Methods and apparatus for projectile guidance

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Reexamination Certificate

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C244S003100

Reexamination Certificate

active

07947938

ABSTRACT:
Methods and apparatus for projectile systems according to various aspects of the present invention comprise a projectile attached to an auxiliary control system. The auxiliary control system may include a control system and a transverse propulsion system. The control system controls the trajectory of the projectile system, for example by activating the transverse propulsion system to adjust the trajectory.

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