EP 0234030 B1 19901128 - GUIDANCE SYSTEM FOR A MISSILE
Title (en)
GUIDANCE SYSTEM FOR A MISSILE
Publication
Application
Priority
CH 34986 A 19860130
Abstract (en)
[origin: US4709875A] The apparatus for guiding a missile generates an electromagnetic guide beam such as a CO2-laser guide beam including spatial coding. For spatially encoding the guide beam there is employed a modulator as well as a scanning device which are intercoupled by means of a computer. The guide beam is moved in steps or increments by the scanning device in order to scan individual field sectors of a scanning field. Following each individual step, a code is transferred to or associated with a scanned field sector of the scanning field by the guide beam such that for each field sector of the scanning field a code is generated which indicates the actual position of the missile, and a code which indicates the desired position of the missile. Consequently, a number of missiles can be guided simultaneously in different field sectors.
IPC 1-7
IPC 8 full level
F41G 7/26 (2006.01)
CPC (source: EP US)
F41G 7/26 (2013.01 - EP US)
Designated contracting state (EPC)
BE CH DE ES FR GB IT LI NL SE
DOCDB simple family (publication)
EP 0234030 A1 19870902; EP 0234030 B1 19901128; CA 1264842 A 19900123; DE 3675926 D1 19910110; DK 48287 A 19870731; DK 48287 D0 19870129; ES 2019870 B3 19910716; IL 81417 A0 19870831; IL 81417 A 19930610; NO 165814 B 19910102; NO 165814 C 19910410; NO 870062 D0 19870107; NO 870062 L 19870731; US 4709875 A 19871201
DOCDB simple family (application)
EP 86117392 A 19861213; CA 528161 A 19870126; DE 3675926 T 19861213; DK 48287 A 19870129; ES 86117392 T 19861213; IL 8141787 A 19870129; NO 870062 A 19870107; US 569787 A 19870122