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This document compares three modern control techniques - fuzzy logic, l1, and H-infinity - for controlling the attitude of a flexible spacecraft modelled after an Optus communications satellite. It presents the control design process for each technique. Using a linear model of the Optus satellite, it simulates the response of the system and control inputs to a step input of pi/2 radians for each control method. It lists the advantages and disadvantages of each control technique and outlines directions for f

Author

hossein_AU

Language

EN