Nonlinear Gyromoment Spacecraft Attitude Control with Precise Pointing the Flexible Antennas

Yevgeny Somov, Sergey Butyrin, Sergey Somov

New approach for modeling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on spacecraft attitude guidance and digital gyromoment nonlinear control with precise pointing the large-scale flexible antennas, are presented

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