Method for guiding a rocket

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

Reexamination Certificate

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C244S003170

Reexamination Certificate

active

07083139

ABSTRACT:
Method for guiding a rocket (1) to a target, wherein, the rocket (1) being equipped with automatic guiding means with an image-formation device (10) and means for correction of the trajectory (11):the target is acquired by a sighting device and its position is determined;the sighting device and the rocket image-formation device (10) are brought into line;the images of the rocket image-formation device (10) are stabilized;a guiding law is produced;the rocket (1) is launched; andthe rocket is guided according to this law until the rocket itself acquires the target.

REFERENCES:
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patent: 3712563 (1973-01-01), Alpers
patent: 3794272 (1974-02-01), Hecker
patent: 3986682 (1976-10-01), Dryden
patent: 4881270 (1989-11-01), Knecht et al.
patent: 5072396 (1991-12-01), Fitzpatrick et al.
patent: 5785275 (1998-07-01), Hiebl
patent: 5785281 (1998-07-01), Peter et al.
patent: 5881969 (1999-03-01), Miller
patent: 6347762 (2002-02-01), Sims et al.
patent: 6491253 (2002-12-01), McIngvale
patent: 33 34 729 (1985-04-01), None

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