Control moment gyro /CMG/ for spacecraft attitude control, determining optimal gimbal angle rate for desired torque
Optimal control moment gyro distribution and steering laws
AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ASTRODYNAMICS CONFERENCE ; 1970 ; SANTA BARBARA, CA
1970-08-01
Conference paper
No indication
English
A Generalized Framework for Linearly-Constrained Singularity-Free Control Moment Gyro Steering Laws
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