Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2011-01-18
2011-01-18
Gregory, Bernarr E (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
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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Gregory Bernarr E
Raytheon Company
Renner , Otto, Boisselle & Sklar, LLP
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