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Attitude control for satellites: variable gain sliding mode

keywords SMC, SPACECRAFT DYANMICS

Reference persons ELISA CAPELLO

Research Groups 08- Dinamica, controllo e simulazione del volo

Description The student will study the problem of precise attitude control for satellites, with a variable gain sliding mode controller

Required skills Control laws and spacecraft dynamics


Deadline 15/02/2020      PROPONI LA TUA CANDIDATURA




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