Root / Conference Proceedings / 3rd INTERNATIONAL CONFERENCE "PHYSICS AND CONTROL" (PhysCon 2007) / Nonlinear Gyromoment Spacecraft Attitude Control with Precise Pointing the Flexible Antennas

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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