An all rotating platform has been modified with the purpose of having at one's disposal an operative monocopter. The nature of the modifications are described, as well as the control strategy designed and implemented to control the prototype. This strategy corresponds to a H-inf controller in which a nonlinear function has been included to cancel the propeller quadratic force.
Design and implementation of H-inf controller for micro-monocopter
Electronics Letters ; 44 , 12 ; 719-721
2008
3 Seiten, 4 Quellen
Article (Journal)
English
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