Flight path correction method for artillery shell uses correction elements deployed during flight incorporated in body of shell, shell detonator, or correction unit

摘要

The flight path correction method uses selectively deployed correction elements (10.1,10.2) projecting from the body of the shell (1), the shell detonator (2), or a separate correction unit (5) which rotates during the flight of the shell with a roll frequency of between 5 and 30 Hz, with an air bearing between the correction unit and the shell. An Independent claim is also included for a flight path correction device .