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Atwo degree-of-freedom controller structure is proposed in this paper for robust tracking of desired trajectories. The inputs required for these trajectories, estimated by an augmented state-space model approach, constitutes the feed-forward part that ensures output tracking for the nominal plant model, and a feedback part, via a multiple model approach, makes the overall system robust. This method is then applied to helicopter hover control.

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International Journal of Aerospace Innovations


International Journal of Aerospace Innovations

Print ISSN: 1757-2258

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