GB1535338A - Radar systems - Google Patents

Radar systems

Info

Publication number
GB1535338A
GB1535338A GB4682975A GB4682975A GB1535338A GB 1535338 A GB1535338 A GB 1535338A GB 4682975 A GB4682975 A GB 4682975A GB 4682975 A GB4682975 A GB 4682975A GB 1535338 A GB1535338 A GB 1535338A
Authority
GB
United Kingdom
Prior art keywords
switch
value
target
radar
nov
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
Application number
GB4682975A
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Publication of GB1535338A publication Critical patent/GB1535338A/en
Expired legal-status Critical Current

Links

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
    • G01S7/28Details of pulse systems
    • G01S7/285Receivers
    • G01S7/292Extracting wanted echo-signals

Abstract

1535338 Radar SIEMENS AG 13 Nov 1975 [13 Nov 1974] 46829/75 Heading H4D A radar system is provided with means for detecting manoeuvres of the target in the form of changes in the state of motion, in particular any transition from zero acceleration using a radar receiver incorporating two Kalman filters for the optimum estimation of a variable parameter, the first, for analysing low level target accelerations and the second for higher order accelerations. In Fig. 9, echo signals U are fed to radar receiver Ra where they are converted to digital signals Z k and applied to computer Re. Switch S, controlled by threshold detector Sw is set to connect signals Sk to a 1st low-level Kalman filter Fl, when no manoeuvre is detected. Filter Fl produces estimated values of a state vector #X k representative of the target's position from which a prediction value #X k - is derived. The innovation value I k is formed by the correlation means to establish the difference between each measured value and the relevant prediction value and fed to a shift register Sr of length N. To complete the correlation the numerical values stored in the shift registered positions are then multiplied by respective estimating error factors, S 0 , etc., and added to obtain a total which is applied to threshold detector Sw. Operation of switch S is made, to switch Kalman filters, when said threshold value is exceeded.
GB4682975A 1974-11-13 1975-11-13 Radar systems Expired GB1535338A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742453846 DE2453846C2 (en) 1974-11-13 1974-11-13 ARRANGEMENT FOR FAST DETECTION OF FLIGHT MANEUVERS

Publications (1)

Publication Number Publication Date
GB1535338A true GB1535338A (en) 1978-12-13

Family

ID=5930742

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4682975A Expired GB1535338A (en) 1974-11-13 1975-11-13 Radar systems

Country Status (3)

Country Link
DE (1) DE2453846C2 (en)
FR (1) FR2291504A1 (en)
GB (1) GB1535338A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2214749A (en) * 1988-01-29 1989-09-06 Marconi Co Ltd Radar seeker transient suppressor
GB2220812A (en) * 1980-03-20 1990-01-17 Messerschmitt Boelkow Blohm Aerial combat director

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4144571A (en) * 1977-03-15 1979-03-13 E-Systems, Inc. Vehicle guidance system
US4495580A (en) * 1981-03-30 1985-01-22 E-Systems, Inc. Navigation system
JPS59191608A (en) * 1983-04-11 1984-10-30 ロツクウエル・インタ−ナシヨナル・コ−ポレ−シヨン Improvement in processing through put speed
US4910526A (en) * 1987-05-18 1990-03-20 Avion Systems, Inc. Airborne surveillance method and system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2220812A (en) * 1980-03-20 1990-01-17 Messerschmitt Boelkow Blohm Aerial combat director
GB2220812B (en) * 1980-03-20 1990-06-20 Messerschmitt Boelkow Blohm A combat flight director system
GB2214749A (en) * 1988-01-29 1989-09-06 Marconi Co Ltd Radar seeker transient suppressor
US4991794A (en) * 1988-01-29 1991-02-12 The Marconi Company Limited Radar seeker transient suppressor
GB2214749B (en) * 1988-01-29 1992-02-19 Marconi Co Ltd Radar seeker transient suppressor

Also Published As

Publication number Publication date
DE2453846C2 (en) 1976-09-09
FR2291504B1 (en) 1977-12-16
FR2291504A1 (en) 1976-06-11
DE2453846B1 (en) 1976-01-29

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee