Controllability of spacecraft attitude using control moment gyroscopes

descriptionPublicationkeyboard_double_arrow_right Article , Conference object 01 Jan 2006 India Publisher:IEEEJournal:2006 American Control Conference

Authors: Sanjay P. Bhat; Pawan K. Tiwari;

doi: 10.1109/acc.2006.1657281 , 10.1109/tac.2008.2008324

handle: 10054/744 , 100/1269

Controllability of spacecraft attitude using control moment gyroscopes

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Abstract

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India

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Keywords

Controllability, Attitude Control, Gyroscopes, Angular Momentum, Nonlinear Control System, Attainable sets, reachability, Steering Law, Control of mechanical systems, Orbital mechanics, Gyro Systems, Control/observation systems governed by ordinary differential equations, Control Moment Gyroscopes

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