Ammunition article controllable during its final flight phase and method for navigation thereof towards a target

Claim 1

In an article of ammunition which is controllable during its final flight phase; an impulse system in the cross-sectional plane of the center of gravity of said article which is radially oriented and rotatable about the longitudinal axis of said article; sensor means on said article for detecting a target object; and a control circuit on board of said article for activating said impulse system subsequent to the detection of the target object located opposite thereto relative to the momentary orientation of said impulse system; the improvement comprising: said impulse system comprising a plurality of pulse transmitters arranged about the periphery of said article of ammunition, said sensor means providing for the constant tracking of a singly detected target object and for deliverying target deviating information relative to distance and direction to said control circuit, said control circuit activating the particular pulse transmitter which, predicated upon its inherent power range and its momentary orientation counteracts a spatial displacement of a sighting line on board of the article of ammunition towards the detected target object as a result of the thereby produced vectorial change in velocity in the approach of the article of ammunition to the target object.