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Singularity Avoidance of Control Moment Gyros Using Optimization of Initial Gimbal Angles and Application to Multi Target Pointing for Satellite Attitude Control
By: Yasuyuki Nanamori, Masaki Takahashi, Shigemune Taniwaki, Kazuo Yoshida and Yoshiaki Ohkami.
Pub. 2007, 16pgs.
PDF File. AAS 07-398.
Price: $29.00
 

Reprinted from Advances in the Astronautical Sciences Volume 129.

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