In this technical note, we deal with the attitude tracking and disturbance rejection problem of spacecraft for a class of persistent disturbances with unbounded energy which include the sinusoidal disturbance as a special case. The approach involves the integration of techniques from robust control, adaptive control, and robust output regulation theory.
Journal title
IEEE Transactions on Automatic ControlVolume
54Issue
3Pagination
600-605Publisher
Institute of Electrical and Electronics Engineers (IEEE)College/Research Centre
Faculty of Engineering and Built EnvironmentSchool
School of Electrical Engineering and Computer ScienceRights statement
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