Design and experimental evaluation of rotor speed regulators for model helicopters in a test bench

Abstract

This work is focused on the design of a rotor speed regulator for small-scale helicopters. A nominal model identification procedure for the main rotor system is performed using an iterative hybrid procedure. Such a model has both linear and nonlinear components and models not only engine throttle but also the effect of collective pitch variation. Collective… (More)
DOI: 10.1109/IROS.2007.4399549

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