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SINGULARITY AVOIDANCE IN A CMG SATELLITE ATTITUDE CONTROL
SINGULARITY AVOIDANCE IN A CMG SATELLITE ATTITUDE CONTROL
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机译:CMG卫星姿态控制中的奇异规避
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摘要
Control moment gyros in an array are rotated to reorient a satellite by an attitude signal. If the signal causes a gyro to have position that will produce a singularity in attitude control, a disturbance is introduced into the signal to avoid the singularity.
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