and maintaining the quality of a high resolution range profile for a target in the presence of jamming.
- Modern radar systems having high resolution capability are useful in many situations, such as target detection, target discrimination, target recognition, and terrain imaging. Such radar systems are frequency agile and operate at rapidly varying frequencies. These radar systems are vulnerable to diverse threats such as intentional jamming, spoofing, and radar frequency interference (RFI). Also, in air and missile defense applications, the target platform may also comprise countermeasures such as jamming and chaff.
- Of particular interest are systems having high resolution in range. The performance of high range resolution (HRR) systems is degraded in the presence of jamming interference. Typically, jamming is in the form of a high power transmission designed to impair a radar system's performance. Jamming may comprise a signal modulated with noise or other disruptive information. The object of typical jammers is to impair the performance of a radar system's receiving electronics and/or obscure display of potential targets of interest. The source of jamming interference may be mobile or may be relatively stationary (e.g., land based systems). HRR processing is vulnerable to interference due to jamming because it requires a relatively wide operational bandwidth, thus increasing the chances that a jammer at a particular frequency will be in the operational bandwidth. HRR processing is also vulnerable to jamming interference because of the relatively long coherent integration time associated with HRR processing. This increases the likelihood that a jammer will transmit while the HRR echoes are being received. Therefore, to avoid performance degradation due to jamming interference, it is desirable to eliminate jamming interference from the received signal (e.g., via cancellation, attenuation).
- Jamming interference is typically cancelled by adaptively forming beam patterns, wherein nulls of the beam patterns are steered in the direction of the source(s) of jamming interference. Many existing adaptive techniques require a training period in which a signal is not present (such as during a passive listening period), or a period in which the signal value is low compared to jamming interference (such as in a search radar system) in order to distinguish signal energy from jammer energy. However, during HRR processing, signal content is available in all frequency samples. Thus, conventional adaptive techniques may cancel desired signal content in addition to canceling jamming interference. Also, conventional adaptive techniques tend to modulate the signal of interest, causing degradation in sidelobe performance, as a result of changing adaptive weight values. Thus, conventional adaptive techniques may degrade the image quality of an HRR profile.
- Wideband jamming cancellation, in conjunction with stretch processing, was introduced in a document entitled “Nulling Over Extremely Wide Bandwidths When Using Stretch Processing”, proceedings of Adaptive Sensor Array Processing (ASAP), March 1999. The technique introduced in that document processed a wideband signal as a sequence of narrowband signals. However, this technique does not address the signal cancellation or the adaptive weight modulation problems described above. Thus a need exists for an HRR process that can create an HRR profile and maintain the quality of the profile in the presence of countermeasures.
- A system and method for creating a high resolution range (HRR) profile for a radar target of interest in the presence of jamming interference include transmitting an HRR waveform and receiving an echo signal resulting from the transmitted HRR waveform. Beam patterns are formed for each echo signal segment of the echo signal such that at least one null of each beam pattern is steered toward at least one interference and a frequency dependent gain of each beam pattern is maintained toward the center of the target of interest. The HRR profile is created from the beam patterns.
- The foregoing and other objects, aspects and advantages will be better understood from the following detailed description of a preferred embodiment of the invention with reference to the drawings, in which:
- FIG. 1A is a graph of an exemplary relationship between time and frequency of a chirp waveform, in accordance with an embodiment of the present invention;
- FIG. 1B is a diagram of an envelope of an exemplary
stepped frequency waveform 36 in accordance with an embodiment of the present invention; - FIG. 2 is a functional block diagram of an exemplary HRR processing system in accordance with an embodiment of the present invention;
- FIG. 3 is a flow diagram of an exemplary process for creating an HRR profile in accordance with an embodiment of the present invention; and
- FIG. 4 is a block diagram of a radar system comprising an
antenna array 60 andcomputer processor 62 in accordance with an exemplary embodiment of the invention. - It is an object of many radar systems to obtain long detection range and fine range resolution. High range resolution (HRR) processing is advantageous, inter alia, to distinguish targets that are relatively close together, to create detail target images, to aid in target recognition, and to form detailed ground images. One means for accomplishing this objective is to transmit an HRR waveform, which provides the desired average power (thus providing desired detection range) and decoding the received echoes resulting from the HRR waveform(s) via pulse compression, and performing a weighted inverse fast Fourier Transform (FFT).
- An HRR waveform may comprise a continuous LFM (linear frequency modulated) chirp waveform or a stepped frequency waveform (pulses of energy). FIG. 1A is a graph of an exemplary relationship between time and frequency of a chirp waveform, in accordance with an embodiment of the present invention. A chirp waveform is a waveform wherein the frequency of the waveform is either increased or decreased at a constant rate with respect to time.
Curve 34 indicates the frequency of an exemplary chirp waveform as a function of time.Curve 34 is monotonically increasing, although in another embodiment of the invention,curve 34 is monotonically decreasing.Curve 34 is depicted as a straight line, indicating a linear relationship between the frequency and time of the generated waveform. Although a linear HRR waveform is described herein, a nonlinear HRR waveform, such a parabolic HRR waveform, is also envisioned. - FIG. 1B is a diagram of an envelope of an exemplary
stepped frequency waveform 36 in accordance with an embodiment of the present invention.Waveform 36 comprises a plurality ofwaveform segments 35 each having a different frequency, f1 through fN-1. Frequencies f0 through fN-1 may increase or decrease with respect to time. The duration, in time, of each waveform segment is denoted as T1 through TN, respectively. In an exemplary embodiment of the invention, durations T1 through TN are equal. The separation betweenwaveform segments 35 is Δf. In an exemplary embodiment of the invention, Δf is the same between allsegments 35 ofwaveform 36. - Pulse compression comprises a delay line or filter (or similar means), that introduces a time delay into a signal. The time delay is inversely proportional to the frequency of the signal. Thus, the introduced time delay decreases with frequency at the same rate as the frequency of the echoes increases. For example, referring to FIG. 1B, if f0 is the highest frequency and fN-1 is the lowest frequency, f1 will take less time to pass through the pulse compressor than fN-1. Also, echoes resulting from each
segment 35 of a transmitted HRR waveform will be delayed in the same manner. The result is that all frequencies are aligned at the output of the pulse compressor to the same time. Thus, the information contained in each echo resulting from each transmittedwaveform segment 35 are superimposed upon one another. Thus, echoes from closely spaced targets are merged in the received echo resulting from the HRR waveform, but are separate at the output of the pulse compressor. - FIG. 2 is a functional block diagram of an exemplary
HRR processing system 200 in accordance with an embodiment of the present invention. In an exemplary embodiment of theinvention antenna 12 is an antenna array.Transmitter 14 receives a modulated center frequency from waveform generator/oscillator 20. Waveform generator/oscillator 20 is a frequency agile oscillator, thus being capable of changing frequencies rapidly.Transmitter 14 is a radar transmitter of any appropriate type well known in the art.Waveform generator 20 generates HRR waveforms used to create a HRR profile in accordance with the present invention. In an exemplary embodiment of the invention, the waveforms generated bywaveform generator 20 comprise chirp waveforms and/or stepped frequency waveforms.Waveform generator 20 may also generate the waveform(s) used for detecting radar targets of interest. Waveforms may include LFM and stepped frequency waveforms. -
Antenna 12 transmits radar signals 13 and receives reflected radar signals 15 (echoes), and providessignals 17 corresponding to these echoes todechirper 16.Dechirper 16 dechirps the received echo signal. Dechirping comprises multiplying the chirped signal by a signal provided by the waveform generator/oscillator 20 having the same slope as the chirped signal. Dechirping produces a baseband signal, which is provided todigital beamformer 18. Adaptive digital beamformer 18 (ADBF) is a frequency dependent beamformer. Beam patterns are formed for each received echo from each segment of the transmitted HRR waveform inbeamformer 18. In an exemplary embodiment of the invention, beams are adaptively formed in adaptivedigital beamformer 18.Beamformer 18 providesbeamformed signals 19 to rangebin selector 22. In an exemplary embodiment of the invention, a target tracker operates in conjunction with HRR processing system 200 (tracker not shown in FIG. 2). The tracker updates information pertaining to the location of a target of interest (e.g., updates estimated angle of arrival and estimation range). Tracker information 25 is provided to rangebin selector 22 to determine the target center, and theresultant signal 23 is provided topulse compressor 24. The resultant signal is pulse compressed bypulse compressor 24 using the same type of waveform that was used to generate the HRR waveform (i.e., LFM or stepped frequency waveform). Pulse compression comprises a matched filtering process, wherein the provided signal is convolved with a replica of the HRR waveform. - The compressed
signal 31 is motion compensated and then provided to aninverse FFT processor 32 to create an HRR profile. Quadratic phase motion compensation comprises multiplying the phase component of thecompressed signal 31 by its complex conjugate to remove higher order (quadratic) terms, which are related to velocity. If this term is not removed, the HRR profile image may comprise modulation distortion. The quadratic phase motion compensated signal is - In operation, a target of interest is detected and tracked using conventional narrowband waveforms. These narrowband waveforms may include CW and/or FM (linear and nonlinear) waveforms. Target tracking comprises updating and maintaining positional information pertaining to a target of interest (e.g., estimated arrival angel, estimated range). In an exemplary embodiment of the invention, once target tracking is commenced, HRR processing is commenced. HRR processing, in accordance with an exemplary embodiment of the invention, comprises transmitting an HRR waveform, receiving echo signals resulting from the transmitted HRR waveform, adaptively beamforming segments of the received echo signals to produce beamformed data, performing pulse compression on the beamformed data, performing quadratic phase motion compensation on the compressed data, providing the compensated compressed signal to an inverse FFT processor for producing an HRR profile (image).
- FIG. 3 is a flow diagram of an exemplary process for creating an HRR profile in accordance with an embodiment of the present invention. A target of interest is detected in
step 40 and tracked instep 42. This detection and tracking may comprise any means known in the art. HRR processing in accordance with the present invention may be accomplished independent of the detection and tracking of the target of interest. However, the quality of the HRR profile may be improved if motion compensation is performed in accordance with information provided by the tracker. The HRR waveform is transmitted instep 44. The HRR waveform may comprise an FM chirp waveform and/or a stepped frequency waveform. Echoes resulting from the interaction of the transmitted HRR waveform and objects including the target(s) of interest, ground clutter, targets not of interest, and other objects, are received instep 46. The chirped received echo signal is dechirped instep 47 using an LFM dechirping waveform having the same slope as the transmitted chirped signal. - Beamforming is performed in
step 48. In an exemplary embodiment of the invention, beamforming is performed adaptively. Each echo signal corresponding to eachsegment 35 of the transmitted HRR waveform is beamformed. That is, a beam pattern is formed for each received echo signal corresponding to eachsegment 35, and weights are calculated for each beam pattern. If the transmitted HRR waveform is a chirp waveform, the received echo is separated into segments and beamforming is performed for each segment. - HRR processing is vulnerable to interference due to jamming because it requires a relatively wide operational bandwidth. This increases the chances that a jammer at a particular frequency will be in the operational bandwidth. HRR processing is also vulnerable to jamming interference because of the relatively long coherent integration time associated with HRR processing, thus increasing the likelihood that a jammer will transmit while the HRR echoes are being received. Therefore, it is generally desirable to eliminate jamming interference from the received signal (e.g., via cancellation or attenuating) in order to avoid performance degradation. Jamming interference may be canceled adaptively or manually.
- In an exemplary embodiment of the invention, jamming interference is cancelled adaptively by forming beam patterns, wherein nulls of the beam patterns are steered in the direction of the source(s) of jamming interference. Many existing adaptive techniques require a training period where no signal is present (such as during a passive listening period), or a period where the signal value is low compared to the jamming interference signal (such as in a search radar system) in order to distinguish signal energy from jammer energy. However, during HRR processing, signal content is available in substantially all frequency samples. Thus, conventional adaptive techniques may cancel desired signal in addition to canceling jamming interference. Further, conventional adaptive techniques tend to modulate the signal of interest, causing degradation in sidelobe performance as a result of changing adaptive weight values. Thus, conventional adaptive techniques may degrade the image quality of the HRR profile. An HRR process in accordance with the present invention tends to overcome these problems by tracking the target center, with respect to range, for each pulse and constrain the adaptive processing such that the frequency dependent gain is maintained toward the target center for each adaptive processing block.
- Still referring to FIG. 3, beams are formed with respect to the target center in accordance with information provided by the tracker. Weights are adaptively calculated for each received echo signal corresponding to each waveform segment35 (see FIG. 1B) of the transmitted HRR waveform, and the weights are calculated to steer at least one null toward an interference, and within the constraints that frequency dependent gain is maintained toward the target center.
-
- where, ri is the vector of the array (or sub-array) measurement for the selected range bin of the ith pulse, gSA is the array (or sub-array) gain vector at frequency fi and steering direction (Tx, Ty), Ji and ni are the jamming interference and noise component, respectively, c is the speed of light in a in the transmission medium, Rk is the position of the kth scattering center, and Tx is the azimuth directional cosine and Ty is the elevation directional cosine calculated in accordance with the following equations.
- T x=cos(β)sin(θ) (2)
- T y=sin(β), (3)
- where θ is the steering angle, in azimuth, off boresight of the antenna array, and β is the steering angle, in elevation, off boresight of the antenna array.
- Because there is no passive listening period for wideband imaging (HRR profile), there is a potential for signal cancellation. This is due to the adaptive beamforming algorithm attempting to calculate weights, which steers a null towards the signal. This signal cancellation can be avoided if a constraint is used such that the frequency dependent gain is steered toward the target reference center. This constraint will maintain the mainlobe of the beam pattern steered substantially toward the target center, and allow nulls to be formed in the direction of jamming interference. Weights formed within this constrain, in accordance with an exemplary embodiment of the invention are calculated in accordance with the following equation.
- where, the index i indicates the number of processing blocks into which the received echoes are separated for processing, Ci is the covariance matrix estimate of the ith processing block, Wi is the adaptive weight of the ith block, gSA(Tx, Ty, fi) is the array (or sub-array) gain vector used as the steering vector, H indicates the complex conjugate transpose, gΣ(Tx S, Ty S, fi) is the sum beam gain (tapered beam pattern steered toward the target) at frequency fi and steering direction (Tx S, Ty S), and the superscript S indicates the steering direction toward the target center, which is constant for each processing block.
- A sum beam is typically the weighted sum of the sub-array measurements. Sum beam antenna patterns usually peak at the desired signal direction and have low sidelobes. Accordingly, a desired sum beam gain is achieved and maintained towards the target reference for all pulses while jamming is cancelled. In this manner, the image or HRR profile quality is maintained with low range sidelobes and can be used for target discrimination or recognition applications.
- Referring again to FIG. 3, pulse compression is then performed on the beamformed data at
step 50. The selection of the bin representing the target center is determined in accordance with target range information provided by the tracker. This is followed by pulse compression and quadratic phase motion compensation. This information aids in compensating for target motion. Target motion compensation improves the quality of the HRR profile (image) by reducing quadratic phase error. - Tapered, inverse FFT processing is performed on the quadratic phase motion compensated data at
step 52. Weighted tapering is optional, however weighted tapering processing may enhance the quality of the HRR profile. Processing a wideband signal using narrowband techniques (e.g., dechirping with a linear frequency modulated waveform followed by a bandpass filter) is also referred to as stretch processing. Stretch processing is described in a document entitled “Nulling Over Extremely Wide Bandwidths When Using Stretch Processing”, proceedings of Adaptive Sensor Array Processing (ASAP), March 1999, which is hereby incorporated by reference in its entirety. Stretch processing is a process, which enables processing of wideband waveforms (e.g., HRR waveforms) with narrowband processing techniques. Stretch processing comprises converting pulse delay time, in range, to frequency. Thus the received energy from any one range has a constant frequency, and the received energy from different ranges may be separated by well know narrowband processing techniques, such as narrowband filtering with a plurality of narrowband filters via a Fast Fourier Transform (FFT). Thus, targets, which are relatively closely spaced in range, are distinguishable in the HRR profile. The pulse compressed, weighted, tapered, inverse FFT signals are formed into images instep 54. - The present invention may be embodied in the form of computer-implemented processes and apparatus for practicing those processes. The present invention may also be embodied in the form of computer program code embodied in tangible media, such as floppy diskettes, read only memories (ROMs), CD-ROMs, hard drives, high density disk, or any other computer-readable storage medium, wherein, when the computer program code is loaded into and executed by
computer processor 32, thecomputer processor 32 becomes an apparatus for practicing the invention. The present invention may also be embodied in the form of computer program code, for example, whether stored in a storage medium, loaded into and/or executed bycomputer processor 32, or transmitted over some transmission medium, such as over electrical wiring or cabling, through fiber optics, or via electromagnetic radiation, wherein, when the computer program code is loaded into and executed bycomputer processor 32, thecomputer processor 32 becomes an apparatus for practicing the invention. When implemented on a general-purpose processor, the computer program code segments configure the processor to create specific logic circuits. - The present invention may be embodied in the form of computer-implemented processes and apparatus for practicing those processes. FIG. 4 is a block diagram of a radar system comprising an
antenna array 60 andcomputer processor 62 in accordance with an exemplary embodiment of the invention. HRR waveforms are created byprocessor 62 and provided toantenna array 60. HRR waveforms are transmitted byantenna array 60. Reflected energy resulting for the transmission of the HRR waveforms is received byantenna array 60 and is provided tocomputer processor 62.Computer processor 62 performs processes for forming beam patterns, performing pulse compression, performing stretch processing, and generating images in accordance with the present invention, as herein described. Processing may also be performed by special purpose hardware. - The present invention may be embodied in the form of computer-implemented processes and apparatus for practicing those processes. The present invention may also be embodied in the form of computer program code embodied in tangible media, such as floppy diskettes, read only memories (ROMs), CD-ROMs, hard drives, high density disk, or any other computer-readable storage medium, wherein, when the computer program code is loaded into and executed by
computer processor 62, thecomputer processor 62 becomes an apparatus for practicing the invention. The present invention may also be embodied in the form of computer program code, for example, whether stored in a storage medium, loaded into and/or executed bycomputer processor 62, or transmitted over some transmission medium, such as over electrical wiring or cabling, through fiber optics, or via electromagnetic radiation, wherein, when the computer program code is loaded into and executed bycomputer processor 62, thecomputer processor 62 becomes an apparatus for practicing the invention. When implemented on a general-purpose processor, the computer program code segments configure the processor to create specific logic circuits. - Although illustrated and described herein with reference to certain specific embodiments, the present invention is nevertheless not intended to be limited to the details shown. Rather, various modifications may be made in the details within the scope and range of equivalents of the claims and without departing from the spirit of the invention.
Claims (20)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/948,959 US6531976B1 (en) | 2001-09-07 | 2001-09-07 | Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming |
PCT/US2002/028487 WO2003023438A2 (en) | 2001-09-07 | 2002-09-06 | Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming |
AU2002335716A AU2002335716A1 (en) | 2001-09-07 | 2002-09-06 | Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming |
EP02770479A EP1423724A4 (en) | 2001-09-07 | 2002-09-06 | Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/948,959 US6531976B1 (en) | 2001-09-07 | 2001-09-07 | Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming |
Publications (2)
Publication Number | Publication Date |
---|---|
US6531976B1 US6531976B1 (en) | 2003-03-11 |
US20030048214A1 true US20030048214A1 (en) | 2003-03-13 |
Family
ID=25488434
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/948,959 Expired - Fee Related US6531976B1 (en) | 2001-09-07 | 2001-09-07 | Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming |
Country Status (4)
Country | Link |
---|---|
US (1) | US6531976B1 (en) |
EP (1) | EP1423724A4 (en) |
AU (1) | AU2002335716A1 (en) |
WO (1) | WO2003023438A2 (en) |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1582890A1 (en) * | 2004-03-31 | 2005-10-05 | EADS Deutschland GmbH | Pulse radar with linear frequency modulation |
US20060273951A1 (en) * | 2005-06-02 | 2006-12-07 | Raytheon Company | Radar system and method for reducing clutter in a high-clutter environment |
US7221307B1 (en) * | 2004-07-08 | 2007-05-22 | Lockheed Martin Corporation | Determination of the presence of closely spaced targets |
WO2008094701A1 (en) * | 2007-01-31 | 2008-08-07 | Signal Labs, Inc. | System and methods for multistep target detection and parameter estimation |
US20080303711A1 (en) * | 2007-06-11 | 2008-12-11 | Mitsubishi Electric Corporation | Radar apparatus |
US20090090298A1 (en) * | 2007-08-31 | 2009-04-09 | Optomec, Inc. | Apparatus for Anisotropic Focusing |
US20100156700A1 (en) * | 2008-12-19 | 2010-06-24 | Thales | Method of managing the frequencies and boresightings emitted by a dispersive-antenna radar |
CN101881822A (en) * | 2010-06-07 | 2010-11-10 | 电子科技大学 | Method for inhibiting same frequency interference of shared-spectrum radars |
FR2986333A1 (en) * | 2012-01-27 | 2013-08-02 | Thales Sa | General-purpose monitoring method for detecting pollution traces by airborne radar, involves filtering echoes received by filter, compressing impulses by raising pseudonym ambiguities and performing low frequency recurrence process |
EP2233944A3 (en) * | 2009-03-24 | 2014-03-19 | Honeywell International Inc. | Marine radar systems and methods |
GB2521098A (en) * | 2007-12-06 | 2015-06-17 | Thales Holdings Uk Plc | High-resolution radar |
EP2226647B1 (en) * | 2009-03-04 | 2016-09-14 | Honeywell International Inc. | Systems and methods for suppressing ambiguous peaks from stepped frequency techniques |
US20180203108A1 (en) * | 2017-01-19 | 2018-07-19 | GM Global Technology Operations LLC | Iterative approach to achieve angular ambiguity resolution |
US10036800B2 (en) * | 2014-08-08 | 2018-07-31 | The United States Of America, As Represented By The Secretary Of The Navy | Systems and methods for using coherent noise filtering |
KR102077254B1 (en) * | 2018-10-17 | 2020-02-13 | 국방과학연구소 | Method for generating range deception signal of radar pulse and apparatus thereof |
KR20220071680A (en) * | 2020-11-24 | 2022-05-31 | 국방과학연구소 | Method for constructing high-resolution range profile of target in narrowband radar system |
WO2023141344A1 (en) * | 2022-01-24 | 2023-07-27 | Arizona Board Of Regents On Behalf Of The University Of Arizona | Real-time computer generated hologram (cgh) generation by compute unified device architecture (cuda)-open-gl for adaptive beam steering |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1287379B1 (en) * | 2000-06-06 | 2008-07-30 | Altratek Inc. | Sensor system and method for detecting and tracking targets |
US6690315B1 (en) * | 2003-01-31 | 2004-02-10 | United States Of America As Represented By The Secretary Of The Air Force | Quadbit kernel function algorithm and receiver |
US7440989B1 (en) | 2004-04-02 | 2008-10-21 | The United States Of America As Represented By The Secretary Of The Air Force | Kernel function approximation and receiver |
US8232907B2 (en) * | 2004-08-23 | 2012-07-31 | Telephonics Corporation | Step frequency high resolution radar |
US7474257B2 (en) * | 2004-11-08 | 2009-01-06 | The United States Of America As Represented By The Secretary Of The Navy | Multistatic adaptive pulse compression method and system |
US7345629B2 (en) * | 2006-02-21 | 2008-03-18 | Northrop Grumman Corporation | Wideband active phased array antenna system |
US7671789B1 (en) * | 2008-10-03 | 2010-03-02 | Lockheed Martin Corporation | Method and system for target detection and angle estimation based on a radar signal |
US8401206B2 (en) * | 2009-01-15 | 2013-03-19 | Microsoft Corporation | Adaptive beamformer using a log domain optimization criterion |
US8466829B1 (en) | 2009-09-14 | 2013-06-18 | Lockheed Martin Corporation | Super-angular and range-resolution with phased array antenna and multifrequency dither |
CN102169177B (en) * | 2011-01-21 | 2012-12-26 | 西安电子科技大学 | Time-domain-characteristic-based method for identifying high-resolution range profile of radar target |
US9275690B2 (en) | 2012-05-30 | 2016-03-01 | Tahoe Rf Semiconductor, Inc. | Power management in an electronic system through reducing energy usage of a battery and/or controlling an output power of an amplifier thereof |
US9509351B2 (en) | 2012-07-27 | 2016-11-29 | Tahoe Rf Semiconductor, Inc. | Simultaneous accommodation of a low power signal and an interfering signal in a radio frequency (RF) receiver |
US9722310B2 (en) | 2013-03-15 | 2017-08-01 | Gigpeak, Inc. | Extending beamforming capability of a coupled voltage controlled oscillator (VCO) array during local oscillator (LO) signal generation through frequency multiplication |
US9837714B2 (en) | 2013-03-15 | 2017-12-05 | Integrated Device Technology, Inc. | Extending beamforming capability of a coupled voltage controlled oscillator (VCO) array during local oscillator (LO) signal generation through a circular configuration thereof |
US9666942B2 (en) | 2013-03-15 | 2017-05-30 | Gigpeak, Inc. | Adaptive transmit array for beam-steering |
US9531070B2 (en) | 2013-03-15 | 2016-12-27 | Christopher T. Schiller | Extending beamforming capability of a coupled voltage controlled oscillator (VCO) array during local oscillator (LO) signal generation through accommodating differential coupling between VCOs thereof |
US9780449B2 (en) | 2013-03-15 | 2017-10-03 | Integrated Device Technology, Inc. | Phase shift based improved reference input frequency signal injection into a coupled voltage controlled oscillator (VCO) array during local oscillator (LO) signal generation to reduce a phase-steering requirement during beamforming |
US9184498B2 (en) | 2013-03-15 | 2015-11-10 | Gigoptix, Inc. | Extending beamforming capability of a coupled voltage controlled oscillator (VCO) array during local oscillator (LO) signal generation through fine control of a tunable frequency of a tank circuit of a VCO thereof |
US9716315B2 (en) * | 2013-03-15 | 2017-07-25 | Gigpeak, Inc. | Automatic high-resolution adaptive beam-steering |
US9535156B2 (en) | 2013-03-15 | 2017-01-03 | Src, Inc. | Passive listening pulse adaptive sidelobe canceller |
CN103558596A (en) * | 2013-11-14 | 2014-02-05 | 上海电机学院 | Stepped frequency radar fuze velocity compensation method |
US9379768B2 (en) * | 2014-01-31 | 2016-06-28 | Harris Corporation | Communication system with narrowband interference mitigation and related methods |
US10024973B1 (en) | 2015-04-03 | 2018-07-17 | Interstate Electronics Corporation | Global navigation satellite system spoofer identification technique |
US10056699B2 (en) | 2015-06-16 | 2018-08-21 | The Mitre Cooperation | Substrate-loaded frequency-scaled ultra-wide spectrum element |
US9991605B2 (en) | 2015-06-16 | 2018-06-05 | The Mitre Corporation | Frequency-scaled ultra-wide spectrum element |
US10545246B1 (en) * | 2016-07-08 | 2020-01-28 | Interstate Electronics Corporation | Global navigation satellite system spoofer identification technique based on carrier to noise ratio signatures |
CN106772257B (en) * | 2017-01-10 | 2019-02-26 | 西北工业大学 | A kind of low sidelobe robust adaptive beamforming method |
US10854993B2 (en) | 2017-09-18 | 2020-12-01 | The Mitre Corporation | Low-profile, wideband electronically scanned array for geo-location, communications, and radar |
US10725182B2 (en) | 2018-01-04 | 2020-07-28 | Interstate Electronics Corporation | Systems and methods for providing anti-spoofing capability to a global navigation satellite system receiver |
US10886625B2 (en) | 2018-08-28 | 2021-01-05 | The Mitre Corporation | Low-profile wideband antenna array configured to utilize efficient manufacturing processes |
CN110018461B (en) * | 2019-04-16 | 2023-03-24 | 西安电子工程研究所 | Group target identification method based on high-resolution range profile and monopulse angle measurement |
CN110531337B (en) * | 2019-09-29 | 2021-06-29 | 北京润科通用技术有限公司 | Target reliability calculation method and device based on membership analysis |
CN111830501B (en) * | 2020-06-28 | 2023-04-28 | 中国人民解放军战略支援部队信息工程大学 | HRRP history feature assisted signal fuzzy data association method and system |
CN113673554B (en) * | 2021-07-07 | 2024-06-14 | 西安电子科技大学 | Radar high-resolution range profile target recognition method based on width learning |
CN113687325B (en) * | 2021-07-08 | 2024-02-06 | 西安电子科技大学 | Method for detecting shielding small target based on LP and HRRP models |
CN113721216B (en) * | 2021-08-30 | 2024-05-17 | 西安电子科技大学 | Target detection waveform optimization and processing method of agile coherent radar |
CN116359857B (en) * | 2023-06-02 | 2023-09-01 | 中国人民解放军空军预警学院 | Space-time-frequency self-adaptive main lobe deception jamming prevention method and device for airborne early warning radar |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3747097A (en) * | 1971-02-24 | 1973-07-17 | Us Navy | Radar target imaging technique |
US3813670A (en) * | 1971-12-17 | 1974-05-28 | Us Navy | High resolution range tracking circuit |
US4229738A (en) * | 1979-01-19 | 1980-10-21 | The United States Of America As Represented By The Secretary Of The Army | Early-late gate |
US5600326A (en) * | 1991-12-16 | 1997-02-04 | Martin Marietta Corp. | Adaptive digital beamforming architecture and algorithm for nulling mainlobe and multiple sidelobe radar jammers while preserving monopulse ratio angle estimation accuracy |
US5594451A (en) * | 1995-06-06 | 1997-01-14 | Hughes Aircraft Company | Processing method using an advanced radar waveform for simultaneous matched processing and range profiling of different size targets |
US5990823A (en) * | 1997-05-07 | 1999-11-23 | Lockheed Martin Corporation | Wavelet-based radar |
US6084540A (en) * | 1998-07-20 | 2000-07-04 | Lockheed Martin Corp. | Determination of jammer directions using multiple antenna beam patterns |
US5952965A (en) * | 1998-07-21 | 1999-09-14 | Marconi Aerospace Systems Inc. Advanced Systems Division | Adaptive main beam nulling using array antenna auxiliary patterns |
-
2001
- 2001-09-07 US US09/948,959 patent/US6531976B1/en not_active Expired - Fee Related
-
2002
- 2002-09-06 EP EP02770479A patent/EP1423724A4/en not_active Withdrawn
- 2002-09-06 AU AU2002335716A patent/AU2002335716A1/en not_active Abandoned
- 2002-09-06 WO PCT/US2002/028487 patent/WO2003023438A2/en not_active Application Discontinuation
Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7362261B2 (en) | 2004-03-31 | 2008-04-22 | Eads Deutschland Gmbh | Linear frequency-modulated pulse radar |
US20050219116A1 (en) * | 2004-03-31 | 2005-10-06 | Eads Deutschland Gmbh | Linear frequency-modulated pulse radar |
EP1582890A1 (en) * | 2004-03-31 | 2005-10-05 | EADS Deutschland GmbH | Pulse radar with linear frequency modulation |
US7221307B1 (en) * | 2004-07-08 | 2007-05-22 | Lockheed Martin Corporation | Determination of the presence of closely spaced targets |
US7236124B2 (en) * | 2005-06-02 | 2007-06-26 | Raytheon Company | Radar system and method for reducing clutter in a high-clutter environment |
US20060273951A1 (en) * | 2005-06-02 | 2006-12-07 | Raytheon Company | Radar system and method for reducing clutter in a high-clutter environment |
WO2008094701A1 (en) * | 2007-01-31 | 2008-08-07 | Signal Labs, Inc. | System and methods for multistep target detection and parameter estimation |
US20080303711A1 (en) * | 2007-06-11 | 2008-12-11 | Mitsubishi Electric Corporation | Radar apparatus |
US7579982B2 (en) * | 2007-06-11 | 2009-08-25 | Mitsubishi Electric Corporation | Radar apparatus |
US20090090298A1 (en) * | 2007-08-31 | 2009-04-09 | Optomec, Inc. | Apparatus for Anisotropic Focusing |
GB2521098A (en) * | 2007-12-06 | 2015-06-17 | Thales Holdings Uk Plc | High-resolution radar |
GB2521098B (en) * | 2007-12-06 | 2016-03-23 | Thales Holdings Uk Plc | High-resolution radar |
US20100156700A1 (en) * | 2008-12-19 | 2010-06-24 | Thales | Method of managing the frequencies and boresightings emitted by a dispersive-antenna radar |
EP2226647B1 (en) * | 2009-03-04 | 2016-09-14 | Honeywell International Inc. | Systems and methods for suppressing ambiguous peaks from stepped frequency techniques |
EP2233944A3 (en) * | 2009-03-24 | 2014-03-19 | Honeywell International Inc. | Marine radar systems and methods |
CN101881822A (en) * | 2010-06-07 | 2010-11-10 | 电子科技大学 | Method for inhibiting same frequency interference of shared-spectrum radars |
FR2986333A1 (en) * | 2012-01-27 | 2013-08-02 | Thales Sa | General-purpose monitoring method for detecting pollution traces by airborne radar, involves filtering echoes received by filter, compressing impulses by raising pseudonym ambiguities and performing low frequency recurrence process |
US10036800B2 (en) * | 2014-08-08 | 2018-07-31 | The United States Of America, As Represented By The Secretary Of The Navy | Systems and methods for using coherent noise filtering |
US20180203108A1 (en) * | 2017-01-19 | 2018-07-19 | GM Global Technology Operations LLC | Iterative approach to achieve angular ambiguity resolution |
US10705202B2 (en) * | 2017-01-19 | 2020-07-07 | GM Global Technology Operations LLC | Iterative approach to achieve angular ambiguity resolution |
KR102077254B1 (en) * | 2018-10-17 | 2020-02-13 | 국방과학연구소 | Method for generating range deception signal of radar pulse and apparatus thereof |
KR20220071680A (en) * | 2020-11-24 | 2022-05-31 | 국방과학연구소 | Method for constructing high-resolution range profile of target in narrowband radar system |
KR102434426B1 (en) | 2020-11-24 | 2022-08-19 | 국방과학연구소 | Method for constructing high-resolution range profile of target in narrowband radar system |
WO2023141344A1 (en) * | 2022-01-24 | 2023-07-27 | Arizona Board Of Regents On Behalf Of The University Of Arizona | Real-time computer generated hologram (cgh) generation by compute unified device architecture (cuda)-open-gl for adaptive beam steering |
Also Published As
Publication number | Publication date |
---|---|
WO2003023438A2 (en) | 2003-03-20 |
WO2003023438A3 (en) | 2003-12-24 |
WO2003023438A9 (en) | 2004-04-15 |
EP1423724A2 (en) | 2004-06-02 |
AU2002335716A1 (en) | 2003-03-24 |
EP1423724A4 (en) | 2005-09-28 |
US6531976B1 (en) | 2003-03-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6531976B1 (en) | Adaptive digital beamforming radar technique for creating high resolution range profile for target in motion in the presence of jamming | |
US9529078B2 (en) | Using orthogonal space projections to generate a constant false alarm rate control parameter | |
Sjögren et al. | Suppression of clutter in multichannel SAR GMTI | |
CN110412568B (en) | Distance fuzzy clutter suppression method based on extended azimuth phase coding | |
US6697009B2 (en) | Adaptive digital beamforming architecture for target detection and angle estimation in multiple mainlobe and sidelobe jamming | |
EP1267444A2 (en) | Adaptive digital sub-array beamforming and deterministic sum and difference beamforming with jamming cancellation and monopulse ratio preservation | |
US20070247353A1 (en) | Method and Apparatus for Performing Bistatic Radar Functions | |
US6720910B2 (en) | Pri-staggered post-doppler adaptive monopulse processing for detection and location of a moving target in ground clutter | |
US20060181451A1 (en) | System and method for combining displaced phase center antenna and space-time adaptive processing techniques to enhance clutter suppression in radar on moving platforms | |
DE60109990T2 (en) | Monopulse radar processor for determining the azimuth and elevation angles of two targets over a matrix of amplitude ratios | |
CN109061619A (en) | A kind of method of signal processing, equipment and computer storage medium | |
US8760340B2 (en) | Processing radar return signals to detect targets | |
JP2005512435A (en) | System and method for an automatically calibrated reduced rank adaptive processor | |
CN113253222B (en) | Airborne FDA-MIMO bistatic radar distance fuzzy clutter suppression and dimension reduction search method | |
US5703593A (en) | Adaptive DPCA subsystem | |
US20060066475A1 (en) | Method for reducing angular blur in radar pictures | |
CN106054142B (en) | A kind of airborne MIMO radar main lobe smart munition suppressing method and system | |
CN114779183A (en) | Self-adaptive three-dimensional angle Doppler compensation method based on FDA-MIMO radar | |
JPH05223919A (en) | Signal processor | |
US20030132874A1 (en) | Radar system and method | |
Doerry et al. | GMTI Direction of Arrival Measurements from Multiple Phase Centers | |
CN115343683B (en) | Clutter suppression method based on combination of equal Doppler sample and equal cone angle sample | |
CN117784078B (en) | Airborne radar space-time polarization combined self-adaptive processing clutter suppression method and device | |
EP4345499A1 (en) | Two-way radar beam pattern steering | |
CN115343702A (en) | Space-based early warning radar cascade three-dimensional space-time adaptive processing method and space-based early warning radar |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: LOCKHEED MARTIN CORPORATION, MARYLAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:GENERAL ELECTRIC COMPANY;REEL/FRAME:012156/0525 Effective date: 20010906 Owner name: GENERAL ELECTRIC COMPANY, CONNECTICUT Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:YU, KAI-BOR;REEL/FRAME:012156/0704 Effective date: 20010904 |
|
FPAY | Fee payment |
Year of fee payment: 4 |
|
REMI | Maintenance fee reminder mailed | ||
LAPS | Lapse for failure to pay maintenance fees | ||
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
|
FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20110311 |