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Autonomous Helicopter Model Flight Using Robust H2-Type Switching Control

E. Joelianto

Abstract


This paper presents robust H2-type control design for a small scale helicopter with five mathematical models to represent wide mode flight operation. The robust controller is designed by describing the mathematical models as a linear impulsive system for each mode. Simulation shows the performance of the robust controller for landing mission.

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References


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DOI: http://dx.doi.org/10.21535%2FProICIUS.2011.v7.379

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