The roll orientation of a thrust vector control (TVC) or other missile section is measured and used to compensate the operation of the control surface. A measurement of a roll orientation of the control surface relative to the missile is obtained from a detector, memory or other source. Compensated control commands are determined at least in part based upon the measurement to account for the roll orientation of the control surface relative to the missile, and the compensated control command is provided to thereby actuate the control surface during operation of the missile.
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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