Global Patent Index - EP 2405233 B1

EP 2405233 B1 20150211 - Method for guiding a military missile

Title (en)

Method for guiding a military missile

Title (de)

Verfahren zum Steuern eines Gefechtsflugkörpers

Title (fr)

Procédé de commande d'une munition aérienne

Publication

EP 2405233 B1 20150211 (DE)

Application

EP 11005432 A 20110702

Priority

  • DE 102010026428 A 20100708
  • DE 102010052202 A 20101124

Abstract (en)

[origin: EP2405233A2] The method involves controlling mission components during flight of a combat missile by a control unit. Detection data for the mission components are contained in a data storage. Type data is read out from the mission components by the control unit. Types of the mission components are identified based on the detection data and the type data by the control unit. Control steps are executed based on the type of the mission components by the control unit. Flight data of the combat missile is calculated from mission data. An independent claim is also included for a system including multiple combat missiles.

IPC 8 full level

F42B 15/01 (2006.01)

CPC (source: EP)

F41G 7/2253 (2013.01); F41G 7/226 (2013.01); F41G 7/2293 (2013.01); F42B 15/01 (2013.01)

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DOCDB simple family (publication)

EP 2405233 A2 20120111; EP 2405233 A3 20140625; EP 2405233 B1 20150211; DE 102010052202 A1 20120112; IL 213934 A0 20111201; IL 213934 A 20141231

DOCDB simple family (application)

EP 11005432 A 20110702; DE 102010052202 A 20101124; IL 21393411 A 20110705