Patent ID: 9157702
Filing Date: 2015-10-13
Classification: F41G,F42B

Abstract:
1. A munition guidance system, comprising: a generally tubular enclosure, having an internal cavity adapted for receiving a munition, wherein an outer diameter of said enclosure is at most the largest outer diameter of said munition; a plurality of guidance wings enclosed within said enclosure and configured for being erected outwardly from said enclosure; a target identification unit for identifying a target; and a processing and control unit enclosed within said enclosure and being configured for erecting said wings based on at least one criterion, and for controlling said guidance wings so as to maneuver said munition while flying; wherein said at least one criterion is at least one of: (i) time of flight of said munition, (ii) positive identification signal received from said target identification unit, and (iii) relative location data received from said target identification unit.