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
01.08.1970
Aufsatz (Konferenz)
Keine Angabe
Englisch
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