SMALL SATELLITE ATTITUDE CONTROL USING LINEAR MOVING MASS ACTUATORS Jacob Bean Advisor: Dr. Troy Henderson Department of Aerospace and Ocean Engineering Virginia Polytechnic Institute and State University, Blacksburg, Va

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Date: 2013-05-02 13:43:42 Physics Mechanics Motion physics) Rotation Physical quantities Gyroscopes Rigid bodies Moment of inertia Angular momentum Rotation around a fixed axis Reaction wheel Inertial measurement unit		SMALL SATELLITE ATTITUDE CONTROL USING LINEAR MOVING MASS ACTUATORS Jacob Bean Advisor: Dr. Troy Henderson Department of Aerospace and Ocean Engineering Virginia Polytechnic Institute and State University, Blacksburg, Va Add to Reading List Source URL: www.vsgc.odu.edu Download Document from Source Website File Size: 1,12 MB Share Document on Facebook

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