Methods and apparatus for guiding a projectile

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

Reexamination Certificate

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Details

C244S003100, C244S003150, C244S003210

Reexamination Certificate

active

07872215

ABSTRACT:
Methods and apparatus for guiding a projectile according to various aspects of the present comprise a force source disposed on the projectile and a control system operably connected to the force source. The control system is configured to initially activate the force source when the force source is substantially in a selected rotational position, and subsequently activate the force source when the force source rotates to substantially the selected rotational position a second time.

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patent: 5123611 (1992-06-01), Morgand
patent: 6695251 (2004-02-01), Rodden et al.
patent: 7416154 (2008-08-01), Bittle et al.

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