A study of reaction wheel configurations for a 3-axis satellite attitude controlISMAIL, Zuliana; VARATHARAJOO, Renuganth.Advances in space research. 2010, Vol 45, Num 6, pp 750-759, issn 0273-1177, 10 p.Article

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Fault tolerant control for satellites with four reaction wheelsJIN, Jaehyun; KO, Sangho; RYOO, Chang-Kyung et al.Control engineering practice. 2008, Vol 16, Num 10, pp 1250-1258, issn 0967-0661, 9 p.Article

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