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Zhang Honghua Zhang Guofeng ( Beijing Institute of Control Engineering,Beijing10 0 0 80 )
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Abstract: To guarantee the attitude control performance of the large satellite,the mathematical model with flapping motion is derived,the simple controller form is given and the adaptive internal model control is proposed.The analytical and simulation results show that the adaptive internal model control is very effective for the precision control of the large satellites.
Zhang Honghua Zhang Guofeng ( Beijing Institute of Control Engineering,Beijing10 0 0 80 ). Adaptive Internal Model Control of Satellites With Flexible Appendages[J]. .
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