Abstract: A guided artillery projectile with a flight attitude or trajectory regulator in the autopilot of the projectile for the guidance of a transition into a gliding trajectory at the assumption of a predetermined pitch angle after the passage through the apogee of the ballistic firing trajectory.
Type:
Grant
Filed:
October 21, 1988
Date of Patent:
November 28, 1989
Assignee:
Diehl GmbH & Co.
Inventors:
Karl-Heinz Lachmann, Peter Sundermeyer, Johann Schreier, Albrecht Reindler, Jurgen Leininger