CA1251545A - Method of detection and identification of one or more remote objects - Google Patents
Method of detection and identification of one or more remote objectsInfo
- Publication number
- CA1251545A CA1251545A CA000498720A CA498720A CA1251545A CA 1251545 A CA1251545 A CA 1251545A CA 000498720 A CA000498720 A CA 000498720A CA 498720 A CA498720 A CA 498720A CA 1251545 A CA1251545 A CA 1251545A
- Authority
- CA
- Canada
- Prior art keywords
- wave energy
- signatures
- signature
- prestored
- measured signature
- 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.)
- Expired
Links
Landscapes
- Radar Systems Or Details Thereof (AREA)
Abstract
ABSTRACT
A method of detection and identification of one or more remote objects by transmitting wave energy towards the object and receiving wave energy reflected from the object as well as processing of information associated with the wave energy received. The following novel and specific combination of steps is characteristic to the method according to the invention -a) said processing comprises a number of separate signal parameters pertaining to the wave energy received, said parameters together forming a measured signature relating to the object, b) the measured signature is compared with a number of prestored signatures comprising the same separate sig-nal parameters relating to known objects being of interest to the detection and the identification, c) there is effected a recording of which signatures among the prestored signatures which within predeter-mined tolerances correspond to the measured signature, d) subsequent transmission and reception of wave energy is used for updating the separate parameters and thereby the measured signature, e) the updated measured signature is compared with the re-corded restored signatures for updated recording of a smaller number of prestored signatures which within pre-determined tolerances correspond to the updated measured signature, f) and repeating steps d) and e) until there remains a small number of recorded prestored signatures, pre-ferably only one signature, which defines a small number of objects, preferably only one such object, being of interest.
The method is primarily intended for radar systems, but other uses are also possible, such as in sonar systems.
A method of detection and identification of one or more remote objects by transmitting wave energy towards the object and receiving wave energy reflected from the object as well as processing of information associated with the wave energy received. The following novel and specific combination of steps is characteristic to the method according to the invention -a) said processing comprises a number of separate signal parameters pertaining to the wave energy received, said parameters together forming a measured signature relating to the object, b) the measured signature is compared with a number of prestored signatures comprising the same separate sig-nal parameters relating to known objects being of interest to the detection and the identification, c) there is effected a recording of which signatures among the prestored signatures which within predeter-mined tolerances correspond to the measured signature, d) subsequent transmission and reception of wave energy is used for updating the separate parameters and thereby the measured signature, e) the updated measured signature is compared with the re-corded restored signatures for updated recording of a smaller number of prestored signatures which within pre-determined tolerances correspond to the updated measured signature, f) and repeating steps d) and e) until there remains a small number of recorded prestored signatures, pre-ferably only one signature, which defines a small number of objects, preferably only one such object, being of interest.
The method is primarily intended for radar systems, but other uses are also possible, such as in sonar systems.
Description
~2515~S
This invention is primarily directed to an improved radar for detecting and identifying remote objects or targets by means of electromagnetic wave energy. The method and principles to be described may also be applied, however, to other types of wave energy, such as ultrasonic waves in sonar systems.
~ s in known radar systems the present method involves the utilization of various processing techniques for extracting useful information from the return signal or waves reflected from the target.
The radar system described here provides optimum detec-tion and identification of targets while minimizing the effect of background clutter and the impairments caused by the propagation of the electromagnetic waves through space.
This is achieved utilizing a set of new concepts for sig-nal processing, the applicability of which is made feasible by the development of new technology for generating microwaves and in particular digital signal processing.
Thus, in a main aspect this invention relates to method of detection and identification of one or more remote objects by transmitting wave energy towards the object and receiving wave energy reflected from the object as well as processing of infor-mation associated with the wave energy received, wherein said pro-cessing comprises detecting a number of separate signal parameters pertaining to the wave energy received, said parameters together forming a measured signature relating to the object, and the meas-ured signature is compared with a number of prestored signatures each comprising the same separate signal parameters relating to ~25~5~5 , known objects being of interest to the detection and the identi-fication, characterized in that A) said separate signal parameters are selected to relate to a number of independent observation domains, B) there is effected a recording of those signatures among the prestored signatures which within predetermined tolerances cor-respond to the measured signature, C) subsequent transmission and reception of wave energy is used for updating the separate para-meters and thereby the measured signature, D) the updated measured signature is compared with the recorded prestored signatures for updated recording of a smaller number of prestored signatures which within predetermined tolerances correspond to the updated measured signature, E) and steps C) and D) are repeated until there remains a small number of recorded prestored signatures, preferably only one such signature, which defines a small number of objects, pre-ferably only one such object, being of interest.
In order to obtain a number of separate signal para-meters adequate for processing as stated above, it is an advantage to use a multifrequency radar signal transmission. More specifi-cally, multifrequency polarimetric illumination of targets makes it possible to determine characteristics of target signatures.
With multifrequency illumination several independent feature or signal parameter domains of the targets are revealed. In other words this involves the simultaneous use of orthogonal signatures for identification of targe*s or objects of interest.
Such parameters or feature domains may be the following:
i the multifrequency response for the number of scales ~SlSa~S
-2a-investigated (target do~n-range signature), ii the time variations of each scale selective (see i above) multifrequency response (vibration pattern), iii mutual coherence of time and space variations (target rigidity), iv the polarization properties of each scale (target sym-metry), v polarimetric Doppler (target torsion).
As each of these parameter sets (domains) are indepen-dent and thus mathematically orthogonal~ a multidimensional target estimation is performed.
Among the parameter domains mentioned above, the multi-frequency illumination response is considered to be fundamental.
In addition thereto, the polarization properties associated with possible target symmetry may be very useful.
51~;~5 The aspect angle of target as seen from the radar location at any instant is also an important magnitude which could to some extent be considered as one of the separate signal para-meters referred to. In this context, however, the aspect angle is treated as a variable different from the types of signal parameters in the domains as listed above (i ...v).
In the drawing there is an illustration of a preferred structure of a system for carrying out the method according to this invention.
The radar system structure shown in -the drawing comprises a transmitter or wave-form generator 11 feeding an antenna 11A, as well as a receiver 12 with an associated receiving antenna 12A. These co~ponents are broadband coherent microwave components. ~he transmitter and receiver antenna may for example be combined as a single unit. Within the an-tenna beams there is indicated a target/to be detected and identified. T
As will be explained later the wave-form generator 11 is preferably an adaptive wave-form generator making it possible to adapt the wave-forms transmitted in accordance with infor-mation which may exist or may be gained with respect to the target or objects being out interest. Correspondingly, the receiver 12 may be a matched receiver having characteristics which may be selected to correspond to the particular wave-form or signature transmitted at any instant.
The signals received and detected are supplied to block 13 which comprises further detection and filtering circuits operating according to generally known principles in order to extract predetermined features or signal parameters from the received wave-form. As shown by blocks 21, 22, 23, 24 and 25 these features may consist of the following parameter domains:
21 - Multifrequency signature 22 - Beat Doppler signature 23 - Mutual coherency signature 24 - Polarimetric signature 25 - Polarimetric Doppler signature.
As will be understood, these blocks 21 - 25 correspond to the respective items i - v listed above.
~L~515~
Both analog and digital signal processing may be involved in blocks 13 and 21 - 25, and in any case the output signals from blocks 21 - 25 are in a digital form. There is a hori-zontal dashed line C-C shown in the drawing, to indicate that the functions or blocks found below that line are performed in a suitable computer. It is to be understood that there is no strict boundary between the more or less conventional signal processing blocks and circuits described above and the compu-terized functions to be explained in the following. Thus, line C-C serves to indicate that there is at a certain level of sig-nal processing relating to the various parameters or domains involved, a stage where the processing is substantially taken over by the computer in a purely digital form.
A main block or function which is typically computerized is block 40 which is a store or target library containing known signal parameters in one or more feature domains pertaining to all the targets or objects being of interest for the system con-cerned. These may for example be objects in the form of several types of passenger aircraft which normally operate on a given airport. The complete set of signal parameters pertaining to a certain aircraft may be stored in block 40 for a number of different aspect angles of such aircraft as seen from antennas 11A and 12A. Depending upon the number of signal parameters employed, the number of different aircraft to be covered and the number of aspect angles being relevant, the required storage capacity in library block 40 may be very high.
In block 41 designated signature estimation there is essen-tially performed a comparison between an actually measured signa-ture consisting of parameter sets furnished by blocks 21 - 25 for each transmission and accompanying reception of illuminating electromagnetic wave energy directed towards the target. Such measured signature is then compared initially with all the prestored signatures found in library block 40 in order to de-termine whether one or more of such prestored signatures corres-pond to the measured signature within predetermined tolerances.
Thus, by cross-referring to the library in this manner, the target identity is estimated for each of the features or signal parameters involved. The most probable target identity may be ~:~51Sf~
obtained by weighting the vote of each feature by a feature significance factor.
At this point reference is made to blocks 26 and 27 which relate to information extracted with respect to position and velocity of the target. This is information being per se funda-mental in almost all earlier and conventional radar systems.
According to the present invention such information from blocks 26 and 27 is processed further in target bearing block 30 so as to determine or estimate the aspect angle of the target.
The term aspect angle as used here, in fact comprises three angles which together define the direction of the longitudinal axis of a target in space.
As already mentioned above, such target aspect angle may be introduced in block 41 together with aspect angle information obtained from library block 40, thereby increasing the possible amount of detail with which a target may be identified. Thus, in a particular embodiment of this invention, having specific advantages, the comparison of a measured signature with pre-stored signatures is limited to prestored signatures pertà ining to the aspect angle concerned, as delivered from target bearing block 30 through connection 31.
Thus, when estimation of target identity is completed, the target by its own movement will cause the measured features or signature to change if the movement is such that the aspect angle of the target changes. This function of identity enhance-ment by verifying aspect angle dependence is performed in block 42 which on the one hand receives data from library block 40 and on the other hand receives aspect angle data from block 30 through connection 32. Since the target signature as measured will change in a deterministic manner as the aspect angle changes, this results in an improved identification of the target, based upon prestored data with respect to the target concerned, for a range or number of aspect angles. If the signature measured follows the expected changes, the probability of correct identification is increased.
In connection with the above~tracking information may be used to provide an initial knowledge of the target aspect angle for search in the prestored signature library 40. By ~515~
tracking the target over some distance, the true bearing and velocity of the target can be established. These data are used to provide the aspect angle for the target identity esti-mation, thereby reducing the search time and increasing the probability of correct identification.
The output from block 42 may be considered as the final product of the processing method performed by the system de-scribed. Thus, arrow 50 indicates some form of display to be presented to an operator or the like. The output from block 42 may, however, as indicated at 10, be fed back to the adaptive wave-form generator 11 so as to effect possible adjustments of the wave-form signature to ~e transmitted therefrom.
The display represented by arrow 50 may be a cathode ray tube screen arranged for a presentation of the PPI type, indi-cating for exa~ple a map or contours of the field surveyed, targets detected in this field, a listing showing the number of targets and their types, the sectors in which the respec-tive targets are positioned, etc.
From the structure and functions described with reference to the system in the drawing, it appears that the radar ope-rates in a number of modes. It has a detection mode, a tracking mode and an identification mode. In the detection and tracking mode, enhanced sensitivity can be achieved using the matched illumination technique. This is accomplished by transmitting a waveform with a spectrum which is the complex conjugate of the transfer function of the expected target for the assumed look angle. This process of transmitting the com-plex conjugate waveform is repeated to ensure that the approp-riate waveform for the given target at the given look angle is transmitted.
After the target is detected, located and its course de-termined, the identification process is started. The time re-quired for an identification will depend on the number of para-meters required. Some features, such as scale selection vibration pattern, requires an integration time whereby the target will move a distance equal to a few times its own length.
During identification, the target is illuminated with a co-` ~;2 515~5 herent comb of frequencies. The maximal frequency separationgives the minimum scale size investigated, and the minimum fre-quency separation determines the largest scale, which will correspond to the size of the largest target expected. The co-herency of this waveform is such that the relative phase jitter between any two frequencies after a delay corresponding to the maximum distance to the target, is less than a fraction of a wave period.
Upon reception, the in-phase and quadrature components of each frequency line is detected in a homodyne detection circuit.
The bandwidth of this circuit is equivalent to the maximum Doppler shift expected. For the chosen integration time, the RMS power (variance) of the return on each frequency line is determined. Using complex multiplication, two and two returns are combined to give the scale selective return, the scale corresponding to the frequency separation of the two frequency components combined.
The amplitude of these products, normalized with the ampli-tude of each of the two frequency lines gives the multifre-quency response (signature).
Through spectral analysis of the time series associated with each of the scale returns, the beat Doppler signature is calculated. This gives the scale selective vibration pattern. For targets like aircraft the Doppler shift will be proportional to the frequency separation and the speed of the target, whereas for clutter like the sea surface, the Doppler shift will be a function of the square root of the frequency separation only.
The mutual coherency filter gives the rigidity of the target through time-space coherency filtering.
By using two separate transmitting and receiving channels, the polarization signature of each scale is provided in the form of a scattering matrix.
The polarimetric Doppler signature reveals the time variations of the symmetry properties of the target as it moves.
This signature is revealed using spectral analysis of each individual element of the scattering matrix and also correlation between the three independent elements of the scattering matrix.
~s~s The complete set of identification parameters is obtained over the integration period wherein the radar is illuminating the target. This integration period might in the case of a pulsed radar or angular scanning radar be interrupted, provided the sampling frequency is high enough to reveal the vibrations of the target.
Thus, in subsequent transmission and reception of electro-magnetic wave energy the separate parameters and thereby the measured signature are updated. The updated measured signature is compared with the previously recorded prestored signatures having resulted from the previous transmission/reception cycle, for updated recording of a smaller number of prestored signa-tures which within predetermined tolerances correspond to the updated measured signature.
The process whereby the measured signature is compared with the prestored signature can be any of the methods described in estimation theory. In the first approximation, an estimate of the look angle of the target (being unknown at this point), is calculated so that only the set of signatures for this look angle for all the targets in the target library is used.
By repeating these cycles or method steps in analogy with the principles of successive approximations, there will finally remain a very small number of possible targets, and preferably only one and the correct target being identified with a high degree of certainty.
In the process of selecting the one target, only the set of possible targets selected in the previous iteration is further investigated. Furthermore, for each updated signature a new updated estimation of the look angle is calculated, so that the reference signature for the possible target investi-gated in the new iteration is the signature corresponding to the new look angle of the target. Through the coupling of the aspect angle information and signature measurements increased probability of correct identification is accomplished.
Experts in this field will understand that the method de-scribed here may be introduced in existing coherent radar in-stallations by having these retrofitted with the required signal processing and identification means.
This invention is primarily directed to an improved radar for detecting and identifying remote objects or targets by means of electromagnetic wave energy. The method and principles to be described may also be applied, however, to other types of wave energy, such as ultrasonic waves in sonar systems.
~ s in known radar systems the present method involves the utilization of various processing techniques for extracting useful information from the return signal or waves reflected from the target.
The radar system described here provides optimum detec-tion and identification of targets while minimizing the effect of background clutter and the impairments caused by the propagation of the electromagnetic waves through space.
This is achieved utilizing a set of new concepts for sig-nal processing, the applicability of which is made feasible by the development of new technology for generating microwaves and in particular digital signal processing.
Thus, in a main aspect this invention relates to method of detection and identification of one or more remote objects by transmitting wave energy towards the object and receiving wave energy reflected from the object as well as processing of infor-mation associated with the wave energy received, wherein said pro-cessing comprises detecting a number of separate signal parameters pertaining to the wave energy received, said parameters together forming a measured signature relating to the object, and the meas-ured signature is compared with a number of prestored signatures each comprising the same separate signal parameters relating to ~25~5~5 , known objects being of interest to the detection and the identi-fication, characterized in that A) said separate signal parameters are selected to relate to a number of independent observation domains, B) there is effected a recording of those signatures among the prestored signatures which within predetermined tolerances cor-respond to the measured signature, C) subsequent transmission and reception of wave energy is used for updating the separate para-meters and thereby the measured signature, D) the updated measured signature is compared with the recorded prestored signatures for updated recording of a smaller number of prestored signatures which within predetermined tolerances correspond to the updated measured signature, E) and steps C) and D) are repeated until there remains a small number of recorded prestored signatures, preferably only one such signature, which defines a small number of objects, pre-ferably only one such object, being of interest.
In order to obtain a number of separate signal para-meters adequate for processing as stated above, it is an advantage to use a multifrequency radar signal transmission. More specifi-cally, multifrequency polarimetric illumination of targets makes it possible to determine characteristics of target signatures.
With multifrequency illumination several independent feature or signal parameter domains of the targets are revealed. In other words this involves the simultaneous use of orthogonal signatures for identification of targe*s or objects of interest.
Such parameters or feature domains may be the following:
i the multifrequency response for the number of scales ~SlSa~S
-2a-investigated (target do~n-range signature), ii the time variations of each scale selective (see i above) multifrequency response (vibration pattern), iii mutual coherence of time and space variations (target rigidity), iv the polarization properties of each scale (target sym-metry), v polarimetric Doppler (target torsion).
As each of these parameter sets (domains) are indepen-dent and thus mathematically orthogonal~ a multidimensional target estimation is performed.
Among the parameter domains mentioned above, the multi-frequency illumination response is considered to be fundamental.
In addition thereto, the polarization properties associated with possible target symmetry may be very useful.
51~;~5 The aspect angle of target as seen from the radar location at any instant is also an important magnitude which could to some extent be considered as one of the separate signal para-meters referred to. In this context, however, the aspect angle is treated as a variable different from the types of signal parameters in the domains as listed above (i ...v).
In the drawing there is an illustration of a preferred structure of a system for carrying out the method according to this invention.
The radar system structure shown in -the drawing comprises a transmitter or wave-form generator 11 feeding an antenna 11A, as well as a receiver 12 with an associated receiving antenna 12A. These co~ponents are broadband coherent microwave components. ~he transmitter and receiver antenna may for example be combined as a single unit. Within the an-tenna beams there is indicated a target/to be detected and identified. T
As will be explained later the wave-form generator 11 is preferably an adaptive wave-form generator making it possible to adapt the wave-forms transmitted in accordance with infor-mation which may exist or may be gained with respect to the target or objects being out interest. Correspondingly, the receiver 12 may be a matched receiver having characteristics which may be selected to correspond to the particular wave-form or signature transmitted at any instant.
The signals received and detected are supplied to block 13 which comprises further detection and filtering circuits operating according to generally known principles in order to extract predetermined features or signal parameters from the received wave-form. As shown by blocks 21, 22, 23, 24 and 25 these features may consist of the following parameter domains:
21 - Multifrequency signature 22 - Beat Doppler signature 23 - Mutual coherency signature 24 - Polarimetric signature 25 - Polarimetric Doppler signature.
As will be understood, these blocks 21 - 25 correspond to the respective items i - v listed above.
~L~515~
Both analog and digital signal processing may be involved in blocks 13 and 21 - 25, and in any case the output signals from blocks 21 - 25 are in a digital form. There is a hori-zontal dashed line C-C shown in the drawing, to indicate that the functions or blocks found below that line are performed in a suitable computer. It is to be understood that there is no strict boundary between the more or less conventional signal processing blocks and circuits described above and the compu-terized functions to be explained in the following. Thus, line C-C serves to indicate that there is at a certain level of sig-nal processing relating to the various parameters or domains involved, a stage where the processing is substantially taken over by the computer in a purely digital form.
A main block or function which is typically computerized is block 40 which is a store or target library containing known signal parameters in one or more feature domains pertaining to all the targets or objects being of interest for the system con-cerned. These may for example be objects in the form of several types of passenger aircraft which normally operate on a given airport. The complete set of signal parameters pertaining to a certain aircraft may be stored in block 40 for a number of different aspect angles of such aircraft as seen from antennas 11A and 12A. Depending upon the number of signal parameters employed, the number of different aircraft to be covered and the number of aspect angles being relevant, the required storage capacity in library block 40 may be very high.
In block 41 designated signature estimation there is essen-tially performed a comparison between an actually measured signa-ture consisting of parameter sets furnished by blocks 21 - 25 for each transmission and accompanying reception of illuminating electromagnetic wave energy directed towards the target. Such measured signature is then compared initially with all the prestored signatures found in library block 40 in order to de-termine whether one or more of such prestored signatures corres-pond to the measured signature within predetermined tolerances.
Thus, by cross-referring to the library in this manner, the target identity is estimated for each of the features or signal parameters involved. The most probable target identity may be ~:~51Sf~
obtained by weighting the vote of each feature by a feature significance factor.
At this point reference is made to blocks 26 and 27 which relate to information extracted with respect to position and velocity of the target. This is information being per se funda-mental in almost all earlier and conventional radar systems.
According to the present invention such information from blocks 26 and 27 is processed further in target bearing block 30 so as to determine or estimate the aspect angle of the target.
The term aspect angle as used here, in fact comprises three angles which together define the direction of the longitudinal axis of a target in space.
As already mentioned above, such target aspect angle may be introduced in block 41 together with aspect angle information obtained from library block 40, thereby increasing the possible amount of detail with which a target may be identified. Thus, in a particular embodiment of this invention, having specific advantages, the comparison of a measured signature with pre-stored signatures is limited to prestored signatures pertà ining to the aspect angle concerned, as delivered from target bearing block 30 through connection 31.
Thus, when estimation of target identity is completed, the target by its own movement will cause the measured features or signature to change if the movement is such that the aspect angle of the target changes. This function of identity enhance-ment by verifying aspect angle dependence is performed in block 42 which on the one hand receives data from library block 40 and on the other hand receives aspect angle data from block 30 through connection 32. Since the target signature as measured will change in a deterministic manner as the aspect angle changes, this results in an improved identification of the target, based upon prestored data with respect to the target concerned, for a range or number of aspect angles. If the signature measured follows the expected changes, the probability of correct identification is increased.
In connection with the above~tracking information may be used to provide an initial knowledge of the target aspect angle for search in the prestored signature library 40. By ~515~
tracking the target over some distance, the true bearing and velocity of the target can be established. These data are used to provide the aspect angle for the target identity esti-mation, thereby reducing the search time and increasing the probability of correct identification.
The output from block 42 may be considered as the final product of the processing method performed by the system de-scribed. Thus, arrow 50 indicates some form of display to be presented to an operator or the like. The output from block 42 may, however, as indicated at 10, be fed back to the adaptive wave-form generator 11 so as to effect possible adjustments of the wave-form signature to ~e transmitted therefrom.
The display represented by arrow 50 may be a cathode ray tube screen arranged for a presentation of the PPI type, indi-cating for exa~ple a map or contours of the field surveyed, targets detected in this field, a listing showing the number of targets and their types, the sectors in which the respec-tive targets are positioned, etc.
From the structure and functions described with reference to the system in the drawing, it appears that the radar ope-rates in a number of modes. It has a detection mode, a tracking mode and an identification mode. In the detection and tracking mode, enhanced sensitivity can be achieved using the matched illumination technique. This is accomplished by transmitting a waveform with a spectrum which is the complex conjugate of the transfer function of the expected target for the assumed look angle. This process of transmitting the com-plex conjugate waveform is repeated to ensure that the approp-riate waveform for the given target at the given look angle is transmitted.
After the target is detected, located and its course de-termined, the identification process is started. The time re-quired for an identification will depend on the number of para-meters required. Some features, such as scale selection vibration pattern, requires an integration time whereby the target will move a distance equal to a few times its own length.
During identification, the target is illuminated with a co-` ~;2 515~5 herent comb of frequencies. The maximal frequency separationgives the minimum scale size investigated, and the minimum fre-quency separation determines the largest scale, which will correspond to the size of the largest target expected. The co-herency of this waveform is such that the relative phase jitter between any two frequencies after a delay corresponding to the maximum distance to the target, is less than a fraction of a wave period.
Upon reception, the in-phase and quadrature components of each frequency line is detected in a homodyne detection circuit.
The bandwidth of this circuit is equivalent to the maximum Doppler shift expected. For the chosen integration time, the RMS power (variance) of the return on each frequency line is determined. Using complex multiplication, two and two returns are combined to give the scale selective return, the scale corresponding to the frequency separation of the two frequency components combined.
The amplitude of these products, normalized with the ampli-tude of each of the two frequency lines gives the multifre-quency response (signature).
Through spectral analysis of the time series associated with each of the scale returns, the beat Doppler signature is calculated. This gives the scale selective vibration pattern. For targets like aircraft the Doppler shift will be proportional to the frequency separation and the speed of the target, whereas for clutter like the sea surface, the Doppler shift will be a function of the square root of the frequency separation only.
The mutual coherency filter gives the rigidity of the target through time-space coherency filtering.
By using two separate transmitting and receiving channels, the polarization signature of each scale is provided in the form of a scattering matrix.
The polarimetric Doppler signature reveals the time variations of the symmetry properties of the target as it moves.
This signature is revealed using spectral analysis of each individual element of the scattering matrix and also correlation between the three independent elements of the scattering matrix.
~s~s The complete set of identification parameters is obtained over the integration period wherein the radar is illuminating the target. This integration period might in the case of a pulsed radar or angular scanning radar be interrupted, provided the sampling frequency is high enough to reveal the vibrations of the target.
Thus, in subsequent transmission and reception of electro-magnetic wave energy the separate parameters and thereby the measured signature are updated. The updated measured signature is compared with the previously recorded prestored signatures having resulted from the previous transmission/reception cycle, for updated recording of a smaller number of prestored signa-tures which within predetermined tolerances correspond to the updated measured signature.
The process whereby the measured signature is compared with the prestored signature can be any of the methods described in estimation theory. In the first approximation, an estimate of the look angle of the target (being unknown at this point), is calculated so that only the set of signatures for this look angle for all the targets in the target library is used.
By repeating these cycles or method steps in analogy with the principles of successive approximations, there will finally remain a very small number of possible targets, and preferably only one and the correct target being identified with a high degree of certainty.
In the process of selecting the one target, only the set of possible targets selected in the previous iteration is further investigated. Furthermore, for each updated signature a new updated estimation of the look angle is calculated, so that the reference signature for the possible target investi-gated in the new iteration is the signature corresponding to the new look angle of the target. Through the coupling of the aspect angle information and signature measurements increased probability of correct identification is accomplished.
Experts in this field will understand that the method de-scribed here may be introduced in existing coherent radar in-stallations by having these retrofitted with the required signal processing and identification means.
Claims (10)
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. Method of detection and identification of one or more remote objects by transmitting wave energy towards the object and receiving wave energy reflected from the object as well as pro-cessing of information associated with the wave energy received, wherein said processing comprises detecting a number of separate signal parameters pertaining to the wave energy received, said parameters together forming a measured signature relating to the object, and the measured signature is compared with a number of prestored signatures each comprising the same separate signal parameters relating to known objects being of interest to the detec-tion and the identification, characterized in that A) said separate signal parameters are selected to relate to a number of independent observation domains, B) there is effected a recording of those signatures among the prestored signatures which within predeter-mined tolerances correspond to the measured signature, C) subsequent transmission and reception of wave energy is used for updating the separate parameters and thereby the measured signature, D) the updated measured signature is compared with the recorded prestored signatures for updated recording of a smaller number of prestored signatures which within predetermined tolerances correspond to the updated measured signature, E) and steps C) and D) are repeated until there remains a small number of recorded prestored signa-tures, preferably only one such signature, which defines a small number of objects, preferably only one such object, being of interest.
2. Method according to claim 1, characterized in that the separate signal parameters comprise the multifrequency response of the object obtained by transmitting a number of coherent signal frequencies.
3. Method according to claim 2, characterized in that the separate signal parameters comprise the Doppler response of the object for each individual multifrequency component.
4. Method according to claim 3, characterized in that the separate signal parameters comprise the mutual time coherency be-tween the multifrequency response and the Doppler response.
5. Method according to claim 1, characterized in that the separate signal parameters comprise the polarization response of the object.
6. Method according to claim 1, characterized in that the separate signal parameters comprise the polarization Doppler res-ponse of the object.
7. Method according to claim 1, 2 or 3, characterized in that the separate signal parameters comprise the polarization res-ponse of the object and the polarization Doppler response of the object obtained by transmitting wave energy having two orthogonal polarization directions and being so coded that the resulting contribution in each of two corresponding receiver polarization channels can be separated into co-polarized and cross-polarized components which constitute the polarization response and the polarization Doppler response, respectively.
8. Method according to claim 1, characterized in that the prestored signatures relate to a number of different aspect angles for each of the known objects being of interest and that for each transmission, reception and measured signature the aspect angle in which the object is seen is determined.
9. Method according to claim 8, characterized in that the comparison of the measured signature with prestored signatures is limited to prestored signatures pertaining to the actual aspect angle being determined.
10. Method according to claim 1, 2 or 3 wherein the trans-mitted wave energy is adapted to the objects being of interest, characterized in that the prestored signatures pertaining to the successively recorded objects, are taken as a basis for successively corresponding adaption of the transmitted wave energy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000498720A CA1251545A (en) | 1985-12-30 | 1985-12-30 | Method of detection and identification of one or more remote objects |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000498720A CA1251545A (en) | 1985-12-30 | 1985-12-30 | Method of detection and identification of one or more remote objects |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1251545A true CA1251545A (en) | 1989-03-21 |
Family
ID=4132198
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000498720A Expired CA1251545A (en) | 1985-12-30 | 1985-12-30 | Method of detection and identification of one or more remote objects |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA1251545A (en) |
-
1985
- 1985-12-30 CA CA000498720A patent/CA1251545A/en not_active Expired
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0236331B1 (en) | Methods of detection and identification of one or more remote objects | |
| US5504490A (en) | Radar method and device for the measurement of distance | |
| US4706031A (en) | Method and system for detecting an object with a radio wave | |
| Li et al. | Using range profiles as feature vectors to identify aerospace objects | |
| US5247303A (en) | Data quality and ambiguity resolution in a doppler radar system | |
| US4766435A (en) | Adaptive radar for reducing background clutter | |
| AU2009227736B2 (en) | Remote detection and measurement of objects | |
| US4707697A (en) | High resolution noncoherent radar imager | |
| EP0547686B1 (en) | Radar apparatus provided with a coherent clutter map | |
| US4996533A (en) | Single station radar ocean surface current mapper | |
| US4829306A (en) | System for detection of objects with given, known characteristics against a background | |
| US4490718A (en) | Radar apparatus for detecting and/or classifying an agitated reflective target | |
| US4484193A (en) | Radar apparatus for detecting and/or classifying an agitated reflective target when relative translation obtains | |
| US4641138A (en) | Radar apparatus for detecting an agitated reflective target | |
| JPH059752B2 (en) | ||
| EP0851238A2 (en) | Doppler radar | |
| US4881079A (en) | Aperture radar | |
| Yang et al. | Experimental observation and analysis of ionosphere echoes in the mid-latitude region of China using high-frequency surface wave radar and ionosonde | |
| CA1251545A (en) | Method of detection and identification of one or more remote objects | |
| US5694131A (en) | Method and apparatus for detecting multipath interference in a radar receiver | |
| AU664802B2 (en) | Echo ranging system | |
| US4641137A (en) | Radar apparatus for determining range to an agitated reflective target | |
| US4449209A (en) | Utilization of entire transmitted bandwidth in continuous transmission FM sonar | |
| US3991418A (en) | Electromagnetic wave direction finding using Doppler techniques | |
| US5854601A (en) | Methods for estimating the number of emitters and their parameters |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MKEX | Expiry |