GB818494A - - Google Patents

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Publication number
GB818494A
GB818494A GB818494DA GB818494A GB 818494 A GB818494 A GB 818494A GB 818494D A GB818494D A GB 818494DA GB 818494 A GB818494 A GB 818494A
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GB
United Kingdom
Prior art keywords
aerial
target
radar
azimuth
stabilized
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
Publication date
Publication of GB818494A publication Critical patent/GB818494A/en
Expired legal-status Critical Current

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  • Radar Systems Or Details Thereof (AREA)

Abstract

818,494. Radar. ALBISWERK ZURICH A.G. Sept. 3,1956 [Sept. 2, 1955], No. 26909/56. Class 40 (7). Relates to a ship-borne radar system for directing anti-aircraft guns comprising an unstabilized search radar 1 which determines the azimuth α<SP>1</SP>z of a target relative to the unstable deck plane and a fire-directing radar 3 stabilized against roll # and pitch y, the azimuth αz of the target in the stabilized co-ordinates being given by where t is the target elevation. In a first embodiment the aerial 2 of the search radar 1 rotates continuously about an axis normal to the deck plane and the instantaneous azimuthal position α<SP>1</SP> of the aerial 2 in said plane is applied together with the roll and pitch angles # and y and the mean angle of elevation # of the aerial 4 of the stabilized radar 3 to a computer 5 which computes in accordance with the above equation the corresponding azimuth angle α in the stabilized co-ordinates. The output α from the computer 5 is applied to control the angular co-ordinate of a search P.P.I. 6 and a rotatable cursor is continuously aligned with the target response to produce an electrical signal representing the stabilized target azimuth αz which is applied to control the azimuth position of the aerial 4 of the stabilized radar 3. The aerial 4 scans in elevation about the mean angle # until the target is detected. In a modification, Fig. 2 (not shown), the angular co-ordinate of the P.P.I 6 is controlled directly by the unstabilized azimuth angle α<SP>1</SP> and corresponding values of α<SP>1</SP>, # and y are continuously stored during each rotation of the aerial 2. The cursor on the P.P.I. 6 now produces an unstabilized target azimuth signal αz<SP>1</SP> which is applied to the storage device to produce corresponding values of # and y which are applied together with α<SP>1</SP>z and the instantaneous elevation t of the aerial 4 to the computer 5 to produce the required signal αz.
GB818494D Expired GB818494A (en)

Publications (1)

Publication Number Publication Date
GB818494A true GB818494A (en) 1900-01-01

Family

ID=1752362

Family Applications (1)

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GB818494D Expired GB818494A (en)

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GB (1) GB818494A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE977802C (en) * 1964-04-10 1970-07-09 Thomson Houston Comp Francaise Arrangement for establishing and locating targets that are equipped with a jammer
GB2300323A (en) * 1978-09-26 1996-10-30 Bodenseewerk Geraetetech Seeker head
US5702068A (en) * 1978-09-26 1997-12-30 Bodenseewerk Geratetechnik Gmbh Seeker head particularly for automatic target tracking

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE977802C (en) * 1964-04-10 1970-07-09 Thomson Houston Comp Francaise Arrangement for establishing and locating targets that are equipped with a jammer
GB2300323A (en) * 1978-09-26 1996-10-30 Bodenseewerk Geraetetech Seeker head
GB2300323B (en) * 1978-09-26 1997-03-19 Bodenseewerk Geraetetech Seeker head
US5702068A (en) * 1978-09-26 1997-12-30 Bodenseewerk Geratetechnik Gmbh Seeker head particularly for automatic target tracking

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