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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Flight-control system for canard-controlled flight vehicles and methods for adaptively limiting acceleration

Invented by: Richard E. Hindman
Tucson, AZ

Kyle David Andringa
Sahuarita, AZ

Darrell B. Ridgely
Oro Valley, AZ Applicant: Name City State Country Type Hindman

Originally Assigned to: Raytheon Company
Waltham, MA
[Now assigned to . . .]

Issued:2014-08-26
Filed:2010-12-01
Application No:12957557
Examined by:Swiatek; Rob

Embodiments of a flight-control system and methods of reducing the probability of a roll-control reversal in a canard-controlled flight vehicle are generally described herein. In some embodiments, the flight-control system may monitor angular velocities of the flight vehicle to detect the onset of instability and adaptively control an acceleration limit of the flight vehicle based on the detected instability to reduce the probability of a roll-control reversal. The onset of instability may be detected by persistently high angular velocities. The acceleration limit may be further adaptively controlled based on an approach of a vehicle trim limit.

[pdf] U.S. Pat. No. 8,816,260

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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