AU2001257615A1 - Noncoherent integrator for signals with high acceleration uncertainty - Google Patents

Noncoherent integrator for signals with high acceleration uncertainty

Info

Publication number
AU2001257615A1
AU2001257615A1 AU2001257615A AU5761501A AU2001257615A1 AU 2001257615 A1 AU2001257615 A1 AU 2001257615A1 AU 2001257615 A AU2001257615 A AU 2001257615A AU 5761501 A AU5761501 A AU 5761501A AU 2001257615 A1 AU2001257615 A1 AU 2001257615A1
Authority
AU
Australia
Prior art keywords
signals
acceleration
presums
signal processing
frequency domain
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.)
Abandoned
Application number
AU2001257615A
Inventor
Barry G. Mattox
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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
Application filed by Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Publication of AU2001257615A1 publication Critical patent/AU2001257615A1/en
Abandoned legal-status Critical Current

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
    • G01S13/50—Systems of measurement based on relative movement of target
    • G01S13/58—Velocity or trajectory determination systems; Sense-of-movement determination 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
    • 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

Abstract

A radar signal processing method and system for detecting target objects of unknown acceleration and having low SNRs which reduces the computational burdens and provides a more efficient way of performing the operation of non-coherent integration. Radar signal processing is conducted according to a predetermined scheme in which partially processed received signal data is selectively stored and reused, reducing redundant processing. The radar system receives return signals frequency shifted from a predetermined frequency scheme by unknown amounts. The received signals are coherently integrated transforming them into frequency domain templates which are non-coherently arranged into an array matrix. The data of the frequency domain templates are processed to form presums which are stored for use in forming higher level presums and for forming acceleration bins. Once the acceleration bins have been formed, they are analyzed to detect the presence of target object return signals.
AU2001257615A 2000-04-28 2001-04-23 Noncoherent integrator for signals with high acceleration uncertainty Abandoned AU2001257615A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09559665 2000-04-28
US09/559,665 US6437729B1 (en) 2000-04-28 2000-04-28 Integrator for radar return signals with high acceleration uncertainty
PCT/US2001/040570 WO2001084179A1 (en) 2000-04-28 2001-04-23 Noncoherent integrator for signals with high acceleration uncertainty

Publications (1)

Publication Number Publication Date
AU2001257615A1 true AU2001257615A1 (en) 2001-11-12

Family

ID=24234508

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001257615A Abandoned AU2001257615A1 (en) 2000-04-28 2001-04-23 Noncoherent integrator for signals with high acceleration uncertainty

Country Status (9)

Country Link
US (1) US6437729B1 (en)
EP (1) EP1287378B1 (en)
AT (1) ATE337563T1 (en)
AU (1) AU2001257615A1 (en)
DE (1) DE60122506T2 (en)
ES (1) ES2269391T3 (en)
IL (1) IL152495A0 (en)
NO (1) NO20025170L (en)
WO (1) WO2001084179A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6538599B1 (en) * 2001-11-16 2003-03-25 Raytheon Company Noncoherent gain enhancement technique for non-stationary targets
DE10260492A1 (en) * 2002-12-21 2004-07-01 Volkswagen Ag Device and method for determining the relative acceleration
US6828929B2 (en) * 2003-01-30 2004-12-07 Raytheon Company Technique for non-coherent integration of targets with ambiguous velocities
US8604971B2 (en) * 2009-12-01 2013-12-10 Bae Systems Information And Electronic Systems Integration Inc. Scanning near field electromagnetic probe
US9140784B1 (en) * 2013-02-27 2015-09-22 Lockheed Martin Corporation Ballistic missile debris mitigation
JP6207376B2 (en) * 2013-12-17 2017-10-04 三菱電機株式会社 Target detection device
JP6242276B2 (en) * 2014-04-16 2017-12-06 三菱電機株式会社 Radar equipment
JP6755002B2 (en) * 2016-05-26 2020-09-16 パナソニックＩｐマネジメント株式会社 Sensor device and lighting device
US10718860B2 (en) * 2018-01-11 2020-07-21 Infineon Technologies Ag System and method to improve range accuracy in FMCW radar using FSK modulated chirps
US11035931B1 (en) * 2018-10-29 2021-06-15 Ansys, Inc. Accelerated radar data processing via limited pulse extrapolation

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3885240A (en) * 1967-06-27 1975-05-20 Us Navy Storage radar system
US5235338A (en) * 1990-10-31 1993-08-10 Hsiao Stephen S Moving target detection through range cell migration radar
US5784026A (en) * 1996-09-23 1998-07-21 Raytheon E-Systems, Inc. Radar detection of accelerating airborne targets
US6018311A (en) * 1998-07-14 2000-01-25 Raytheon Company Noncoherent gain enhancement technique for improved detection-estimation performance
US6313785B1 (en) * 2000-04-28 2001-11-06 Lockheed Martin Corporation Dual detection processing for detecting signals with high acceleration uncertainty

Also Published As

Publication number Publication date
NO20025170D0 (en) 2002-10-28
EP1287378A4 (en) 2004-11-24
EP1287378A1 (en) 2003-03-05
ES2269391T3 (en) 2007-04-01
IL152495A0 (en) 2003-05-29
DE60122506T2 (en) 2007-04-05
WO2001084179A1 (en) 2001-11-08
NO20025170L (en) 2002-12-27
EP1287378B1 (en) 2006-08-23
DE60122506D1 (en) 2006-10-05
ATE337563T1 (en) 2006-09-15
US6437729B1 (en) 2002-08-20

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