Attitude control of a spacecraft using two SGCMGs.
Attitude control of a spacecraft using two single Gimbal control moment gyroscopes
1998
63 pages , 3580791 byte , 3580552 byte
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.
Includes bibliographical references (leaves 53-54).
Hochschulschrift
Elektronische Ressource
Englisch
Controllability of spacecraft attitude using control moment gyroscopes
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