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

First Page		Document Content
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

	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 DocID: 1qMcV - View Document
	MITSUBISHI ELECTRIC RESEARCH LABORATORIES http://www.merl.com MPC for Coupled Station Keeping, Attitude Control, and Momentum Management of Low-Thrust Geostationary Satellites DocID: 1qJwc - View Document
	The Cubli: A Reaction Wheel Based 3D Inverted Pendulum Mohanarajah Gajamohan, Michael Muehlebach, Tobias Widmer, and Raffaello D’Andrea Abstract— The Cubli is a 15 × 15 × 15 cm cube with reaction wheels mounted on DocID: 1lDbj - View Document
	Millennium Space Systems Wins Commercial Reaction Wheel Contract Reaction Wheel Production Line Ramps Up for Commercial Satellite Constellation EL SEGUNDO, California—October 16, 2014: Millennium Space Systems, a leade DocID: 1gCOz - View Document
	PRESS RELEASE: FOR IMMEDIATE DISTRIBUTION Millennium Space Systems granted exclusive license from NASA Goddard Patented Demiseable Integrated Reaction Wheel Assembly Development Kicks Off EL SEGUNDO, California—Februar DocID: 1gkJN - View Document