Guidance control for spinning or rolling projectile

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8426788
APP PUB NO 20120175458A1
SERIAL NO

13005175

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A projectile, air vehicle or submersible craft with a spinning or rolling fuselage, rotating on its axis, has a collar which can be positioned relative to a longitudinal axis of the projectile using aerodynamic forces. Aerodynamic surfaces, such as lift-producing surfaces, for example tails or canards, are coupled to the collar, and rotate with the collar. An actuator system or mechanism controls orienting of the lift-producing surfaces, such as tilting of the lift producing surfaces, to direct the collar into a desired position relative to a longitudinal axis of the projectile, and to maintain the collar in that position. With such a control the projectile is able to be steered using bank-to-turn maneuvering. The actuator system may use any of a variety of mechanisms to move the lift-producing surfaces, thereby positioning the collar.

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Patent Owner(s)

Patent OwnerAddress
RAYTHEON COMPANY1100 WILSON BLVD ARLINGTON VA 22209

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Geswender, Chris E Green Valley, US 36 382

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