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Three-Axis Attitude Control of a Satellite in Zero Momentum Mode Using a Tilted Wheel Methodology
Conference presentation

Three-Axis Attitude Control of a Satellite in Zero Momentum Mode Using a Tilted Wheel Methodology

LO Inumoh, A Pechev, N Horri and JL Forshaw
AIAA Guidance, Navigation, and Control Conference (Minneapolis, US, 13/08/2012)
17/05/2017

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