a method is disclosed for controlling a flight trajectory of a spinning projectile . in one aspect the method may involve supporting a nose of the projectile in a manner permitting the nose to be wobbled . at least one electrically responsive component may be coupled at a first end to the nose and at a second end to a base portion of the projectile . an angular position of the nose of the projectile may be sensed as the projectile flies through an atmosphere after being fired from a weapon . an electrical signal is controllably applied to the electrically responsive component , in relation to the sensed angular position of the nose , to control an attitude of the nose during flight of the projectile .