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).
Theses
Electronic Resource
English
Controllability of spacecraft attitude using control moment gyroscopes
Tema Archive | 2009
|Spacecraft attitude maneuver using two single-gimbal control moment gyros
Online Contents | 2013
|Spacecraft Attitude Maneuver using Two Single-gimbal Control Moment Gyros
British Library Conference Proceedings | 2012
|