EP 1088199 A1 20010404 - MISSILE GUIDANCE METHOD
Title (en)
MISSILE GUIDANCE METHOD
Title (de)
LENKVERFAHREN FÜR FLUGKÖRPER
Title (fr)
PROCEDE DE GUIDAGE POUR MISSILES
Publication
Application
Priority
- DE 19827168 A 19980618
- EP 9903872 W 19990604
Abstract (en)
[origin: DE19827168A1] The invention relates to a missile guidance method, more particularly for anti-armor projectiles fired directly at a target. In order to avoid missing a target by a narrow margin, the invention provides that the distance to the target (3) be measured with a range finder (8) before the projectile is fired. The flying time previously calculated on the basis of target distance is inputted to the projectile (1). The projectile (1) has one or several sensors which are activated after a predetermined flying time, said sensor or sensors determining whether the projectile (1) will fly over the target at a minimum distance. Optionally, the projectile (1) conducts a single trajectory adjustment with a fixed value.
IPC 1-7
IPC 8 full level
CPC (source: EP US)
F41G 7/007 (2013.01 - EP US); F41G 7/22 (2013.01 - EP US)
Citation (search report)
See references of WO 9966283A1
Designated contracting state (EPC)
AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE
DOCDB simple family (publication)
DE 19827168 A1 19991223; DE 19827168 B4 20190117; AU 4605699 A 20000105; EP 1088199 A1 20010404; US 6488231 B1 20021203; WO 9966283 A1 19991223
DOCDB simple family (application)
DE 19827168 A 19980618; AU 4605699 A 19990604; EP 9903872 W 19990604; EP 99929139 A 19990604; US 71986501 A 20010216