Abstract: A guidance device for projectiles has stationary canards (40) and thrusters (50) positioned on the nose (20) of the projectile (10). The thrusters (50) are initiated from remote or local sensor to provide flight maneuverability to a target.
Type:
Grant
Filed:
July 11, 2000
Date of Patent:
June 11, 2002
Assignee:
The United States of America as represented by the Secretary
of the Army
Inventors:
Anthony Farina, Michael J. Amoruso, Wilfredo Toledo