Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2006-02-07
2010-11-16
Gregory, Bernarr E (Department: 3662)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
C244S003100, C244S003160, C244S003190, C244S003210, C102S382000, C102S384000, C102S473000, C102S501000, C701S200000, C701S224000
Reexamination Certificate
active
07834300
ABSTRACT:
A method and system for guiding and controlling an ordinance body having a trajectory and a bore sight angle including making corrections to the trajectory based on bore sight angle vs. time history. The system is incorporated with existing fuse components in a replacement kit for existing munitions. The method determines nominal time values of the ballistic trajectory of the munition in relation to launch time and determines deviation from the nominal time values by an algorithm by analyzing signals received from a source of radiation located at the target. A processor determines lateral (left/right) and range errors and provides commands to a plurality of flight control surfaces mounted on the munition.
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Carlson Mark A.
Maynard John A.
Zemany Paul D.
BAE Systems Information and Electronic Systems Integration Inc.
Gregory Bernarr E
Long Daniel J.
Sand Michael
Sand & Sebolt
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