Method for guiding a military missile

摘要

#CMT# #/CMT# 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. #CMT# : #/CMT# An independent claim is also included for a system including multiple combat missiles. #CMT#USE : #/CMT# Method for controlling a combat missile (claimed) such as a combat rocket i.e. ground supported rocket. Can also be used for a ground-ground-rocket, a ground-air-rocket and a sea-air supported rocket. #CMT#ADVANTAGE : #/CMT# The method allows the combat missile to be adapted to the mission components, and easily controls the combat missile. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic view of four different mission component groups with multiple mission components. A : Fuselage and wing structure B : Missile motor C : Active motor D : Seeker head.