Spacecraft Attitude Control with Precise Pointing the Flexible Antennas?
نویسنده
چکیده
New approach for modelling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on communication satellite attitude guidance and digital robust control with precise pointing the large-scale flexible antennas, are presented.
منابع مشابه
Guidance and Robust Gyromoment Attitude Control of a Large-Scale Communication Satellite
New approach for modelling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on communication satellite attitude guidance and digital robust control with precise pointing the large-scale flexible antennas, are presented.
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