An integrated propulsion and guidance system for an aircraft or other vehicle includes an engine coupled to a propeller via a driveshaft to produce propulsive force. One or more of the propeller blades are pivotably mounted with respect to the hub of the propeller. A control signal is provided to adjust the blade pitch of the pivotable blades as the blades rotate about the hub. The change in blade pitch as the blade rotates produces a torque imbalance that can be used to control the heading of the vehicle. By varying the magnitude and phase of the control signal provided to the propeller, the torque can be applied in a multitude of distinct reference planes, thereby allowing the orientation of the vehicle to be adjusted through action of the pivotable propeller blade(s).
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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