Attitude control of a spacecraft using two SGCMGs

Attitude control of a spacecraft using two SGCMGs

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998. === Includes bibliographical references (leaves 53-54). === This thesis presents new methods for controlling spacecraft using Control-Moment Gyros (CMGs). CMGs generate torque to change and maintain a spacec...

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Bibliographic Details
Main Author: Kwon, Hyuk-Sang, 1971-
Other Authors: Seth Lloyd.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2005
Subjects:
Mechanical Engineering
Online Access:http://hdl.handle.net/1721.1/9725

Internet

http://hdl.handle.net/1721.1/9725

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