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:
Dec. 14, 2010

Filed:

Sep. 07, 2006
Applicants:

Robert S. Brinkerhoff, Tucson, AZ (US);

Michael J. Mahnken, Way Oro Valley, AZ (US);

Richard D. Loehr, Tucson, AZ (US);

James M Cook, Tucson, AZ (US);

Inventors:

Robert S. Brinkerhoff, Tucson, AZ (US);

Michael J. Mahnken, Way Oro Valley, AZ (US);

Richard D. Loehr, Tucson, AZ (US);

James M Cook, Tucson, AZ (US);

Assignee:

Raytheon Company, Waltham, MA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F42B 15/01 (2006.01); F42B 10/00 (2006.01); F42B 15/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A reliable and inexpensive attitude control system uses a plurality of pitch-over thrusters to perform rapid and precise attitude maneuvers for a flight vehicle. The pitch-over thrusters create rotational moments that directly pitch and yaw the flight vehicle. The use of very simple thrusters and control techniques provides for a reliable and cost effective solution. The ability to perform overlapping pitch and yaw maneuvers with single-shot fixed-impulse thrusters provides for high-speed maneuverability.


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