U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Control system for gun and artillery projectiles

Patent 5788180 Issued on August 4, 1998. Estimated Expiration Date: Icon_subject November 26, 2016. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3088407

3202382

3235204

3485173

Cannon launched platform
Patent #: 4155521
Issued on: 05/22/1979
Inventor: Evans ,   et al.

Guidance devices
Patent #: 4193567
Issued on: 03/18/1980
Inventor: McCarty, Jr.

Spin-stabilized projectile and guidance system therefor
Patent #: 4347996
Issued on: 09/07/1982
Inventor: Grosso

Gyroscopically steerable bullet
Patent #: 4431150
Issued on: 02/14/1984
Inventor: Epperson, Jr.

Mortar system with improved round
Patent #: 4533094
Issued on: 08/06/1985
Inventor: Geis ,   et al.

Guided projectile flight control fin system
Patent #: 4565340
Issued on: 01/21/1986
Inventor: Bains

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Inventors

Application

No. 756376 filed on 11/26/1996

US Classes:

244/3.21, Attitude control mechanisms244/3.15Automatic guidance

Examiners

Primary: Jordan, Charles T.
Assistant: Wesson, Theresa M.

Attorney, Agent or Firm

International Class

F41G 007/00

Abstract

A directional control system for ballistic projectiles, including a projectile capable of being fired from a gun, a tracking device within the projectile capable of sensing and identifying a preferred target direction, a moveable mass located within the projectile, an electromagnetic mass-shifting device within the projectile capable of reversibly moving the mass from a first position to a second position whereby the flight path of the projectile is controlled. The directional control system may be used with a projectile which has no externally protruding bodies. The system includes at least one microprocessor programmed to obtain input from the tracking device and to perform calculations to determine movements of the mass. The moveable mass is positioned to shift the momentum vector perpendicular to the central longitudinal spin axis of the projectile when in motion. The mass shifting device preferably includes an electromagnetic driver, which is aligned such that the mass can be moved reversibly from a first position to a second position. The system preferably includes a tracking device including optical fibers for receiving incoming radiation. The system may include a tracking device which is sensitive to radio frequency radiation, and has at least one antenna sensitive to radio frequency radiation. The tracking device may alternatively have at least one infrared detector sensitive to infrared radiation, and preferably has a pyroelectric detector pair.

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