Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2008-05-06
2008-05-06
Gregory, Bernarr E. (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
C244S003100, C089S001110
Reexamination Certificate
active
07367525
ABSTRACT:
A munition is presented which includes an integrity verification system that measures the integrity of the munition. When an integrity threshold is not met, engagement of the munition with a predetermined target is aborted. Also presented is a methodology for gating the engagement of the munition with the target. The methodology includes performing an integrity check of the munition after it is deployed. The method further includes aborting the engagement of the target when the integrity check of the munition fails.
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Britigan John D.
Habereder Hans L.
McKendree Thomas L.
Daly, Crowley & Mofford & Durkee, LLP
Gregory Bernarr E.
Raytheon Company
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