The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 14, 2016

Filed:

Feb. 25, 2015
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Harry R. Barnard, Bynum, TX (US);

Toby D. Thomas, Southlake, TX (US);

Assignee:

LOCKHEED MARTIN CORPORATION, Bethesda, MD (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F41G 7/22 (2006.01); F42B 15/01 (2006.01); F41G 3/14 (2006.01); G05D 1/12 (2006.01); G05D 1/08 (2006.01); F41G 7/20 (2006.01); F41G 7/00 (2006.01); F42B 15/00 (2006.01);
U.S. Cl.
CPC ...
F42B 15/01 (2013.01); F41G 3/145 (2013.01); F41G 7/20 (2013.01); F41G 7/22 (2013.01); G05D 1/0808 (2013.01); G05D 1/12 (2013.01);
Abstract

Embodiments relate to a projectile system, method and computer program product for controlling the flight of a projectile to make a course change by approximately 90°, greater than 90° or up to 90°. The projectile system comprises a gun-fired projectile having a body, at least one tail fin, a motor firing during a first flight phase and during a second flight phase and at least one controllable canard. The projectile system includes one or more processors configured to determine a turn maneuver profile to a target during the first flight phase, produce control signals to destabilize the body, create a pitch attitude change for the turn maneuver profile and effectuate a turn of the projectile in a direction corresponding to the turn maneuver profile during the first flight phase. The processors control the motor to start the second flight phase to the target after the turn.


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