EP2191294A2 - Adaptive calculation of pulse compression filter coefficients for a radar signal - Google Patents
Adaptive calculation of pulse compression filter coefficients for a radar signalInfo
- Publication number
- EP2191294A2 EP2191294A2 EP08801241A EP08801241A EP2191294A2 EP 2191294 A2 EP2191294 A2 EP 2191294A2 EP 08801241 A EP08801241 A EP 08801241A EP 08801241 A EP08801241 A EP 08801241A EP 2191294 A2 EP2191294 A2 EP 2191294A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- pulse compression
- filter
- signal
- received signal
- filter coefficients
- 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.)
- Ceased
Links
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
- G01S13/08—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
- G01S13/284—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 coded pulses
- G01S13/288—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 coded pulses phase modulated
-
- 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
- G01S7/285—Receivers
- G01S7/288—Coherent receivers
- G01S7/2883—Coherent receivers using FFT processing
Definitions
- the invention relates to a method according to the features of the preamble of the current claim 1.
- the PK filter coefficients should be optimized and adapted to specific components of the signal processing, such as filters used. A signal that has passed through an entire signal processing chain has in some cases other properties than a theoretical signal. The PK filter should therefore not be optimized for an ideal theoretical transmission signal, but adapted to a - according to the signal processing - filtered received signal adapted (adapted). 2. The PK filter should not be optimized to the usually preferred Doppler zero position but to a specific Doppler frequency. This can be about in a PC application that takes place after the Doppler processing at the respective filter outputs. 3. The PK filter should be optimized for transmitter shortcomings. These can be caused, for example, by the C operation of the power amplifier. The transmitter amplifies completely from a certain signal amplitude and the signal goes into saturation. Also, based on the passage of such a transmitter in C mode, the signal receives partly different properties than a theoretical signal.
- the PK filter conventional type can be adapted only to the transmitter behavior of a frequency. However, if during a certain time window the signal does not change appreciably with respect to the PK, an online calculation of the PK filter coefficients for this time window could adaptively optimize the PK image adaptively.
- the calculation of the PK filter coefficients in its conventional manner in which once-calculated coefficients of the PK filter are fixedly implemented during the operation of the radar system, takes place according to an iteration algorithm.
- a corresponding period of time must be set for the calculation of the filter coefficients.
- some experience in dealing with pulse compression is necessary in order to be able to model the desired compressed pulse, especially for truly complex-valued signals. Only when this modeling has been carried out carefully, effective PK side-lobe suppression can be achieved. Consequently, it is almost impossible to implement this algorithm as automatism, without sufficient monitoring. Therefore, this conventional iteration algorithm is rather unsuitable for the adaptive on-line calculation of the PK filter coefficients.
- the object of the invention is to provide a method with which the disadvantages of the prior art can be eliminated.
- pulse compression filter coefficients for a received signal of a radar system are adaptively calculated, the received signal being evaluated with the aid of a complex pulse compression mismatch filter and a pulse compression filter coefficient set h (t) being calculated for an ideal theoretical received signal s (t).
- a transformed set of pulse compression filter coefficients H opt (f) for the complex pulse compression -Mismatch filter H opt (f) are calculated according to the following rule where S (f): the Fourier transform of an undistorted received signal s (t), S v (f): the Fourier transform of a distorted received signal s v (t), Sv * (f): the complex conjugate of S v ( f) H (f): the Fourier transform of the pulse compression mismatch filter h (t).
- s (t), h (t), H op t (f) are to be understood as vectors.
- Such an algorithm for optimizing (adapting) the PK filter coefficients to the present received signal has the following form:
- the conventional iteration algorithm is used to calculate PK filter coefficients in order to calculate a PK mismatched filter h (t) for an ideal theoretical received signal s (t), that is to say for an "unadulterated" received signal, such that a PK output signal g (t) results in a sufficiently high sidelobe distance.
- S (f), H (f) and G (f) are the transfer functions of s (t), h (t) and g (t).
- an adaptive optimal PK filter hopt (t) to be calculated online is searched for-whatever-"falsified," that is, signal distortion-prone receive signal s v (t), which can change during the radar operation such that after the PK a PK output results, which has a high quality PK output in the form of a high sidelobe distance, and: h opt (t) should be able to be calculated online, ie fast and without a monitoring mechanism.
- the same and with respect to the main to sidelobel ratio (HNV) sufficiently good
- Output signal arise, as in the PK filtering of the "unadulterated" received signal s (t), ie g (t).
- Fig. 3 circuit of a radar with a component having the invention.
- the starting point is an example of a well-known in the art pulse compression code, the binary code of the 13er Barker code. It is a real-valued signal with the coding (+ stands for +1 and - for -1) + + + + + + + + + _ + _ +. This Signal or this coding represents in the above formulas the "unadulterated" signal s (t).
- a length 37 PK mismatched filter was calculated at s (t).
- This PK filter which is represented by (1) in Fig. 1, represents h (t) in the above formulas.
- This PK filter h (t) provides the PK output g (t), the magnitude of which is represented by (1) in FIG. 2, and a high peak-to-peak ratio (HNV) of FIG 42.3 dB.
- HNV peak-to-peak ratio
- the signal s v (t) which does not consist of 13 but instead of 14 sub-pulses according to the coding + + + + + + + + - + + _ + _ as s), is present as a "corrupted" signal.
- a PK-MMF h opt (t) should be found so that s v (t) gives the same PK-output g (t) at pulse compression with h opt (t) as the PK of s (t) with h ( t).
- FIG. 3 illustrates, with reference to a schematic representation of a radar system, how an online calculation of the PK filter coefficients according to the invention can be achieved.
- a signal sample is taken at predetermined time intervals after the signal processing in the branch of the signal generation.
- the signal conditioning essentially consists of the actual signal generation, mixers, preamplifiers and Power amplifier (bottom view in Fig. 3).
- a signal sample is coupled out and fed to the receiving path during the dead time (upper illustration in FIG. 3) of the pulse.
- the signal sample passes through the relevant components of the signal processing in the reception train, which is usually a bandwidth-determining antialiasing filter and necessary mixers.
- the resulting signal sample corresponds to the expected received pulse before the PK. This is then used for the online calculation according to the above formula (the theoretical signal and its associated PK filter are already available) and in this way the pulse compression filter adapted from time to time to the present waveform (adapted).
- H m S (J) - H (J). s; (J)
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)
- Amplifiers (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007041669A DE102007041669B4 (en) | 2007-09-01 | 2007-09-01 | Method for improving the signal quality of radar systems |
PCT/DE2008/001433 WO2009026911A2 (en) | 2007-09-01 | 2008-09-01 | Adaptive calculation of pulse compression filter coefficients for a radar signal |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2191294A2 true EP2191294A2 (en) | 2010-06-02 |
Family
ID=40291331
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08801241A Ceased EP2191294A2 (en) | 2007-09-01 | 2008-09-01 | Adaptive calculation of pulse compression filter coefficients for a radar signal |
Country Status (4)
Country | Link |
---|---|
US (1) | US8193972B2 (en) |
EP (1) | EP2191294A2 (en) |
DE (1) | DE102007041669B4 (en) |
WO (1) | WO2009026911A2 (en) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8947292B2 (en) * | 2009-02-06 | 2015-02-03 | Saab Ab | Radar system and method for a synthetic aperture radar |
US7688257B1 (en) * | 2009-03-24 | 2010-03-30 | Honeywell International Inc. | Marine radar systems and methods |
US8305262B1 (en) * | 2010-03-08 | 2012-11-06 | Lockheed Martin Corporation | Mismatched pulse compression of nonlinear FM signal |
CN101915906B (en) * | 2010-07-20 | 2012-10-31 | 中国人民解放军空军雷达学院 | Adaptive beam forming side lobe shaping method |
JP5810287B2 (en) * | 2010-07-29 | 2015-11-11 | パナソニックIpマネジメント株式会社 | Radar equipment |
RU2503971C1 (en) * | 2012-06-05 | 2014-01-10 | Открытое акционерное общество "Государственный Рязанский приборный завод" | Method to suppress side tabs of autocorrelation function of wideband signal |
US9791548B2 (en) | 2012-09-19 | 2017-10-17 | Furuno Electric Co., Ltd. | Pulse compression radar |
GB201219732D0 (en) * | 2012-11-02 | 2012-12-12 | Qinetiq Ltd | A radar imaging system |
US9417315B2 (en) | 2012-12-20 | 2016-08-16 | The Board Of Regents Of The University Of Oklahoma | Radar system and methods for making and using same |
FR3030774B1 (en) * | 2014-12-19 | 2017-01-20 | Thales Sa | METHOD FOR DETERMINING PARAMETERS OF A COMPRESSION FILTER AND MULTIVOYAL RADAR |
US10001548B2 (en) | 2015-01-23 | 2018-06-19 | Navico Holding As | Amplitude envelope correction |
US20170054449A1 (en) * | 2015-08-19 | 2017-02-23 | Texas Instruments Incorporated | Method and System for Compression of Radar Signals |
US10107896B2 (en) * | 2016-01-27 | 2018-10-23 | Rohde & Schwarz Gmbh & Co. Kg | Measuring device and measuring method for measuring the ambiguity function of radar signals |
CN106093876B (en) * | 2016-07-19 | 2018-11-09 | 西安电子科技大学 | The orthogonal wide main lobe phase encoded signal design method of distributed MIMO radar |
CN106093877B (en) * | 2016-07-19 | 2018-09-21 | 西安电子科技大学 | Orthogonal width main lobe phase encoded signal and mismatched filter combined optimization method |
EP3428681A1 (en) * | 2017-07-14 | 2019-01-16 | Melexis Technologies SA | Method for coded ultrasonic echo detection |
EP3721255A2 (en) | 2017-12-05 | 2020-10-14 | FCS Flight Calibration Services GmbH | Method for passively measuring electromagnetic reflection properties of scattering bodies and method for producing at least one artificial target for a monostatic, rotating radar through a floating platform |
US10725175B2 (en) | 2018-10-30 | 2020-07-28 | United States Of America As Represented By The Secretary Of The Air Force | Method, apparatus and system for receiving waveform-diverse signals |
CN110221262B (en) * | 2019-07-01 | 2021-02-26 | 北京遥感设备研究所 | Radar equipment LFM signal main lobe reduction determination platform and method |
CN111025258B (en) * | 2019-12-04 | 2022-02-08 | 北京理工大学 | Joint mismatch filter for radar waveform diversity and design method thereof |
CN118132898A (en) * | 2024-05-07 | 2024-06-04 | 中国人民解放军空军预警学院 | Active anti-slice forwarding type interference waveform mismatch filter optimization method and device |
Family Cites Families (11)
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US4901082A (en) * | 1988-11-17 | 1990-02-13 | Grumman Aerospace Corporation | Adaptive waveform radar |
JPH0727021B2 (en) * | 1989-02-10 | 1995-03-29 | 三菱電機株式会社 | Synthetic aperture radar device |
US4968968A (en) * | 1989-11-09 | 1990-11-06 | Hughes Aircraft Company | Transmitter phase and amplitude correction for linear FM systems |
US5786788A (en) * | 1996-10-08 | 1998-07-28 | Raytheon Company | Radar system and method for reducing range sidelobes |
DE4230558A1 (en) | 1992-02-07 | 1993-08-12 | Deutsche Aerospace | METHOD FOR DETECTING A TARGET |
US5552793A (en) * | 1994-12-02 | 1996-09-03 | Hughes Missile Systems Company | Self calibrated act pulse compression system |
FR2776392B1 (en) * | 1998-03-23 | 2000-04-28 | Alsthom Cge Alcatel | PULSE COMPRESSION RADAR |
US7313199B2 (en) * | 2002-03-21 | 2007-12-25 | Hypres, Inc. | Power amplifier linearization |
US7019686B2 (en) * | 2004-02-27 | 2006-03-28 | Honeywell International Inc. | RF channel calibration for non-linear FM waveforms |
US8049663B2 (en) * | 2008-05-21 | 2011-11-01 | Raytheon Company | Hardware compensating pulse compression filter system and method |
US7688257B1 (en) * | 2009-03-24 | 2010-03-30 | Honeywell International Inc. | Marine radar systems and methods |
-
2007
- 2007-09-01 DE DE102007041669A patent/DE102007041669B4/en not_active Expired - Fee Related
-
2008
- 2008-09-01 EP EP08801241A patent/EP2191294A2/en not_active Ceased
- 2008-09-01 WO PCT/DE2008/001433 patent/WO2009026911A2/en active Application Filing
- 2008-09-01 US US12/675,939 patent/US8193972B2/en active Active
Non-Patent Citations (2)
Title |
---|
None * |
See also references of WO2009026911A2 * |
Also Published As
Publication number | Publication date |
---|---|
WO2009026911A3 (en) | 2009-05-14 |
US8193972B2 (en) | 2012-06-05 |
DE102007041669A1 (en) | 2009-04-16 |
WO2009026911A2 (en) | 2009-03-05 |
DE102007041669B4 (en) | 2013-04-18 |
US20100194626A1 (en) | 2010-08-05 |
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