WO1995028652A1 - A system for correcting receiver errors in radar - Google Patents

A system for correcting receiver errors in radar Download PDF

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Publication number
WO1995028652A1
WO1995028652A1 PCT/AU1995/000217 AU9500217W WO9528652A1 WO 1995028652 A1 WO1995028652 A1 WO 1995028652A1 AU 9500217 W AU9500217 W AU 9500217W WO 9528652 A1 WO9528652 A1 WO 9528652A1
Authority
WO
WIPO (PCT)
Prior art keywords
system
receiver
signals
frequency
transform
Prior art date
Application number
PCT/AU1995/000217
Other languages
French (fr)
Inventor
Ian Dennis Longstaff
David Andrew Noon
Glen Francis Stickley
Original Assignee
The University Of Queensland
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority to AUPM5112A priority Critical patent/AUPM511294A0/en
Priority to AUPM5112 priority
Application filed by The University Of Queensland filed Critical The University Of Queensland
Priority claimed from AU22099/95A external-priority patent/AU2209995A/en
Publication of WO1995028652A1 publication Critical patent/WO1995028652A1/en

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/40Means for monitoring or calibrating
    • G01S7/4004Means for monitoring or calibrating of parts of a radar system
    • G01S7/4021Means for monitoring or calibrating of parts of a radar system of receivers
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/35Details of non-pulse systems
    • G01S7/352Receivers
    • G01S7/354Extracting wanted echo-signals
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S13/00Systems 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
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/06Systems determining position data of a target
    • G01S13/08Systems for measuring distance only
    • G01S13/32Systems for measuring distance only using transmission of continuous unmodulated waves, amplitude-, frequency- or phase-modulated waves
    • G01S13/34Systems for measuring distance only using transmission of continuous unmodulated waves, amplitude-, frequency- or phase-modulated waves using transmission of frequency-modulated waves and the received signal, or a signal derived therefrom, being heterodyned with a locally-generated signal related to the contemporaneous transmitted signal to give a beat-frequency signal
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S13/00Systems 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
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/06Systems determining position data of a target
    • G01S13/08Systems for measuring distance only
    • G01S13/32Systems for measuring distance only using transmission of continuous unmodulated waves, amplitude-, frequency- or phase-modulated waves
    • G01S13/36Systems for measuring distance only using transmission of continuous unmodulated waves, amplitude-, frequency- or phase-modulated waves with phase comparison between the received signal and the contemporaneously transmitted signal
    • G01S13/38Systems for measuring distance only using transmission of continuous unmodulated waves, amplitude-, frequency- or phase-modulated waves with phase comparison between the received signal and the contemporaneously transmitted signal wherein more than one modulation frequency is used
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/35Details of non-pulse systems
    • G01S7/352Receivers
    • G01S2007/358Receivers using I/Q processing

Abstract

The system involves applying a predetermined signal to a radar receiver at each frequency of stepped frequencies employed or at the intermediate frequency and obtaining digitised quadrature signals. An estimate of a correction transform is obtained from the quadrature signals and stored. The predetermined signal is disconnected and the transform employed to correct for quadrature phase error and quadrature gain error in the received signals at each frequency step or at the intermediate frequency during reception of signals by the receiver.

Description

TITLE "A SYSTEM FOR CORRECTING RECEIVER ERRORS IN RADAR" FIELD OF THE INVENTION THE INVENTION relates to a system for correcting receiver errors in radar. In particular, the invention concerns correcting receiver errors in step frequency radar.

BACKGROUND OF THE INVENTION

A step frequency radar signal can be used to synthesise a narrow time domain pulse. Receiver errors occur because the quadrature (I, Q) receiver is imperfect in its operation. The errors introduced by the quadrature receiver include phase errors and gain errors in the quadrature signals obtained from the receiver. In addition to this, offset errors and common gain errors are also present.

Correct operation of the receiver requires the reference signals to the quadrature receiver to be exactly 90° out of phase. As well, the quadrature channel gains must be equivalent. If these conditions are not met, spurious range signals are generated in the range signal synthesis process.

In a homodyne system, offset errors may be corrected employing the method suggested by Noon et al in the paper entitled "An Inexpensive Microwave Distance Measuring System" 1993 Microwave and Optical Technology Letters, 6, pages 287 to 292. Correction of offset errors is also required for superheterodyne and heterodyne systems but only at the intermediate frequency (IF).

It is an object of the present invention to provide a system which at least minimises the difficulties referred to above.

DISCLOSURE OF THE INVENTION According to one aspect, the present invention provides a system for correcting receiver errors in a radar, the system including applying a predetermined signal to a radar receiver at each frequency of stepped frequencies employed or at an intermediate frequency, sampling quadrature signals obtained from the receiver at each frequency step or at the intermediate frequency, forming an estimate of a correction transform for the quadrature signals and storing the transform and then disconnecting the predetermined signal and employing the transform to correct for quadrature phase error and quadrature gain error in received signals at each frequency step or at the intermediate frequency during reception of signals by the receiver.

The quadrature signals are received from I, Q channels made available by the receiver. The signals provided by the I, Q channels may be digitised employing an analogue to digital converter. To secure the correction transform at each of the stepped frequencies employed in the radar system, the stepped frequency signals are progressively coupled to the receiver and mixed with the predetermined signal referred to above. For superheterodyne and heterodyne systems, the intermediate frequency is coupled to the receiver and mixed with the predetermined signal referred to above. System gain errors may be corrected after correction of quadrature phase gain and offset errors in the receiver. Offset error correction may be carried out employing the method disclosed in the Noon et al publication. The predetermined signal employed to secure an estimate of the correction transform may consist of narrow band Gaussian noise and this Gaussian noise signal may be applied to the receiver and mixed with the stepped frequency input coupled to the receiver or with the IF.

It is preferred that the amplitude of the Gaussian noise signal be selected to substantially fill the dynamic range of the A-D converter employed to digitise the signals secured from the I,Q channels. A sufficient number of samples of the noise should be taken at each frequency step or at the IF in order to ensure that an effective estimate of the covariance matrix can be obtained from which the correction transform is secured. This allows optimum transformation to be determined for converting sampled data into uncorrelated data of equal variance. It is preferred that the variance be constrained to be the same at each frequency of the frequency steps or at each intermediate frequency. After the correction transform has been secured, then during actual operation of the radar, the transform may be applied to the I, Q signals at each step frequency signal or at each IF to decorrelate the quadrature channls.

As an alternative to employing a narrow band Gaussian noise signal as the predetermined signal, a sinusoidal signal may be used. Where a sinusoidal signal is employed, the amplitude of that signal should be selected to substantially fill the dynamic range of the A-D converter. It is also preferred that the frequency of the sinusoidal signal be tuned so that it has a slight frequency offset from the transmitted radar frequency at each frequency step or from the IF. The offset should be such that it falls within the instantaneous band width of the receiver and is sufficiently offset from the centre frequency of the receiver to allow more than 2 π radians of rotation during a data sampling period. Where the predetermined signal is a sinusoidal signal, the system of the invention may employ the covariance matrix transform similar to that used where the predetermined signal is narrow band Gaussian noise. As an alternative to this, an ellipse may be fitted to the locii of points formed on a complex plane of the quadrature signals taken at each frequency step or at the IF. The minor and major axes of the ellipse may be determined and allow the correction transform to be determined for converting received data into a circle and hence correct phase and gain errors. In an alternative to that described above, the predetermined signal employed in the system of the invention may comprise a modulated form of an output from the transmitter. Provided the form of the modulation is known, it is possible to determine the correction transform required to correct for phase and gain errors in the quadrature signals.

As mentioned above, in addition to correcting for quadrature phase and gain errors, the invention may also provide for correction of system gain errors. A correction factor may be secured and applied at each frequency step employed in the transmitter such that the magnitude of the complex signal at the receiver is constant across the transmitter band.

DISCLOSURE OF THE DRAWINGS

A particular preferred embodiment of the invention will now be described by way of example with reference to the drawings in which: Figure 1 shows a block diagram form of part of a quadrature radar system and how a quadrature phase and gain correction transform may be secured;

Figure 2 shows a block diagram of the way in which the correction transform secured in the system of Figure 1 is used in part of a quadrature radar receiver;

Figure 3 is a block diagram showing a preferred system securing an offset correction transform;

Figure 4 is a block diagram showing a system employing the transform secured in Figure 3 and using it to correct offset errors;

Figure 5 is a block diagram showing a preferred system for securing a system gain correction transform;

Figure 6 is a block diagram of a system « employing the transform of Figure 5 in system gain correction;

Figure 7 is a detailed block diagram of a system as shown in Figure 1;

Figure 8 is a detailed block diagram of what is shown in Figure 2; and Figure 9 is a diagram of a radar receiver showing offset correction, quadrature gain and phase correction and system gain correction in diagrammatic form. DETAILED DESCRIPTION OF THE DRAWINGS Figure 1 shows a quadrature receiver which mixes a coupled signal from the transmitter with a received signal at each frequency stop or at the IF to enable the quadrature signals I, Q to be secured for each frequency step employed in the transmitter. The I, Q signals are digitised in an A-D converter and processed in a digital signal processor (DSP) which applies a correction transform at each frequency step or at the IF to the digitised receiver signals to correct for quadrature gain and phase errors. The transform required is stored in a memory and applied to the digital signal processor such that corrected digitised I, Q signals are secured from the digital signal processor at each frequency step or at the IF.

Figure 2 is useful in explaining the manner in which an estimate of the correction transform may be secured and stored in memory. As shown in this Figure, the received signal is disconnected from the receiver and in its place, the predetermined signal previously mentioned is applied to the receiver and mixed with the coupled signal at each frequency step or at the IF. The predetermined signal, as discussed, may consist of narrow band Gaussian noise, a sinusoidal signal, an attenuated and modulated form of the transmitter output or any other suitable signal. The quadrature signals I, Q secured from the receiver are digitised in an analog to digital (A-D) converter and applied to a digital signal processor (DSP). Since the characteristics of the predetermined signal are known, the digital signal processor is able to determine an estimate of a correction transform required to correct for phase and gain errors introduced by the quadrature receiver at each of the frequencies or at the IF. The correction transform is stored in memory and employed as discussed above in relation to Figure 1 to correct for phase and gain errors during actual reception of the signals during use of the radar system.

Figure 3 of the drawings shows a block diagram of a preferred radar system and illustrates the way in which an offset correction transform may be secured. The RF input to the quadrature receiver is terminated with a matched terminator. The coupled signal is applied to the mixer and the resultant I, Q quadrature signals are applied to the input of an analog to digital converter. The digitised I, Q signals are then processed for each frequency or at the IF to provide an offset correction transform in memory which may be used during operation of the radar system as shown in Figure 4 to provide for offset correction in an operational system. In Figure 4, the received signal and the coupling signal are mixed in the quadrature receiver to provide I, Q signals at each frequency step or at the IF. These I, Q signals are digitised in the A-D converter and the digitised signal applied to a digital signal processor in which those signals are modified in line with the transform stored in memory to provide resultant I, Q signals at each of the frequency steps or at the IF which have been corrected for offset error.

Figure 5 of the drawings shows a block diagram of one way in which system gain error may be corrected. System gain correction or pre-whitening correction may be achieved by directly mixing the output of the transmitter for each of the frequency steps with the coupled signal at each frequency step or at the IF to provide I, Q signals for application to the analog-to-digital converter. The digitised I, Q signals so produced are applied to the digital signal processor and a correction transform stored in memory. In Figure 6, that correction transform can then be applied to the digitised I, Q signals secured during actual use of the radar system to produce at the output of the digital signal processor, I, Q signals which have been corrected for system gain errors.

Figure 7 of the drawings is a more detailed block diagram form of what is shown in Figure 1. The signal from the wideband Gaussian noise generator is mixed with the coupled signal at each frequency step or at the IF in the quadrature receiver. The resultant I, Q signals are then passed through a low pass filter. The nett effect of this is the same as if a narrow band Gaussian noise signal was mixed with the coupled signal and the resultant I, Q signals were not low pass filtered. The narrow band signals secured from the low pass filter are digitised in the analog to digital converter and samples of the I, Q signals are taken at each frequency step and a covariance matrix is secured at each frequency step or at the IF. The matrix at each frequency step or at the IF is then processed to determine transforms which will decorrelate the I, Q signals and a scaling transform is produced to equalise the I, Q channel gains. A memory is then employed to store each of the transforms for each frequency step or at the IF.

Figure 8 of the drawings is a more detailed block diagram form of what is shown in Figure 2 and shows the manner in which the stored correction transform may be employed to correct I, Q signals for phase and gain errors. This is achieved by mixing the received signal with the coupled signal at each frequency step or at the IF in the receiver, low pass filtering the I, Q signals and then digitising those signals in an analog to digital converter. Samples are taken of the I, Q signals for each frequency step employed in the transmitter and then the correction transform is applied at each step to correct the quadrature gain and phase errors to provide corrected I, Q signals.

Figure 9 shows a simplified block diagram form which illustrates the manner in which I, Q signals received from the quadrature receiver may be corrected for offset gain, quadrature gain and phase errors and system gain errors to provide I, Q signals corrected for all of these errors.

Claims

AMENDED CLAIMS
[received by the International Bureau on 15 August 1995 (15.08.95); original claims 1-12 replaced by amended claims 1-9 (2 pages)] .
1. A system for correcting receiver errors in a radar, the system including- applying a Gaussian noise signal to a radar receiver at each frequency of stepped frequencies employed or at an intermediate frequency, sampling quadrature signals obtained from the receiver at each frequency step or at the intermediate frequency, forming an estimate of a correction transform for the quadrature signals and storing the transform and then disconnecting the Gaussian noise signal and employing the transform to correct for quadrature phase error and quadrature gain error in received signals at each frequency step or at the intermediate frequency during reception of signals by the receiver. 2. The system of Claim 1 wherein the quadrature signals are sampled employing an analogue to digital converter.
3. The system of Claim 1 or 2 wherein the correction transform is secured by progressively coupling the stepped frequency signals to the receiver and mixing the stepped frequency signals with the Gaussian noise signal.
4. The system of Claim 1 or 2 wherein the correction transform is secured by coupling the intermediate frequency to the receiver and mixing the intermediate frequency with the Gaussian noise signal.
5. The system of Claim 1 wherein a predetermined number of samples of the noise signal is taken at each of the stepped frequencies or at the intermediate frequency to ensure that an effective estimate of a covariance matrix is obtained from which the correction transform is secured for allowing the transform to be determined for converting sampled data into uncorrelated data of equal variance. 6. The system of Claim 5 wherein the variance of is constrained to be the same at each of the stepped frequencies or at each intermediate frequency. 7. The system of Claim 5 employing an ellipse fitted to locii of points formed on a complex plane of the quadrature signals taken at each frequency step or at the intermediate frequency and determining the major and minor axes of the ellipse and the correction transform for converting received data into a circle and hence correct for phase and gain errors.
8. The system of Claim 5 or 7 wherein the output from a transmitter of the system is modulated and input into the receiver to determine the correction transform. 9. The system of Claim 1 including correcting for system gain errors by determining a correction factor and applying that factor at each frequency step employed in a transmitter of the system so that the magnitude of the complex signal at the receiver is constant across the transmitter band.
PCT/AU1995/000217 1994-04-18 1995-04-18 A system for correcting receiver errors in radar WO1995028652A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
AUPM5112A AUPM511294A0 (en) 1994-04-18 1994-04-18 A system for correcting receiver errors in radar
AUPM5112 1994-04-18

Applications Claiming Priority (1)

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AU22099/95A AU2209995A (en) 1994-04-18 1995-04-18 A system for correcting receiver errors in radar

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998038523A1 (en) * 1997-02-28 1998-09-03 Siemens Aktiengesellschaft Distance and speed measuring method and device

Citations (8)

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Publication number Priority date Publication date Assignee Title
US3950750A (en) * 1974-10-03 1976-04-13 Raytheon Company Radar system having quadrature phase detector compensator
US4003054A (en) * 1974-10-03 1977-01-11 Raytheon Company Method of compensating for imbalances in a quadrature demodulator
EP0110260A1 (en) * 1982-11-29 1984-06-13 Hollandse Signaalapparaten B.V. Pulse radar apparatus
US4616229A (en) * 1983-09-30 1986-10-07 Westinghouse Electric Corp. System and method of compensating a doppler processor for input unbalance and an unbalance measuring sensor for use therein
US4646093A (en) * 1984-08-22 1987-02-24 Raytheon Company Digital monopulse for tracking radar
US4931800A (en) * 1989-05-12 1990-06-05 Raytheon Company Stagger compensated moving target detector
US4994810A (en) * 1990-03-26 1991-02-19 Allied-Signal Inc. Monopulse processor digital correction circuit
US5063529A (en) * 1989-12-29 1991-11-05 Texas Instruments Incorporated Method for calibrating a phased array antenna

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3950750A (en) * 1974-10-03 1976-04-13 Raytheon Company Radar system having quadrature phase detector compensator
US4003054A (en) * 1974-10-03 1977-01-11 Raytheon Company Method of compensating for imbalances in a quadrature demodulator
EP0110260A1 (en) * 1982-11-29 1984-06-13 Hollandse Signaalapparaten B.V. Pulse radar apparatus
US4616229A (en) * 1983-09-30 1986-10-07 Westinghouse Electric Corp. System and method of compensating a doppler processor for input unbalance and an unbalance measuring sensor for use therein
US4646093A (en) * 1984-08-22 1987-02-24 Raytheon Company Digital monopulse for tracking radar
US4931800A (en) * 1989-05-12 1990-06-05 Raytheon Company Stagger compensated moving target detector
US5063529A (en) * 1989-12-29 1991-11-05 Texas Instruments Incorporated Method for calibrating a phased array antenna
US4994810A (en) * 1990-03-26 1991-02-19 Allied-Signal Inc. Monopulse processor digital correction circuit

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
IEEE, TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, Vol. AES-17, No. 1, January 1981, F.E. CHURCHILL et al., "The Correction of I and Q Errors in A Coherent Processor", pages 131-137. *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998038523A1 (en) * 1997-02-28 1998-09-03 Siemens Aktiengesellschaft Distance and speed measuring method and device

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Publication number Publication date
ZA9503125B (en) 1996-01-09
AUPM511294A0 (en) 1994-05-12

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