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NASA Technical Note [NASA TN D-5868]: Performance of twin gyro attitude control system including passive compensation and nonlinear control law

By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Campbell, Richard A.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1970Description: 98p.Subject(s): Spacecraft | Space vehicle attitude control | Twin control moment gyro
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